USH526H - Non-metallic chassis structure with electromagnetic field attenuating capability - Google Patents

Non-metallic chassis structure with electromagnetic field attenuating capability Download PDF

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Publication number
USH526H
USH526H US07/112,007 US11200787A USH526H US H526 H USH526 H US H526H US 11200787 A US11200787 A US 11200787A US H526 H USH526 H US H526H
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chassis
film layer
coating
metallic film
metallic
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US07/112,007
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Martin B. Miller
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US Air Force
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US Air Force
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    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K9/00—Screening of apparatus or components against electric or magnetic fields
    • H05K9/0007—Casings
    • H05K9/0045—Casings being rigid plastic containers having a coating of shielding material

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  • This invention relates to the field of laminate structures and to a class of such structures used for both mechanical support and electromagnetic radiation shielding in electronic apparatus.
  • Organic material structures are increasingly selected for fabricating the chassis, cabinets, enclosures, racks, cases and bases employed in modern military and commercial electronic equipment.
  • chassis or enclosures with the terms chassis and enclosure being used interchangeably.
  • a large incentive in the movement to organic material structures for military electronic equipment stems from the present peacetime environment for military development wherein small production runs and frequent design changes are major development considerations.
  • the absence of standardized shapes and dimensions for the variety of electronic systems purchased by government agencies together with the small number of large quantity production runs available have also contributed to the need for flexible and low-cost structures.
  • Metallic materials especially aluminum sheet metal have previously been used in ground-based and airborne electronic equipment structures and doubtless will continue to be favored for many such applications.
  • Aluminum sheet metal in thicknesses of 0.062 inch, 0.092 inch, 0.125 inch, and 0.188 inch are particularly popular in constructing such present-day military electronic equipment.
  • non-metallic materials such as fiberglass-reinforced with an epoxy impregnant are desirable for electronic systems.
  • integrated circuit electronics for example, the need for the structural strength of metallic enclosures and has decreased while the pressure for small size, conformable physical shape, light weight low cost, and predictable reliability have remained present and increasing in intensity.
  • electromagnetic shielding both between portions of a given circuit and for containment or exclusion of electromagnetic fields.
  • Such fields affect the performance of nearby electronic apparatus, cause undesirable exposure of living organisms to electromagnetic radiation, and contribute to the military detectability of an electronic apparatus.
  • the term "interference active" or “active” is used herein to generically describe electronic equipment which may be either sensitive to externally-sourced electromagnetic radiation or act as a source of electromagnetic radiation that is undesirable and in need of confinement--that is to represent both EMI/RFI receivers and transmitters.
  • EMI is, of course, an abbreviation for electromagnetic interference and RFI designates radio frequency interference.
  • the electromagnetic radiation can be of the electric field (E field) or magnetic field (H field) type, or a combination of E and H fields.
  • An organic layer and metal film layer laminate composition is found desirable for meeting these needs in many electronic systems.
  • the properties of electrical conductivity and magnetic shielding are found to be particularly determinative of the materials used in such laminate structures.
  • the patent art includes several examples of laminate structures used in electronic equipment.
  • This art includes the patent of Leonard J Costanza U.S. Pat. No. 3,806,928, which concerns a laminated sandwich joint structure for honeycomb sections subjected to radiation at radar frequencies.
  • the Costanza patent is concerned with maintaining the electrical continuity between large multi-layer sections of objects such as a jet engine air intake diffuser where it is desirable to maintain the electrical properties of the structure without abrupt changes resulting from the presence of physical joints.
  • the structure of the Costanza patent includes epoxy-impregnated fabric layers with some of the fabric material being impregnated by conductive carbon such as acetylene black or furnace black, and with the fabric layers being comprised of woven fiberglass filaments.
  • Costanza patent The goal of the Costanza patent is actually to achieve minimum discontinuities in the electrical properties of the connected honeycomb sections in order that radar reflections from the assembled structure are minimized. Conversely, the Costanza arrangement is also useful in constructing radar-transparent honeycomb structures for use in situations where minimum attenuation of a radar signal is desirable, as in a radome for example.
  • the absorptive material in the Adkins shield structure may comprise steel wool, carbon-impregnated rubber, ferrite in a plastic-stranded carrier, or some combination of similar lossy materials; the conductive material layer is comprised of conductor having sheet resistivity preferably in the range of 1.5 ⁇ 10 -6 to 100 ⁇ 10 -6 ohm-cm.
  • radio frequency shielding arrangement is shown in the patent of William A. Manly, U.S. Pat. No. 4,371,742, which discloses an absorptive shield for transmission lines.
  • the shield of the Manly patent is composed of flexible materials filled with ferromagnetic or ferrimagnetic powders of selected particle size and distribution; the particles used may include varieties of iron, nickel, and cobalt.
  • the absorptive magnetic material of the Manly patent is also shown configured into objects such as an enclosure for electronic equipment.
  • An object of the present invention is to provide an electronic chassis structure which is largely non-metallic in composition
  • Another object of the invention is to provide a structural composition useful in the fabrication of electronic apparatus having need for an alternate to conventional metal fabrication, together with the need for electromagnetic shielding requirements.
  • Another object of the invention is to provide a desirable combination of metallic films for use in non-metallic electronic structural members.
  • Another object of the invention is to provide an electronic chassis structure which combines a non-metallic substrate with a multi-layer double surface metal film shielding arrangement.
  • a chassis for use with radio frequency electromagnetic interference active electronic apparatus that includes an organic material substrate member configured as a closable geometric shape having a plurality of angularly disposed connected-together surface portions and a closure means for closing the substrate member, with the closure means including a closure surface portion.
  • the chassis includes arrangements located on the surface portions for mounting components of the electronic apparatus, plus a multi-layered electromagnetic radiation energy shielding and physical protection coating located on a plurality of the surface portions, the coating further including a first metallic film layer disposed over both faces of the surface portions in intimate physical contact therewith, a second metallic film layer disposed over the first film layer of the surface portions in physical contact with the first film layer and wherein the first and second metallic films are composed of different metals at least one of which is a good electrical conductor.
  • FIG. 1 is an electronic chassis or enclosure in accordance with the present invention together with a representative electronic hardware system.
  • FIG. 2 is an enlarged cross-sectional view of the FIG. 1 chassis taken along the cutting line 2--2 in FIG. 1.
  • FIG. 3 shows the relationship between shielding effectiveness and frequency for the material used in the FIG. 1 and FIG. 2 structure when subjected to electric fields of varying frequency.
  • FIG. 4 shows the relationship between shielding effectiveness and frequency for the material used in the FIG. 1 and FIG. 2 structure when subjected to magnetic fields of varying frequency.
  • FIG. 5 shows the test arrangement for measuring shielding effectiveness.
  • FIG. 6 shows the relationship between electric field shielding effectiveness and frequency using a different frequency scale and different test panel size.
  • FIG. 7 shows the relationship between magnetic field shielding effectiveness and frequency using a different frequency scale and different test panel size.
  • FIG. 8 is a flow diagram for fabricating a chassis of the present type.
  • FIG. 1 of the drawings there is shown an exploded view of a typical electronic chassis or enclosure which may be fabricated according to the present invention.
  • the FIG. 1 chassis includes a closable or main portion 100 having top and bottom ends 102 and 104 and fixed sides 106 and 108 which meet the ends 102 and 104 in substantially right angles.
  • the FIG. 1 chassis also includes a cover or closure member 110 which is also formed in the shape of a right angle and is arranged to mate with the open sides of the main portion 100.
  • the cover or closure member 110 includes a pair of sides 112 and 114 and also includes a pair of integrally connected internal shield members 116 and 118 which surround a portion of the enclosed electronic apparatus when the cover 110 is fixed in place on the chassis main portion 100.
  • the cover 110 in FIG. 1 further includes a window member 122 and window housing 120, which serve to admit light from an examined scene to the electro-optical apparatus enclosed by the FIG. 1 chassis.
  • the cover 110 is arranged to accommodate a plurality of fastening members 128 which may be in the form of machine screws or spring engaging fasteners of the type known in the fastening art.
  • the fastening members 128 cooperate with mating portions 130 located in an orthogonal lip 132 surrounding the opening of the chassis closable main portion 100 in FIG. 1.
  • a plurality of printed circuit boards indicated generally at 138, 140, and 142 are shown mounted in the closable portion of the FIG. 1 chassis by way of machine screws or the like 156 which may engage the respective side and end portions of the FIG. 1 chassis by way of holes, standoff supports and nuts, or alternately and preferably, by way of attached bosses integral with and extended inward from the inner surface of the fixed sides and bottom of the FIG. 1 chassis.
  • an electro-optic scanner 143 an apparatus typical of the small signal, electromagnetic radiation sensitive equipment which might be mounted in a FIG. 1 type chassis.
  • Other such radiation sensitive equipment might include radio frequency receivers, ionized particle detectors and the sense amplifiers used in EDP systems.
  • a chassis of the FIG. 1 type might also be useful for enclosing an apparatus such as an oscillator which tends to generate strong electromagnetic fields capable of disrupting adjacent electronic circuits or providing undesirable detectability if allowed to escape from the chassis.
  • the electro-optic scanner apparatus 143 generally includes lenses 144, 146 and 148, an optical signal to electrical signal transducing retina 150, a plurality of integrated circuit packages 152 which may comprise, for example, a RAM memory and a plurality of discrete transistors 154.
  • the internal shield members 116 and 118 surround the electro-optic scanner apparatus 143 when the cover 110 is placed in mating position with the closable portion of the FIG. 1 chassis, such shielding preventing the coupling of strong signals from the integrated circuits 152 and the transistors 154, for example, into the low-level circuitry of the retina 150 and the preamplifiers associated therewith.
  • the construction of the bottom and side members 104, 106, 108, 112, and 114 is also arranged to minimize the coupling of externally-sourced electromagnetic radiation to the low-level circuitry of the scanner 143.
  • the scanner and electronic circuitry shown in FIG. 1 may, for example, be a part of an electronic imaging apparatus intended for mounting in an aircraft or spacecraft for the purpose of transmitting signals representing viewed images to a remote location; the scanner 143 therefore could comprise a portion of an overall system and could be the computer-controlled generator of modulating signals for a radio frequency transmitter which is not shown.
  • the radio frequency electric and magnetic fields from such as transmitter would, however, require exclusion from the low-level circuitry of the retina 150 thereby necessitating use of shielding construction in the FIG. 1 apparatus and in the radio frequency circuitry housing.
  • FIG. 1 In the present peacetime military environment an electronic subsystem such as shown in FIG. 1 would probably be fabricated on a small quantity basis for test, evaluation, and design evolution with quantities between 1 and 40 units being commonly produced. In addition to this relatively low production quantity, evolutionary changes such as, for example, changing of lens sizes or providing additional openings in the FIG. 1 chassis for new system integration connections are to be expected during the evolution. In view of this environment, a flexible chassis fabrication arrangement adaptable to, for example, an average 12-unit production quantity is desirable.
  • FIG. 2 of the drawings A cross-section view of a non-metallic structural material that is conveniently usable in such a low quantity and low noise environment for the FIG. 1 chassis is shown in FIG. 2 of the drawings.
  • the FIG. 2 cross-sectional view is taken along the cutting line 2--2 shown at 111 in FIG. 1.
  • the closable portion 100 of the FIG. 1 chassis is also presumed fabricated from the type of material indicated in FIG. 2 of the drawings.
  • a non-metallic or organic substrate is indicated at 200, this substrate is, for example, of sixty-thousandths (0.060) inch thickness and is covered on each side by a pair of metallic film layers 202, 204 and 206, 208.
  • metallic film layers 202, 204 and 206, 208 The considerations for selecting materials for these film layers are described in some detail below.
  • the weight saving realized by substituting a non-metallic material for aluminum alloys can vary, depending upon the design requirements for the chassis under consideration.
  • Advanced composite materials such as Kevlar® and graphite-reinforced composites offer greater weight savings than fiberglass reinforced epoxy (e.g., fiberglass cloth impregnated with epoxy resin), but at an increased cost, as shown in Table 3 and Table 4.
  • the composite materials offer better mechanical properties and substantial weight savings in comparison with metal, but are preferably used only in applications where increased performance is required and the increased cost can be justified.
  • the material Kevlar® in these tables is produced by E. I. duPont De Nemours Corporation (duPont) of Wilmington, Del., the name Kevlar® is a registered trademark of duPont.
  • the tooling cost illustrated in Table 4 is based on a typical moderate sized chassis for a ground-based radar subsystem. As is apparent from these costs, the injection molding and compression molding techniques are principally applicable to large volume production where the high cost of tooling can be amortized over large quantities such as 5,000 parts or more. In the usual military equipment development scenario, this quantity is not available and a small average lot size is common.
  • the pultrusion process referred to in Table 4 typically involves fabrication of structural members such as channels and angles from fiberglass mat and fiberglass roving using forming dies and a mandrel and employing a curing heat sequence wherein a continuous length of structural shape is formed.
  • the pultrusion process although attractive for electronic chassis parts construction, is generally found to involve loss of some physical dimensions; the angle of the orthogonal lip 132 in FIG. 1 is, for example, found difficult to control with the accuracy desired for achieving a good EMI/RFI seal with a mating part such as the cover 110 in the FIG. 1 structure.
  • Non-metallic structure EMI/RFI shielding can be categorized into three classes:
  • Arc or flame metal spray of metals such as zinc, aluminum and nickel.
  • Conductive organic coating such as paint with silver or nickel particles.
  • Ion plating of metals such as aluminum, copper and nickel.
  • Vacuum metallization of aluminum, copper or nickel Vacuum metallization of aluminum, copper or nickel.
  • Electro-deposition of copper or nickel or similar materials are Electro-deposition of copper or nickel or similar materials.
  • An arc or flame spray process requires detailed surface preparation, for good adhesion--by use of grit blast, plasma or chemical etch, or the use of base coat primer. This process often encounters problems of non-uniform thickness flaking, blistering, and warping of the plastic during the spraying or preparing processes.
  • EMI/RFI shielding in the range of 60 to 90 dB is, however, achievable with the arc or flame spray process coatings.
  • Non-uniformity in thickness and difficulty in establishing good electrical grounding are problems attending the application of organic conductive coatings such as paint filled with graphite, silver, copper or nickel.
  • Both ion plating and vacuum metallization techniques involve processing in a vacuum chamber with ion plating resulting in particle fusion to the plastic surface with greater adhesion than occurs in vacuum metallization. Both methods, however, produce only thin coatings having low shielding effectiveness and high susceptibility to mechanical abuse.
  • Electroless deposition for the nickel film and electroplating (electrolytic deposition) for the copper film when used in the company of a conditioned or etched plastic surface is found to be the most satisfactory of the possible laminate alternatives.
  • the preferred non-electrical deposition process for the present invention is proprietary to the Shipley company of 2300 Washington Street, Newton Mass. A 02162 and is identified as the Niposit® NL63 process. The name Niposit® is a registered trademark of the Shipley company.
  • Table 6 Several methods for conditioning the surface of a fiberglass epoxy structure to achieve optimum metal laminate adhesion during temperature cycling between -54° C. and +68° C. are shown in Table 6. Table 6 is based on one inch wide by four inch long samples.
  • the table 6 samples are also found to be capable of enduring temperature cycling without damage to the attachment of the electroplated finish. Specifically, blisters and separations between an electroplated finish and the epoxy fiber glass surface of the table 6 samples are absent after ten cycles of exposure to -55° C. for ten minutes, room temperature for five minutes, and 125° C. for fifteen minutes. Even better adhesion between an epoxy impregnated fiberglass substrate and electroplated copper and nickel films can be obtained through improved plating processes, as are known in the art.
  • Table 7 shown at the end of this specification, provides a comparison of the considered metallization processes for the present electronic chassis construction.
  • FIG. 5 measuring apparatus includes a radio frequency receiver 516 coupled to a radio frequency transmitter 518 through a sample 514 of the FIG. 2 material which may be square in shape and have, for example, dimensions of 60 cm on each side of the square.
  • the sample 514 is located in an aperture of a shielded room enclosure 508 which houses the source of test radio frequency energy.
  • the radio frequency energy is provided by a signal synthesizing generator 506 and an amplifier 504 which are coupled to a transmitting antenna 502.
  • the receiver 516 may comprise a spectrum analyzer 512 which is coupled through an attenuator 510 to a receiving antenna 500.
  • the antennas 500 and 502 in FIG. 5 may be varied according to the frequency and the type of radiation being considered, that is, a loop antenna is preferred for magnetic radiation and for electric field radiation at lower radio frequencies, while a dipole antenna or a dipole with companion elements is preferred at higher frequencies.
  • suitable antennas are known in the radio frequency transmitting and receiving art.
  • test panels used as samples at 514 in FIG. 5 are shown in Table 8 below.
  • Tables 11 and 12 are shown graphically in FIGS. 3 and 4 of the drawings.
  • the family of curves shown in FIG. 3 is plotted on a logarithmic scale of frequencies 300 falling between 10 kHZ and 1000 kHZ or 1 megacycle, the curves represent electric field strength attenuation across the aforementioned square sample of chassis material.
  • the attenuation measurements are plotted along a linear scale of logarithmic values 302.
  • curve number 3 relate the individual curves to the above-identified sample numbers; curve number 1 representing the aluminum sample, curve 2 the epoxy-fiberglass laminate with two layers of metallic film on each side, curve number 3 represents the epoxy-fiberglass laminate with no metallization, and curve number 4 represents the epoxy-fiberglass laminate with a CO-SHIELD 4914 nickel-filled paint, which is manufactured by Chomerics Inc. of 77 Dragon Court, Woburn Mass. 01888.
  • the curves of FIG. 4 show magnetic field attenuation versus frequency for the four identified test panels with the numbers 400, 402, 404, 406, 408 and 410 corresponding to the similar numbers in the 300 series in FIG. 3.
  • FIGS. 6 and 7 curves is the similar attenuation characteristics of fiberglass with double metal foil coatings on each surface to the characteristics of a solid aluminum test panel, that is, the curves 304 and 306 and 404 and 406 in FIGS. 3 and 4.
  • the similarity of these curves also extends into the higher frequency range than is represented by the FIGS. 3 and 4 drawings--as is shown in FIGS. 6 and 7 of the drawings.
  • FIGS. 6 and 7 the attenuation characteristics of smaller-sized test panels measuring 6 ⁇ 6 inches is shown.
  • the sample identities in FIGS. 6 and 7 correspond to those in FIGS. 3 and 4, with the 600 and 700 series numbers being used in lieu of the 300 and 400 series numbers in FIGS. 3 and 4.
  • the amount of energy which can be transmitted through a given hole size in the shielded room 508 accounts for the differences between data in FIG. 3 and FIG. 6 and FIG. 4 and FIG. 7, the smaller hole size permits less radio frequency energy to penetrate, however, the comparison of materials is yet valid.
  • each side of the substrate 200 is therefore preferably coated with a film of copper which is in turn coated by a film of nickel.
  • the film layers 204 and 202 may be regarded as the copper and nickel film layers for the exterior surface of the FIG. 1 closure member 110, and the film layers 206 and 208 as the copper and nickel film layers for the interior surfacer 124 of the closure member 110.
  • these films are deposited by the electroless process for the copper film and an electrolytic or electroplating deposition for the nickel film.
  • a thin coating of electroless nickel applied to the substrate 200 prior to deposition of the copper layers 204 and 206 improves the adhesion of the copper film layers.
  • Such a coating is represented by the layer 210 in FIG. 2; this adhesion promoting layer 210 is shown to be of lesser thickness than are the previously described or primary film layers 202, 204, 206 and 208 in FIG. 2 in keeping with its thin coating nature.
  • the outer, thicker, film of nickel serves as a hard abrasive resistant external surface to protect the soft copper film beneath it.
  • Metal film layer coatings over one surface of a chassis structure is a viable shielding arrangement; however coating both the inside and outside surfaces of a chassis (e.g., surfaces 126 and 127 in FIG. 1) with such metal films, in addition to providing desirable double shielding, also eliminates the costly process of masking the completed chassis for areas not to be coated. Double coatings also afford double protection against damage to one surface which could result in intense local EMI/RFI leakage in the absence of a second or backup coating.
  • top, bottom and side members 102, 104 106, 108, 112 and 114 in FIG. 1 are also preferably coated with the copper and nickel films.
  • a molded-in-place EMI/RFI gasket can be used as an effective seal between the portions 100 and 110 of the FIG. 1 chassis.
  • Other types of seals such as wire mesh gaskets, metal filled elastomers, carbon-filled materials, and honeycomb-core materials enabling ventilatlon also provide adequate seals for the chassis in FIG. 1.
  • FIG. 8 A flow diagram for a process for making the EMI/RFI shielding non-metallic substrate chassis of the present invention is shown in FIG. 8 of the drawings.
  • the chassis structure and its bosses or appendages or holes for supporting electronic parts is formed in blocks 800, 802, and 804; molds, skeleton frames or similar pliable cloth supporting arrangements may be used in these steps.
  • the ossifying step at block 806 in FIG. 8 represents the impregnating of the fiberglass cloth with epoxy resin and the subsequent epoxy curing; a plurality of impregnating and curing steps may be desired.
  • Preparation of the chassis surfaces for the desired two film coatings is achieved at blocks 808 and 810 in FIG. 8, the preparation including physical abrasion and/or etching with chemical reagents, as is known in the art, and the electroless deposition of a thin, adhesion promoting, nickel film, an optional step as is indicated by the bypass line 816.
  • Deposition of the desired shielding and protective films is achieved in blocks 812 and 814; copper and nickel being the preferred films, as indicated.
  • the combination of copper and nickel film layers using the electroplating process provides the following desirable characteristics for the FIG. 1 and FIG. 2 structure.
  • the nickel exterior film provides abrasion and environmental resistance to protect the copper-plated surface.
  • a continuous coating is provided over all of the surfaces, including seams, thereby eliminating leaks of EMI/RFI.
  • the surface is relatively smooth and can be marked or painted easily.
  • the preferred arrangement for the non-metallic substrate chassis involves a formed substrate of fiberglass impregnated with epoxy and plated metallic layers on each slde of the chassis surface, the plated layers preferably extend around corners and edges of the chassis to preclude radio frequency energy leakage and the plated metallic layers also extend through the depth of holes and apertures in the fiberglass structure to both minimize leakage at these points and to provide conducting paths between the plated films on each surface of the fiberglass substrate.
  • nickel is preferred for the chassis outermost film layer, a layer of rhodium can with little doubt be substituted for the nickel layer with only small performance change while yet maintaining reasonable chassis cost.
  • Other alternate metals such as gold and cobalt, while being of good electrical and mechanical properties, would increase the chassis cost unduly.
  • the nickel on copper plating system described above and applied on both the inside and outside surfaces of a chassis is found to provide EMI shielding equal to that afforded by solid alumium; this plating system promises to overcome a significant obstacle in the use of plastics for chassis.
  • the preferred fiberglass and metal film chassis is capable of achieving a weight savings of up to 30%; this is especially useful in the case of electronic systems intended for use in aircraft or spacecraft but is also desirable in reducing the mass of ground-based equipment.

Abstract

An electronic equipment chassis structure using non-metallic plastic material such as epoxy-impregnated fiberglass together with layers of shielding metal film, preferably of copper overlaid by nickel. Desirable radio frequency shielding is achieved in comparison with the metal chassis structures and in the presence of decreased chassis mass, lower fabrication cost and chassis change enabling flexibility. Examples of material characteristics, representative fabrication costs, and attained radio frequency attenuation properties are included.

Description

RIGHTS OF THE GOVERNMENT
The invention described herein may be manufactured and used by or for the Government of the United States for all governmental purposes without the payment of any royalty.
This application is a continuation of application Ser. No. 705,834, filed Feb. 26, 1985, now abandoned.
BACKGROUND OF THE INVENTION
This invention relates to the field of laminate structures and to a class of such structures used for both mechanical support and electromagnetic radiation shielding in electronic apparatus.
Organic material structures are increasingly selected for fabricating the chassis, cabinets, enclosures, racks, cases and bases employed in modern military and commercial electronic equipment. Herein such structures are collectively called chassis or enclosures with the terms chassis and enclosure being used interchangeably. A large incentive in the movement to organic material structures for military electronic equipment stems from the present peacetime environment for military development wherein small production runs and frequent design changes are major development considerations. The absence of standardized shapes and dimensions for the variety of electronic systems purchased by government agencies together with the small number of large quantity production runs available have also contributed to the need for flexible and low-cost structures.
Metallic materials especially aluminum sheet metal, have previously been used in ground-based and airborne electronic equipment structures and doubtless will continue to be favored for many such applications. Aluminum sheet metal in thicknesses of 0.062 inch, 0.092 inch, 0.125 inch, and 0.188 inch are particularly popular in constructing such present-day military electronic equipment. Increasingly, however, the flexibility, weight considerations, and other desirable properties of non-metallic materials such as fiberglass-reinforced with an epoxy impregnant are desirable for electronic systems. With the advent of integrated circuit electronics, for example, the need for the structural strength of metallic enclosures and has decreased while the pressure for small size, conformable physical shape, light weight low cost, and predictable reliability have remained present and increasing in intensity.
In the realm of non ground-based equipment, the electronic systems designed for spacecraft or modern high-performance aircraft are particularly demanding examples of the high quality, performance-driven electronic system having unique enclosure requirements which are often best met by non-metallic or organic materials. Less notable, but nevertheless important examples of a trend away from the automatic use of metallic structural elements in electronic apparatus are to be found in consumer and automotive electronic equipment where present-day practice is to incorporate plastic materials for all but the most severely stressed mechanical components of an electronic chassis. Present-day television receivers, for example, employ cabinets, printed circuit boards, supporting structures, and even carrying handles fabricated from organic plastic materials and rely on metal fittings only in, for example, mounting the cathode ray tube, and in some cases, for a skeleton framework.
Despite the desirability of plastic and organic structures used in these applications, there remains a need for electromagnetic shielding both between portions of a given circuit and for containment or exclusion of electromagnetic fields. Such fields affect the performance of nearby electronic apparatus, cause undesirable exposure of living organisms to electromagnetic radiation, and contribute to the military detectability of an electronic apparatus. The term "interference active" or "active" is used herein to generically describe electronic equipment which may be either sensitive to externally-sourced electromagnetic radiation or act as a source of electromagnetic radiation that is undesirable and in need of confinement--that is to represent both EMI/RFI receivers and transmitters. EMI is, of course, an abbreviation for electromagnetic interference and RFI designates radio frequency interference. In either the electromagnetic radiation receiver or transmitter case, the electromagnetic radiation can be of the electric field (E field) or magnetic field (H field) type, or a combination of E and H fields.
Accompanying the need for electromagnetic shielding, particularly in high-performance and rugged electronic equipment of the type designed for military use, is the need for heat conduction from the electronic components of a system, and heat dissipation to the surrounding environment, together with a need for large and highly electrically conductive ground planes which serve to establish a zero electrical signal reference point in most systems.
An organic layer and metal film layer laminate composition is found desirable for meeting these needs in many electronic systems. In the case of ground-based radar and similar high-frequency electronic equipment, the properties of electrical conductivity and magnetic shielding are found to be particularly determinative of the materials used in such laminate structures.
The patent art includes several examples of laminate structures used in electronic equipment. This art includes the patent of Leonard J Costanza U.S. Pat. No. 3,806,928, which concerns a laminated sandwich joint structure for honeycomb sections subjected to radiation at radar frequencies. The Costanza patent is concerned with maintaining the electrical continuity between large multi-layer sections of objects such as a jet engine air intake diffuser where it is desirable to maintain the electrical properties of the structure without abrupt changes resulting from the presence of physical joints. The structure of the Costanza patent includes epoxy-impregnated fabric layers with some of the fabric material being impregnated by conductive carbon such as acetylene black or furnace black, and with the fabric layers being comprised of woven fiberglass filaments. The goal of the Costanza patent is actually to achieve minimum discontinuities in the electrical properties of the connected honeycomb sections in order that radar reflections from the assembled structure are minimized. Conversely, the Costanza arrangement is also useful in constructing radar-transparent honeycomb structures for use in situations where minimum attenuation of a radar signal is desirable, as in a radome for example.
Another example of laminate materials having useful electromagnetic properties is found in the patent of Dale M. Grimes et al, U.S. Pat. No. 3,938,152, which concerns a multi-layer structure useful in absorbing and minimizing reflections of electromagnetic radiation of preselected radar wavelengths. The Grimes et al patent contemplates the use of a ferrimagnetic film which is composed of nickel oxide, zinc oxide, and ferric oxide, or alternately of mixed crystal ferrites which are compounds of cadmium, iron, and lithium. Alternately, the Grimes patent teaches the use of hexagonal ferrites which include zinc, barium, iron and oxygen. In the Grimes structure these compositions serve as signal attenuators and are applied over a highly-conductive planar backing member.
Another example of a radar signal attenuating laminate structure is found in the patent of Otto Halpern, U.S. Pat. No. 3,007,160, which concerns a laminate film structure wherein electrical resonance is achieved in the outermost film layer. This layer is also made to be electrically lossy and incorporates copper flakes or similar dispersed conductive material. The Halpern structure contemplates the use of an adhesive layer between the resonating--absorbing layer and a metallic reflecting layer.
Yet another multi-layer electromagnetic field attenuating structure is shown in the patent of Harold Adkins, U.S. Pat. No. 4,408,255, which is concerned with an electromagnetic interference (EMI) radiation shield that is useful in such equipment as electronic data processing machines. The Adkins patent considers both the electrical or E field and the magnetic or H field components of radio frequency intereference originating in data processing circuitry. The Adkins patent contemplates the combination of a magnetically permeable material with a sheet of conductive material bonded on one side thereof. The absorptive material in the Adkins shield structure may comprise steel wool, carbon-impregnated rubber, ferrite in a plastic-stranded carrier, or some combination of similar lossy materials; the conductive material layer is comprised of conductor having sheet resistivity preferably in the range of 1.5×10-6 to 100×10-6 ohm-cm.
Yet another radio frequency shielding arrangement is shown in the patent of William A. Manly, U.S. Pat. No. 4,371,742, which discloses an absorptive shield for transmission lines. The shield of the Manly patent is composed of flexible materials filled with ferromagnetic or ferrimagnetic powders of selected particle size and distribution; the particles used may include varieties of iron, nickel, and cobalt. The absorptive magnetic material of the Manly patent is also shown configured into objects such as an enclosure for electronic equipment.
SUMMARY OF THE INVENTION
An object of the present invention is to provide an electronic chassis structure which is largely non-metallic in composition,
Another object of the invention is to provide a structural composition useful in the fabrication of electronic apparatus having need for an alternate to conventional metal fabrication, together with the need for electromagnetic shielding requirements.
Another object of the invention is to provide a desirable combination of metallic films for use in non-metallic electronic structural members.
Another object of the invention is to provide an electronic chassis structure which combines a non-metallic substrate with a multi-layer double surface metal film shielding arrangement.
These and other objects are achieved by providing a chassis for use with radio frequency electromagnetic interference active electronic apparatus that includes an organic material substrate member configured as a closable geometric shape having a plurality of angularly disposed connected-together surface portions and a closure means for closing the substrate member, with the closure means including a closure surface portion. The chassis includes arrangements located on the surface portions for mounting components of the electronic apparatus, plus a multi-layered electromagnetic radiation energy shielding and physical protection coating located on a plurality of the surface portions, the coating further including a first metallic film layer disposed over both faces of the surface portions in intimate physical contact therewith, a second metallic film layer disposed over the first film layer of the surface portions in physical contact with the first film layer and wherein the first and second metallic films are composed of different metals at least one of which is a good electrical conductor.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is an electronic chassis or enclosure in accordance with the present invention together with a representative electronic hardware system.
FIG. 2 is an enlarged cross-sectional view of the FIG. 1 chassis taken along the cutting line 2--2 in FIG. 1.
FIG. 3 shows the relationship between shielding effectiveness and frequency for the material used in the FIG. 1 and FIG. 2 structure when subjected to electric fields of varying frequency.
FIG. 4 shows the relationship between shielding effectiveness and frequency for the material used in the FIG. 1 and FIG. 2 structure when subjected to magnetic fields of varying frequency.
FIG. 5 shows the test arrangement for measuring shielding effectiveness.
FIG. 6 shows the relationship between electric field shielding effectiveness and frequency using a different frequency scale and different test panel size.
FIG. 7 shows the relationship between magnetic field shielding effectiveness and frequency using a different frequency scale and different test panel size.
FIG. 8 is a flow diagram for fabricating a chassis of the present type.
DETAILED DESCRIPTION
In FIG. 1 of the drawings there is shown an exploded view of a typical electronic chassis or enclosure which may be fabricated according to the present invention. The FIG. 1 chassis includes a closable or main portion 100 having top and bottom ends 102 and 104 and fixed sides 106 and 108 which meet the ends 102 and 104 in substantially right angles. The FIG. 1 chassis also includes a cover or closure member 110 which is also formed in the shape of a right angle and is arranged to mate with the open sides of the main portion 100. The cover or closure member 110 includes a pair of sides 112 and 114 and also includes a pair of integrally connected internal shield members 116 and 118 which surround a portion of the enclosed electronic apparatus when the cover 110 is fixed in place on the chassis main portion 100.
The cover 110 in FIG. 1 further includes a window member 122 and window housing 120, which serve to admit light from an examined scene to the electro-optical apparatus enclosed by the FIG. 1 chassis. The cover 110 is arranged to accommodate a plurality of fastening members 128 which may be in the form of machine screws or spring engaging fasteners of the type known in the fastening art. The fastening members 128 cooperate with mating portions 130 located in an orthogonal lip 132 surrounding the opening of the chassis closable main portion 100 in FIG. 1.
A plurality of printed circuit boards indicated generally at 138, 140, and 142 are shown mounted in the closable portion of the FIG. 1 chassis by way of machine screws or the like 156 which may engage the respective side and end portions of the FIG. 1 chassis by way of holes, standoff supports and nuts, or alternately and preferably, by way of attached bosses integral with and extended inward from the inner surface of the fixed sides and bottom of the FIG. 1 chassis.
Mounted on the printed circuit board 140 is a representation of an electro-optic scanner 143, an apparatus typical of the small signal, electromagnetic radiation sensitive equipment which might be mounted in a FIG. 1 type chassis. Other such radiation sensitive equipment might include radio frequency receivers, ionized particle detectors and the sense amplifiers used in EDP systems. Alternately, a chassis of the FIG. 1 type might also be useful for enclosing an apparatus such as an oscillator which tends to generate strong electromagnetic fields capable of disrupting adjacent electronic circuits or providing undesirable detectability if allowed to escape from the chassis.
The electro-optic scanner apparatus 143 generally includes lenses 144, 146 and 148, an optical signal to electrical signal transducing retina 150, a plurality of integrated circuit packages 152 which may comprise, for example, a RAM memory and a plurality of discrete transistors 154.
As indicated above, the internal shield members 116 and 118 surround the electro-optic scanner apparatus 143 when the cover 110 is placed in mating position with the closable portion of the FIG. 1 chassis, such shielding preventing the coupling of strong signals from the integrated circuits 152 and the transistors 154, for example, into the low-level circuitry of the retina 150 and the preamplifiers associated therewith. The construction of the bottom and side members 104, 106, 108, 112, and 114 is also arranged to minimize the coupling of externally-sourced electromagnetic radiation to the low-level circuitry of the scanner 143.
The scanner and electronic circuitry shown in FIG. 1 may, for example, be a part of an electronic imaging apparatus intended for mounting in an aircraft or spacecraft for the purpose of transmitting signals representing viewed images to a remote location; the scanner 143 therefore could comprise a portion of an overall system and could be the computer-controlled generator of modulating signals for a radio frequency transmitter which is not shown. The radio frequency electric and magnetic fields from such as transmitter would, however, require exclusion from the low-level circuitry of the retina 150 thereby necessitating use of shielding construction in the FIG. 1 apparatus and in the radio frequency circuitry housing.
In the present peacetime military environment an electronic subsystem such as shown in FIG. 1 would probably be fabricated on a small quantity basis for test, evaluation, and design evolution with quantities between 1 and 40 units being commonly produced. In addition to this relatively low production quantity, evolutionary changes such as, for example, changing of lens sizes or providing additional openings in the FIG. 1 chassis for new system integration connections are to be expected during the evolution. In view of this environment, a flexible chassis fabrication arrangement adaptable to, for example, an average 12-unit production quantity is desirable.
A cross-section view of a non-metallic structural material that is conveniently usable in such a low quantity and low noise environment for the FIG. 1 chassis is shown in FIG. 2 of the drawings. The FIG. 2 cross-sectional view is taken along the cutting line 2--2 shown at 111 in FIG. 1. The closable portion 100 of the FIG. 1 chassis is also presumed fabricated from the type of material indicated in FIG. 2 of the drawings.
In FIG. 2, a non-metallic or organic substrate is indicated at 200, this substrate is, for example, of sixty-thousandths (0.060) inch thickness and is covered on each side by a pair of metallic film layers 202, 204 and 206, 208. The considerations for selecting materials for these film layers are described in some detail below.
With respect to the substrate member 200 in FIG. 2, four of the considerations in selecting among several candidate constructions for such members are described in the data of Table 1-Table 4 below; aluminum is shown as a reference in these tables.
              TABLE 1                                                     
______________________________________                                    
                TENSILE STRENGTH (PSI)                                    
MATERIAL          Longitudinal                                            
                              Transverse                                  
______________________________________                                    
Aluminum QQ-A-250/8                                                       
                  31,000-38,000                                           
Fiber Glass Reinforced Epoxy                                              
                  40,000      35,000                                      
G-10, G-11, FR4 (ASTM-229)                                                
Kevlar ® Reinforced Epoxy                                             
                  72,000                                                  
Graphite Composite                                                        
                  81,000      84,000                                      
Polyglass (™) Pultruded                                                
                  30,000      15,000                                      
______________________________________                                    

              TABLE 2                                                     
______________________________________                                    
               DENSITY                                                    
MATERIAL         grams/cm3 pounds/m3                                      
______________________________________                                    
Aluminum Alloys  2.768     0.1                                            
Epoxy/Fiber Glass                                                         
                 1.799     0.065                                          
Epoxy/Fiber Glass                                                         
                 1.716     0.062                                          
(Pultruded)                                                               
Kevlar ® Composite                                                    
                 1.245     0.045                                          
Graphite Composite                                                        
                 1.605     0.058                                          
______________________________________                                    

              TABLE 3                                                     
______________________________________                                    
                     COST                                                 
MATERIAL             PER POUND, $                                         
______________________________________                                    
Fiber Glass Reinforced Epoxy Composite                                    
                     8.30                                                 
7781 Glass Cloth, Mil-R-300, Ty I, Resin                                  
Epoxy Composite      42.00                                                
281 Style Kevlar ® 49                                                 
Graphite-Epoxy Composite                                                  
                     100.00                                               
HM Woven Graphite                                                         
Aluminum Alloy, 6061-T6                                                   
                     2.00                                                 
______________________________________                                    

              TABLE 4                                                     
______________________________________                                    
FABRICATION PROCESS  TOOLING COST, $                                      
______________________________________                                    
Injection Molding (Structural Foam)                                       
                     131,500                                              
Injection Molding (BMC)                                                   
                     32,899                                               
Compression Molding (SMC)                                                 
                     17,000                                               
Pultrusion           13,000                                               
Hand Layup           12,000                                               
Metal (Aluminum) Construction                                             
                      5,200                                               
______________________________________
As illustrated by Table 1 above, the weight saving realized by substituting a non-metallic material for aluminum alloys can vary, depending upon the design requirements for the chassis under consideration. Advanced composite materials such as Kevlar® and graphite-reinforced composites offer greater weight savings than fiberglass reinforced epoxy (e.g., fiberglass cloth impregnated with epoxy resin), but at an increased cost, as shown in Table 3 and Table 4. The composite materials offer better mechanical properties and substantial weight savings in comparison with metal, but are preferably used only in applications where increased performance is required and the increased cost can be justified. The material Kevlar® in these tables is produced by E. I. duPont De Nemours Corporation (duPont) of Wilmington, Del., the name Kevlar® is a registered trademark of duPont.
The tooling cost illustrated in Table 4 is based on a typical moderate sized chassis for a ground-based radar subsystem. As is apparent from these costs, the injection molding and compression molding techniques are principally applicable to large volume production where the high cost of tooling can be amortized over large quantities such as 5,000 parts or more. In the usual military equipment development scenario, this quantity is not available and a small average lot size is common.
The pultrusion process referred to in Table 4 typically involves fabrication of structural members such as channels and angles from fiberglass mat and fiberglass roving using forming dies and a mandrel and employing a curing heat sequence wherein a continuous length of structural shape is formed. The pultrusion process, although attractive for electronic chassis parts construction, is generally found to involve loss of some physical dimensions; the angle of the orthogonal lip 132 in FIG. 1 is, for example, found difficult to control with the accuracy desired for achieving a good EMI/RFI seal with a mating part such as the cover 110 in the FIG. 1 structure.
The tooling costs to mold the typical chassis of Table 4 above by the hand layup method are shown to be lower than any of the other types of molding considered. In addition to a molding tool, only simple tools such as a drill and trim cutter are necessary, and the method is applicable to small quantities of parts. This method is therefore applicable to a variety of requirements and needs only soft tooling instead of expensive hard tooling.
The cost to manufacture several different quantities of the typical cbassis referred to in Table 4 by the several indicated methods and excluding a cover of the type 110 in FIG. 1 are shown in Table 5 below.
              TABLE 5                                                     
______________________________________                                    
     Sheet                                Pultru-                         
     Metal                         Injec  sion                            
     Fab     Injec-                tion   from                            
Units                                                                     
     Alum-   tion     Com-  Hand   (Struct                                
                                          Channels                        
Mfd. inum    (BMC)    pression                                            
                            Layup  Foam)  & Angles                        
______________________________________                                    
 1   $6,236  $33,255  $22,940                                             
                            $12,551                                       
                                   $135,913                               
                                          $14,495                         
10   1,107   3,696    2,806 1,751  13,770 1,882                           
12   920     3,098    2,434 1,551  11,508 1,649                           
25   669     1,673    1,464 1,031  5,627  1,042                           
50   553     1,015    1,017 791    2,912  7,610                           
100  495     686      793   617    1,555  621                             
______________________________________                                    
 Cover and metallization costs are not included.
For the small quantity, lightweight configuration chassis, the choice of an epoxy-impregnated fiberglass construction is reasonable. Such a structure is therefore the preferred embodiment for the substrate 200 in FIG. 2. Since a material of this type inherently lacks EMI/RFI shielding capability and the amount of shielding required in an electronic chassis can range from a shielding effectiveness of 30 dB up to 80 dB and beyond, consideration of suitable shielding arrangements in combination with the substrate material is warranted.
Non-metallic structure EMI/RFI shielding can be categorized into three classes:
1. Intrinsically Conductive Copolymers.
This is an emerging class of materials involving the doping of a plastic raw material with a doping gas in order to achieve a surface resistivity on the order of 10 ohms per square. Chemical stability of the doped plastic material is a subject of continuing state of the art development.
2. Molded Plastics Containing Metal Fillers.
Variously sized aluminum flakes, copper powder, stainless steel wire, and conductive carbon provide shielding in such arrangements--along with the sacrifice of mechanical properties such as impact strength. Expensive tooling is generally required for such structures in order that uniform distribution of the conductive additives be achieved. Both metal fillers and metallized fabrics make the establishment of a low resistance electrical chassis ground somewhat difficult.
3. Surface Metallized Molded Plastic Parts Including Metallization By:
Arc or flame metal spray of metals such as zinc, aluminum and nickel.
Foil or film aluminum adhesively bonded to a plastic substrate.
Conductive organic coating such as paint with silver or nickel particles.
Ion plating of metals such as aluminum, copper and nickel.
Vacuum metallization of aluminum, copper or nickel.
Electro-deposition of copper or nickel or similar materials.
Electroplating of copper, nickel, tin.
An arc or flame spray process requires detailed surface preparation, for good adhesion--by use of grit blast, plasma or chemical etch, or the use of base coat primer. This process often encounters problems of non-uniform thickness flaking, blistering, and warping of the plastic during the spraying or preparing processes. EMI/RFI shielding in the range of 60 to 90 dB is, however, achievable with the arc or flame spray process coatings.
The complex shape of many electronic chassis severely limits the use of film and foil metallizations. Such shielding arrangements also necessitate the use of a conductive adhesive or sealer at the seams of the shielding material.
Non-uniformity in thickness and difficulty in establishing good electrical grounding are problems attending the application of organic conductive coatings such as paint filled with graphite, silver, copper or nickel.
Both ion plating and vacuum metallization techniques involve processing in a vacuum chamber with ion plating resulting in particle fusion to the plastic surface with greater adhesion than occurs in vacuum metallization. Both methods, however, produce only thin coatings having low shielding effectiveness and high susceptibility to mechanical abuse.
Electroless deposition for the nickel film and electroplating (electrolytic deposition) for the copper film when used in the company of a conditioned or etched plastic surface is found to be the most satisfactory of the possible laminate alternatives. The preferred non-electrical deposition process for the present invention is proprietary to the Shipley company of 2300 Washington Street, Newton Mass. A 02162 and is identified as the Niposit® NL63 process. The name Niposit® is a registered trademark of the Shipley company.
Several methods for conditioning the surface of a fiberglass epoxy structure to achieve optimum metal laminate adhesion during temperature cycling between -54° C. and +68° C. are shown in Table 6. Table 6 is based on one inch wide by four inch long samples.
              TABLE 6                                                     
______________________________________                                    
Sample No.                                                                
         Surface Preparation                                              
                           Peel Strength, psi                             
______________________________________                                    
1        Not Treated       8.75-9.0                                       
2        Vapor Degreased with                                             
                            7.0-8.2                                       
         Chlorothane Vapor                                                
3        Abraded With Scotch Brite                                        
                           Plating not                                    
         Pad & Vapor Degreased                                            
                           Peelable (Brittle)                             
4        Vapor Honed & Vapor                                              
                           Plating not                                    
         Degreased         Peelable (Brittle)                             
5        Plasma Cleaned    0.25-1.0                                       
6        Chromic/Sulfuric Acid                                            
                            8.5-9.0                                       
         Etched at 160° F. for                                     
         5 Minutes                                                        
______________________________________                                    
 Peel strength is measured after thermal cycling.
The table 6 samples are also found to be capable of enduring temperature cycling without damage to the attachment of the electroplated finish. Specifically, blisters and separations between an electroplated finish and the epoxy fiber glass surface of the table 6 samples are absent after ten cycles of exposure to -55° C. for ten minutes, room temperature for five minutes, and 125° C. for fifteen minutes. Even better adhesion between an epoxy impregnated fiberglass substrate and electroplated copper and nickel films can be obtained through improved plating processes, as are known in the art.
Table 7, shown at the end of this specification, provides a comparison of the considered metallization processes for the present electronic chassis construction.
An apparatus for measuring the shielding effectiveness of several different coatings for the substrate material 200 in FIG. 2 is shown in FIG. 5 of the drawings. The FIG. 5 measuring apparatus includes a radio frequency receiver 516 coupled to a radio frequency transmitter 518 through a sample 514 of the FIG. 2 material which may be square in shape and have, for example, dimensions of 60 cm on each side of the square. The sample 514 is located in an aperture of a shielded room enclosure 508 which houses the source of test radio frequency energy. The radio frequency energy is provided by a signal synthesizing generator 506 and an amplifier 504 which are coupled to a transmitting antenna 502. In a similar fashion the receiver 516 may comprise a spectrum analyzer 512 which is coupled through an attenuator 510 to a receiving antenna 500. The antennas 500 and 502 in FIG. 5 may be varied according to the frequency and the type of radiation being considered, that is, a loop antenna is preferred for magnetic radiation and for electric field radiation at lower radio frequencies, while a dipole antenna or a dipole with companion elements is preferred at higher frequencies. Generally, suitable antennas are known in the radio frequency transmitting and receiving art.
The configuration of four test panels used as samples at 514 in FIG. 5 are shown in Table 8 below.
              TABLE 8                                                     
______________________________________                                    
Panel #1 -                                                                
        Aluminum QQ-A-250/8 H32 0.16-cm (0.062-inch) thick.               
Panel #2 -                                                                
        G-10 epoxy fiber glass laminate 0.16-cm (0.062-inch)              
        thick with 0.003-cm (0.001-inch) of electroplated                 
        copper plus 0.003-cm (0.001-inch) of nickel on both               
        sides.                                                            
Panel #3 -                                                                
        G-10 epoxy fiber glass laminate 0.16-cm (0.062-inch)              
        thick laminate with no metallization.                             
Panel #4 -                                                                
        G-10 epoxy fiber glass laminate 0.16-cm (0.062-inch)              
        thick with CHO-SHIELD 4914, a nickel filled paint,                
        0.009-cm (0.0035-inch) thick on one side.                         
______________________________________
Electric and magnetic field strength measurements for the four different test panels are shown in Tables 9 and 10 herein, and normalizations of the results from these tables are shown in Tables 11 and 12.
              TABLE 9                                                     
______________________________________                                    
      Trans-                                                              
      mitter &                                                            
      Receiver                                                            
Freq  Dist.    Panel Number and db Attenuation                            
kHZ   in Inches                                                           
               Open     #1    #2     #3    #4                             
______________________________________                                    
 10   6        -69.9    -110.4                                            
                              -112.2 -77.5 -94.0                          
 50   6        -38.5    -121.8                                            
                              -123.3 -41.1 -95.6                          
100   6        -26.4    -121.3                                            
                              -123.0 -29.1 -98.2                          
500   17       -0.70    -118.0                                            
                              -109.9  -3.6 -68.0                          
1000  17       -25.8    -125.0                                            
                              -115.7 -29.0 -80.9                          
______________________________________                                    
 NOTE: Measurements were made using a 41inch rod antenna and a +23 dB CW  
 signal generator.                                                        

              TABLE 10                                                    
______________________________________                                    
      CW Signal                                                           
Freq  Generator Panel Number and Attenuation in db                        
kHZ   Level, dB Open    #1    #2    #3    #4                              
______________________________________                                    
 10   -30       -81.6   -109.8                                            
                              -101.7                                      
                                    -85.7 -85.5                           
 50   -30       -86.1   -119.5                                            
                              -116.2                                      
                                    -89.5 -89.8                           
100   -20       -81.4   -117.9                                            
                              -116.6                                      
                                    -85.0 -85.1                           
500   +10       -65.4   -113.0                                            
                              -112.2                                      
                                    -68.8 -69.3                           
1000  +15       -66.8   -117.1                                            
                              -117.5                                      
                                    -70.0 -71.7                           
______________________________________                                    
 NOTE: Measurements were made using transmitter and receiver distances of 
 one inch and a model ALP10 loop antenna which is available from Fairchild
 Electrometrics Inc. of 100 Church Street, Amsterdam NY.                  

              TABLE 11                                                    
______________________________________                                    
      Transmitter &                                                       
Freq  Receiver Dist                                                       
                 Panel Number and Attenuation in db                       
kHZ   Inches     Open    #1    #2     #3   #4                             
______________________________________                                    
 10   6          --      40.5  42.3   7.6  24.1                           
 50   6          --      83.3  84.8   2.6  57.1                           
100   6          --      94.9  96.6   2.7  71.8                           
500   17         --      117.3 109.2  2.9  67.3                           
1000  17         --      99.2  89.9   3.2  55.1                           
______________________________________                                    
 NOTE: Measurements here include a 41inch rod antenna and a +23 dB CW     
 signal generator.                                                        

              TABLE 12                                                    
______________________________________                                    
      CW Signal                                                           
Freq  Generator Panel Number and Attenuation in db                        
kHZ   Level, dB Open     #1    #2     #3   #4                             
______________________________________                                    
 10   -30       --       28.2  20.1   4.1  3.9                            
 50   -30       --       33.4  30.1   3.4  3.7                            
100   -20       --       36.5  35.2   3.6  3.7                            
500   +10       --       47.6  46.8   3.4  3.9                            
1000  +15       --       50.3  50.7   3.2  4.9                            
______________________________________                                    
 NOTE: Measurements were made using transmitter and receiver distances of 
 one inch and a Fairchild ALP10 loop antenna.
The results of Tables 11 and 12 are shown graphically in FIGS. 3 and 4 of the drawings. The family of curves shown in FIG. 3 is plotted on a logarithmic scale of frequencies 300 falling between 10 kHZ and 1000 kHZ or 1 megacycle, the curves represent electric field strength attenuation across the aforementioned square sample of chassis material. The attenuation measurements are plotted along a linear scale of logarithmic values 302. The identifying numbers 312 in FIG. 3 relate the individual curves to the above-identified sample numbers; curve number 1 representing the aluminum sample, curve 2 the epoxy-fiberglass laminate with two layers of metallic film on each side, curve number 3 represents the epoxy-fiberglass laminate with no metallization, and curve number 4 represents the epoxy-fiberglass laminate with a CO-SHIELD 4914 nickel-filled paint, which is manufactured by Chomerics Inc. of 77 Dragon Court, Woburn Mass. 01888. The curves of FIG. 4 show magnetic field attenuation versus frequency for the four identified test panels with the numbers 400, 402, 404, 406, 408 and 410 corresponding to the similar numbers in the 300 series in FIG. 3. One of the main points to be observed in the FIG. 3 and FIG. 4 curves is the similar attenuation characteristics of fiberglass with double metal foil coatings on each surface to the characteristics of a solid aluminum test panel, that is, the curves 304 and 306 and 404 and 406 in FIGS. 3 and 4. The similarity of these curves also extends into the higher frequency range than is represented by the FIGS. 3 and 4 drawings--as is shown in FIGS. 6 and 7 of the drawings. In FIGS. 6 and 7, the attenuation characteristics of smaller-sized test panels measuring 6×6 inches is shown. The sample identities in FIGS. 6 and 7 correspond to those in FIGS. 3 and 4, with the 600 and 700 series numbers being used in lieu of the 300 and 400 series numbers in FIGS. 3 and 4. The amount of energy which can be transmitted through a given hole size in the shielded room 508 accounts for the differences between data in FIG. 3 and FIG. 6 and FIG. 4 and FIG. 7, the smaller hole size permits less radio frequency energy to penetrate, however, the comparison of materials is yet valid.
These Table 11 and 12 and FIGS. 3 and 4 results indicate the favorable capability of coatings of copper and nickel for use respectively at 204, 202 and 206, 208 in FIG. 2. Each side of the substrate 200 is therefore preferably coated with a film of copper which is in turn coated by a film of nickel. In FIG. 2, the film layers 204 and 202 may be regarded as the copper and nickel film layers for the exterior surface of the FIG. 1 closure member 110, and the film layers 206 and 208 as the copper and nickel film layers for the interior surfacer 124 of the closure member 110. Preferably these films are deposited by the electroless process for the copper film and an electrolytic or electroplating deposition for the nickel film.
It is also found that a thin coating of electroless nickel applied to the substrate 200 prior to deposition of the copper layers 204 and 206 improves the adhesion of the copper film layers. Such a coating is represented by the layer 210 in FIG. 2; this adhesion promoting layer 210 is shown to be of lesser thickness than are the previously described or primary film layers 202, 204, 206 and 208 in FIG. 2 in keeping with its thin coating nature.
In the preferred film arrangement, the outer, thicker, film of nickel serves as a hard abrasive resistant external surface to protect the soft copper film beneath it. Metal film layer coatings over one surface of a chassis structure is a viable shielding arrangement; however coating both the inside and outside surfaces of a chassis (e.g., surfaces 126 and 127 in FIG. 1) with such metal films, in addition to providing desirable double shielding, also eliminates the costly process of masking the completed chassis for areas not to be coated. Double coatings also afford double protection against damage to one surface which could result in intense local EMI/RFI leakage in the absence of a second or backup coating. The interior surfaces 124, 126, 134 and 136 of the closable chassis portion 100 and the cover portion 110 in FIG. 1 are therefore preferably coated with the film of copper overlaid by a film of nickel as described in FIG. 2. In a similar fashion, the exterior surfaces of the top, bottom and side members 102, 104 106, 108, 112 and 114 in FIG. 1 are also preferably coated with the copper and nickel films.
Although not shown in the FIG. 1 drawing, a molded-in-place EMI/RFI gasket can be used as an effective seal between the portions 100 and 110 of the FIG. 1 chassis. Other types of seals such as wire mesh gaskets, metal filled elastomers, carbon-filled materials, and honeycomb-core materials enabling ventilatlon also provide adequate seals for the chassis in FIG. 1.
A flow diagram for a process for making the EMI/RFI shielding non-metallic substrate chassis of the present invention is shown in FIG. 8 of the drawings. In FIG. 8 the chassis structure and its bosses or appendages or holes for supporting electronic parts is formed in blocks 800, 802, and 804; molds, skeleton frames or similar pliable cloth supporting arrangements may be used in these steps.
The ossifying step at block 806 in FIG. 8 represents the impregnating of the fiberglass cloth with epoxy resin and the subsequent epoxy curing; a plurality of impregnating and curing steps may be desired.
Preparation of the chassis surfaces for the desired two film coatings is achieved at blocks 808 and 810 in FIG. 8, the preparation including physical abrasion and/or etching with chemical reagents, as is known in the art, and the electroless deposition of a thin, adhesion promoting, nickel film, an optional step as is indicated by the bypass line 816.
Deposition of the desired shielding and protective films is achieved in blocks 812 and 814; copper and nickel being the preferred films, as indicated.
The combination of copper and nickel film layers using the electroplating process provides the following desirable characteristics for the FIG. 1 and FIG. 2 structure.
1. Substantially the same level of shielding effectiveness is achieved as in a 0.06-inch thick aluminum structure.
2. The nickel exterior film provides abrasion and environmental resistance to protect the copper-plated surface.
3. A continuous coating is provided over all of the surfaces, including seams, thereby eliminating leaks of EMI/RFI.
4. An excellent electrical ground connection can easily be established--through soldering with tin-lead solder as represented by the solder globule 133, and the ground lead wire 135 connecting with the terminal 137 in FIG. 1.
5. The surface is relatively smooth and can be marked or painted easily.
The preferred arrangement for the non-metallic substrate chassis involves a formed substrate of fiberglass impregnated with epoxy and plated metallic layers on each slde of the chassis surface, the plated layers preferably extend around corners and edges of the chassis to preclude radio frequency energy leakage and the plated metallic layers also extend through the depth of holes and apertures in the fiberglass structure to both minimize leakage at these points and to provide conducting paths between the plated films on each surface of the fiberglass substrate. Although nickel is preferred for the chassis outermost film layer, a layer of rhodium can with little doubt be substituted for the nickel layer with only small performance change while yet maintaining reasonable chassis cost. Other alternate metals such as gold and cobalt, while being of good electrical and mechanical properties, would increase the chassis cost unduly.
The nickel on copper plating system described above and applied on both the inside and outside surfaces of a chassis is found to provide EMI shielding equal to that afforded by solid alumium; this plating system promises to overcome a significant obstacle in the use of plastics for chassis. The preferred fiberglass and metal film chassis is capable of achieving a weight savings of up to 30%; this is especially useful in the case of electronic systems intended for use in aircraft or spacecraft but is also desirable in reducing the mass of ground-based equipment.
While the apparatus herein described constitute a preferred embodiment of the invention, it is to be understood that the invention is not limited to this precise form of apparatus or method, and that changes may be made therein without departing from the scope of the invention, which is defined in the appended claims.
                                  TABLE 7                                 
__________________________________________________________________________
                                   APPROXIMATE                            
PROCESS                                                                   
      DESCRIPTION                                                         
               ADVANTAGES                                                 
                        DISADVANTAGES                                     
                                   COST $/Ft.sup.2                        
__________________________________________________________________________
Arc/Flame                                                                 
      Zinc, Nickel,                                                       
               Economical and                                             
                        Application is an art,                            
                                   $1.00 to $2.50                         
Spray Aluminum wire                                                       
               provides good                                              
                        preheating plastic                                
      sprayed directly                                                    
               shielding                                                  
                        parts may cause warp-                             
      on plastic surface                                                  
               effectiveness                                              
                        age. Complex shapes                               
                        difficult to coat                                 
                        uniformly. Flaking                                
                        can cause electrical                              
                        problems.                                         
Conductive                                                                
      Organic coating                                                     
               Easy to apply                                              
                        Surface rich in non-                              
                                   $0.75-$5.00                            
Paints                                                                    
      containing nickel                                                   
               and economical                                             
                        conductive resin.                                 
      or silver particles                                                 
                        Difficult to establish                            
                        electrical ground.                                
Conductive                                                                
      Aluminum & nickel                                                   
               No secondary                                               
                        Difficult to establish                            
                                   $3.00 and up                           
Fillers                                                                   
      metallized cloth.                                                   
               processing                                                 
                        electrical ground.                                
               required.                                                  
                        Physical properties                               
               Parts can be                                               
                        can be improved or                                
               mass produced.                                             
                        downgraded.                                       
Vacuum                                                                    
      Aluminum, copper                                                    
               High     Very thin coating and                             
                                   $1.25 and up                           
Metalliza-                                                                
      & nickel deposited                                                  
               conductivity.                                              
                        easily scratched.                                 
tion  deposited plating                                                   
               Economical.                                                
                        Complex shapes could                              
      or vacuum                                                           
               Good adhesion.                                             
                        cause non-uniform                                 
                        coating.                                          
Plating                                                                   
      Electroless and                                                     
               Provides very                                              
                        Surface preparation                               
                                   $1.00 for thin                         
      electrolytic                                                        
               good shielding                                             
                        required.  electroless                            
      deposition of copper                                                
               effectiveness.      coatings of                            
      or nickel from a                                                    
               Economical,         30 to 50 micro                         
      chemical solution.                                                  
               easy to estab-      inches.                                
               lish electrical     $5.00 for thick                        
               ground. Very        electrolytic                           
               uniform.            coating 1-2                            
                                   mils thick.                            
Conductive                                                                
      Polymer displays                                                    
               No secondary                                               
                        Chemically unstable                               
                                   Not available                          
Copolymer                                                                 
      electrical conduc-                                                  
               processing                                                 
                        and very sensitive                                
      tivity property                                                     
               required.                                                  
                        to moisture.                                      
      after doping                                                        
      process.                                                            
__________________________________________________________________________

Claims (19)

I claim:
1. Electronic apparatus comprising:
interference active radio frequency means emitting or spuriously responding to radio frequency energy signals;
low mass chassis means supporting, enclosing, and shielding said active radio frequency means, said chassis means including:
an organic material substrate member configured to support said active radio frequency means, said substrate member including a first exterior surface area portion and a second interior surface area portion;
a homogeneous first metallic film layer electrical shield coating disposed over said first exterior surface area portion of said substrate member; and
a homogeneous second metallic film layer magnetic shield coating differing in composition from said first metallic film layer coating and disposed over said first metallic film layer in intimate physical contact therewith.
2. The apparatus of claim 1 further including:
a homogeneous third metallic film layer electrical shield coating disposed over said said second interior surface portion of said organic material substrate member and identical in composition with said first metallic film layer electrical shield coating; and
a homogeneous fourth metallic film layer magnetic shield coating differing in composition from said third metallic film layer electrical shield coating and disposed over said third metallic film layer coating in intimate physical contact therewith, said fourth metallic film layer coating being identical in composition with said second metallic film layer coating.
3. The apparatus of claim 2 further including an additional homogeneous thin metallic film coating layer means located intermediate said substrate member and said first metallic film layer coating for enhancing the adhesion between said substrate and said first metallic film layer coating.
4. The apparatus of claim 2 wherein said first metallic film layer electrical shield coating is composed of copper.
5. The apparatus of claim 4 wherein said second metalic film layer coating is composed of nickel.
6. The apparatus of claim 5 wherein said substrate member is composed of epoxy-impregnated fiberglass.
7. A lightweight chassis for use with radio frequency electromagnetic interference active electronic apparatus comprising:
an organic material substrate member configured to a closable geometric shape and having a plurality of first intersecting planes surface portions;
closure means closing said substrate member, said closure means including second surface portions;
means located on selected of said first and second surface portions mounting components of said electronic apparatus;
a multi-layered elecromagnetic radiation energy shielding and physical protection coating located on said first and second surface portions, said coating also including;
a first homogeneous metallic copper film electrical shielding layer disposed over reverse faces of said substrate member and closure means in intimate physical contact therewith; and
a second homogeneous metallic nickel film magnetic shielding layer disposed over said first film layer on said substrate member and closure means in intimate physical contact therewith.
8. The chassis of claim 7 further including shielding divider elements located within said closable geometric shape and connected with one of said substrate member and closure means.
9. The chassis of claim 7 wherein said organic material substrate is comprised of fiberglass cloth impregnated with epoxy resin.
10. The chassis of claim 9 further including an adhesion-promotion thin coating layer intermediate said substrate member and closure means surface portions and said first metallic film layer.
11. The chassis of claim 10 further including a tin-lead solder electrical connection with said nickel metallic film layer.
12. A method for making a non-metallic electrostatic field and electromagnetic field shielding chassis for an electronic apparatus comprising the steps of:
forming an open sided closable chassis structure, having interior and exterior surfaces, from a pliable non-metallic substrate material;
adding electronic component supporting elements to said chassis structure;
ossifying said pliable material into a rigid fixed shape;
covering said chassis structure interior and exterior surfaces with a first metallic film layer of good electrical conductivity; and
coating said first metallic film layer with a second and different metallic film layer on both said interior and exterior surfaces.
13. The method of claim 12 wherein said step of adding electronic component supporting elements includes perforating said chassis structure.
14. The method of claim 12 further including the step of forming an open sided closure member capable of cooperating with said chassis in forming a closed structure and ossifying with said chassis in forming a closed structure and ossifying said closure members.
15. The method of claim 12 wherein said pliable substrate material includes fiber reinforcing material.
16. The method of claim 12 further including the step of applying an adhesion-promoting layer to said chassis structure prior to said covering step.
17. The method of claim 12 wherein said covering step includes depositing said first film layer using a chemical precipitation deposition sequence.
18. The method of claim 12 wherein said coating step includes electroplating.
19. The chassis of claim 10 wherein said adhesion-promoting thin coating layer comprises a layer of nickel.
US07/112,007 1985-02-26 1987-10-19 Non-metallic chassis structure with electromagnetic field attenuating capability Abandoned USH526H (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US07/112,007 USH526H (en) 1985-02-26 1987-10-19 Non-metallic chassis structure with electromagnetic field attenuating capability

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US70583485A 1985-02-26 1985-02-26
US07/112,007 USH526H (en) 1985-02-26 1987-10-19 Non-metallic chassis structure with electromagnetic field attenuating capability

Related Parent Applications (1)

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US70583485A Continuation 1985-02-26 1985-02-26

Publications (1)

Publication Number Publication Date
USH526H true USH526H (en) 1988-09-06

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ID=26809469

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US (1) USH526H (en)

Cited By (29)

* Cited by examiner, † Cited by third party
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US5005106A (en) * 1988-12-08 1991-04-02 E. I. Du Pont De Nemours And Company Multifunctional card having an electromagnetic wave protection
US5195644A (en) * 1992-07-13 1993-03-23 Glenayre Electronics Ltd. Sealed, seamless box and method of manufacturing same
US5264992A (en) * 1991-08-02 1993-11-23 Tusk, Incorporated Modular computer system having self contained workslate unit detachably coupled to base unit including keyboard
US5520976A (en) * 1993-06-30 1996-05-28 Simmonds Precision Products Inc. Composite enclosure for electronic hardware
US5628575A (en) * 1993-12-27 1997-05-13 Fujitsu Ltd. Automatic paper feeder and frame structure of document input device
US5700342A (en) * 1993-06-30 1997-12-23 Simmonds Precision Products Inc. Composite enclosure for electronic hardware
US6252159B1 (en) * 1999-01-21 2001-06-26 Sony Corporation EMI/RFI and vibration resistant electronics enclosure
US6703123B1 (en) 2000-02-18 2004-03-09 Mitsubishi Materials Corporation Conductive fiber, manufacturing method therefor, apparatus, and application
US7054166B1 (en) * 2003-12-03 2006-05-30 Unisys Corporation Apparatus and method for EMI shielding
US20060163987A1 (en) * 2005-01-26 2006-07-27 Kim Yeung-Ki Plasma display device
US20080074342A1 (en) * 2006-09-22 2008-03-27 Ralf Lindackers Antenna assemblies including standard electrical connections and captured retainers and fasteners
US20080100521A1 (en) * 2006-10-30 2008-05-01 Derek Herbert Antenna assemblies with composite bases
US20080122708A1 (en) * 2006-11-28 2008-05-29 Ralf Lindackers Vehicle-mount antenna assemblies having snap-on outer cosmetic covers with compliant latching mechanisms for achieving zero-gap
US20080160253A1 (en) * 2006-12-29 2008-07-03 Hong Fu Jin Precision Industry (Shenzhen) Co., Ltd Plastic coated edge structure used for portable electronic device and method for making the same
US7710034B2 (en) 2005-11-07 2010-05-04 Samsung Sdi Co., Ltd. Chassis including metallic element for dissipating heat and plasma display module having the same
US20100319948A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US20100321891A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US20100321892A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US20100321890A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US20120243846A1 (en) * 2010-12-20 2012-09-27 David Blake Jackson Integrated Security Video and Electromagnetic Pulse Detector
US8599576B2 (en) 2010-10-29 2013-12-03 Emprimus, Llc Electromagnetically-protected electronic equipment
US8642900B2 (en) 2009-10-16 2014-02-04 Emprimus, Llc Modular electromagnetically shielded enclosure
US8643772B2 (en) * 2010-11-05 2014-02-04 Emprimus, Llc Electromagnetically shielded video camera and shielded enclosure for image capture devices
US8754980B2 (en) 2010-11-05 2014-06-17 Emprimus, Llc Electromagnetically shielded camera and shielded enclosure for image capture devices
US8760859B2 (en) 2010-05-03 2014-06-24 Emprimus, Llc Electromagnetically-shielded portable storage device
US8933393B2 (en) 2011-04-06 2015-01-13 Emprimus, Llc Electromagnetically-shielded optical system having a waveguide beyond cutoff extending through a shielding surface of an electromagnetically shielding enclosure
US9093755B2 (en) 2010-12-20 2015-07-28 Emprimus, Llc Lower power localized distributed radio frequency transmitter
US9642290B2 (en) 2013-03-14 2017-05-02 Emprimus, Llc Electromagnetically protected electronic enclosure
US10008767B2 (en) 2016-04-29 2018-06-26 Laird Technologies, Inc. Vehicle-mount antenna assemblies having outer covers with back tension latching mechanisms for achieving zero-gap

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US3230375A (en) 1961-12-04 1966-01-18 Mark B Van Wagoner Laminated radiation resistant panels
US3187281A (en) 1963-03-22 1965-06-01 Gen Electric Ultra high frequency converter having auxiliary shield preventing detuning caused byclosing of cover plate
US3938152A (en) 1963-06-03 1976-02-10 Mcdonnell Douglas Corporation Magnetic absorbers
US3332860A (en) 1963-09-19 1967-07-25 Basf Ag Metallizing plastic surfaces
US3806928A (en) 1964-03-16 1974-04-23 American Rockwell Corp Laminated sandwich construction
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Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5005106A (en) * 1988-12-08 1991-04-02 E. I. Du Pont De Nemours And Company Multifunctional card having an electromagnetic wave protection
US5264992A (en) * 1991-08-02 1993-11-23 Tusk, Incorporated Modular computer system having self contained workslate unit detachably coupled to base unit including keyboard
US5195644A (en) * 1992-07-13 1993-03-23 Glenayre Electronics Ltd. Sealed, seamless box and method of manufacturing same
US5520976A (en) * 1993-06-30 1996-05-28 Simmonds Precision Products Inc. Composite enclosure for electronic hardware
US5700342A (en) * 1993-06-30 1997-12-23 Simmonds Precision Products Inc. Composite enclosure for electronic hardware
US5827585A (en) * 1993-06-30 1998-10-27 Simmonds Precision Products, Inc. Composite enclosure for electronic hardware
US5628575A (en) * 1993-12-27 1997-05-13 Fujitsu Ltd. Automatic paper feeder and frame structure of document input device
US6252159B1 (en) * 1999-01-21 2001-06-26 Sony Corporation EMI/RFI and vibration resistant electronics enclosure
US6703123B1 (en) 2000-02-18 2004-03-09 Mitsubishi Materials Corporation Conductive fiber, manufacturing method therefor, apparatus, and application
US7054166B1 (en) * 2003-12-03 2006-05-30 Unisys Corporation Apparatus and method for EMI shielding
US7659667B2 (en) * 2005-01-26 2010-02-09 Samsung Sdi Co., Ltd. Plasma display device with chassis base formed of plastic and conductive material
US20060163987A1 (en) * 2005-01-26 2006-07-27 Kim Yeung-Ki Plasma display device
US7710034B2 (en) 2005-11-07 2010-05-04 Samsung Sdi Co., Ltd. Chassis including metallic element for dissipating heat and plasma display module having the same
US7492319B2 (en) 2006-09-22 2009-02-17 Laird Technologies, Inc. Antenna assemblies including standard electrical connections and captured retainers and fasteners
US20080074342A1 (en) * 2006-09-22 2008-03-27 Ralf Lindackers Antenna assemblies including standard electrical connections and captured retainers and fasteners
US20080100521A1 (en) * 2006-10-30 2008-05-01 Derek Herbert Antenna assemblies with composite bases
US20080122708A1 (en) * 2006-11-28 2008-05-29 Ralf Lindackers Vehicle-mount antenna assemblies having snap-on outer cosmetic covers with compliant latching mechanisms for achieving zero-gap
US7429958B2 (en) 2006-11-28 2008-09-30 Laird Technologies, Inc. Vehicle-mount antenna assemblies having snap-on outer cosmetic covers with compliant latching mechanisms for achieving zero-gap
US20080160253A1 (en) * 2006-12-29 2008-07-03 Hong Fu Jin Precision Industry (Shenzhen) Co., Ltd Plastic coated edge structure used for portable electronic device and method for making the same
US8059409B2 (en) 2009-06-19 2011-11-15 General Electric Company Avionics chassis
US20100321892A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US20100321890A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US7911796B2 (en) 2009-06-19 2011-03-22 General Electric Company Avionics chassis
US8023267B2 (en) 2009-06-19 2011-09-20 General Electric Company Avionics chassis
US20100319948A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US8222541B2 (en) 2009-06-19 2012-07-17 General Electric Company Avionics chassis
US20100321891A1 (en) * 2009-06-19 2010-12-23 General Electric Company Avionics Chassis
US8642900B2 (en) 2009-10-16 2014-02-04 Emprimus, Llc Modular electromagnetically shielded enclosure
US8760859B2 (en) 2010-05-03 2014-06-24 Emprimus, Llc Electromagnetically-shielded portable storage device
US8599576B2 (en) 2010-10-29 2013-12-03 Emprimus, Llc Electromagnetically-protected electronic equipment
US8643772B2 (en) * 2010-11-05 2014-02-04 Emprimus, Llc Electromagnetically shielded video camera and shielded enclosure for image capture devices
US8754980B2 (en) 2010-11-05 2014-06-17 Emprimus, Llc Electromagnetically shielded camera and shielded enclosure for image capture devices
US20120243846A1 (en) * 2010-12-20 2012-09-27 David Blake Jackson Integrated Security Video and Electromagnetic Pulse Detector
US9093755B2 (en) 2010-12-20 2015-07-28 Emprimus, Llc Lower power localized distributed radio frequency transmitter
US9420219B2 (en) * 2010-12-20 2016-08-16 Emprimus, Llc Integrated security video and electromagnetic pulse detector
US8933393B2 (en) 2011-04-06 2015-01-13 Emprimus, Llc Electromagnetically-shielded optical system having a waveguide beyond cutoff extending through a shielding surface of an electromagnetically shielding enclosure
US9642290B2 (en) 2013-03-14 2017-05-02 Emprimus, Llc Electromagnetically protected electronic enclosure
US10136567B2 (en) 2013-03-14 2018-11-20 Emprimus, Llc Electromagnetically protected electronic enclosure
US10008767B2 (en) 2016-04-29 2018-06-26 Laird Technologies, Inc. Vehicle-mount antenna assemblies having outer covers with back tension latching mechanisms for achieving zero-gap

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