US2511611A - Aperiodic directive antenna system - Google Patents

Aperiodic directive antenna system Download PDF

Info

Publication number
US2511611A
US2511611A US697453A US69745346A US2511611A US 2511611 A US2511611 A US 2511611A US 697453 A US697453 A US 697453A US 69745346 A US69745346 A US 69745346A US 2511611 A US2511611 A US 2511611A
Authority
US
United States
Prior art keywords
conductor
antenna
radiation
antenna system
conductors
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US697453A
Inventor
Harold A Wheeler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hazeltine Research Inc
Original Assignee
Hazeltine Research Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hazeltine Research Inc filed Critical Hazeltine Research Inc
Priority to US697453A priority Critical patent/US2511611A/en
Application granted granted Critical
Publication of US2511611A publication Critical patent/US2511611A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q11/00Electrically-long antennas having dimensions more than twice the shortest operating wavelength and consisting of conductive active radiating elements
    • H01Q11/02Non-resonant antennas, e.g. travelling-wave antenna
    • H01Q11/08Helical antennas

Definitions

  • an aperiodic directive antenna system comprises a helical radiating conductor having a pitch substantially equal to one-half of the operating wave length, a helical diameter much less than one-quarter of the operating wave length and a length of at least substantially one-half a turn.
  • the system has means for terminating one end of the conductor in its characteristic impedance and means for connecting signal-translating apparatus to the antenna system at the opposite end of the conductor, whereby the antenna system is predominantly directive in the direction of the I aforesaid opposite end and exhibits the property of radiation with substantially circular polarlzation.
  • FIG. 1 is a representation of a I two-conductor directive antenna system embodying the invention
  • Fig. 2 is an end view of the Fig.
  • FIG. 3 is a vector diagram utilized in explaining the directive properties of the antenna system of Fig. 1;
  • Fig. 4 is a schematicrepresentation of a diversity receiver employing the present invention; while Figs. 5 and 6 represent modified forms of the invention utilizing a.
  • the arrangement there represented includes an aperiodic directive antenna system of.
  • the antenna structure comprises a pair of similar radiating conductors Ill and H. Each conductor is in the form of a helix, both being pitched in the same sense.
  • helical conductors in and II are positioned coaxially but are rotationally displaced with reference to one another about their common axis. There is a wide latitude permissible in connection with the relative displacement of the conductors.
  • the displacement affects the total radiation of. the system, producing a-maximum when radia-.-
  • the conductor thickness or crosssectional diameter is very much less than the diameter d of the helix defined by theconductor.
  • the conductor thickness and conductor. spacing determine the radiation resistance as well as the reactance of the antenna structure, the radiation resistance being primarily a function of spacing and the reactance being a function of spacing as well as thickness.
  • the thickness is very small in relation to a quarter of the operatin wave length as already indicated and its upper limit is approximately determined by one-half of the conductor spacing or one-half a radian length, whichever is the smaller.
  • the dimension radian length is the wave length divided by two pi.
  • each conductor I and l I is atlea's't 'approximately one-half a turn of the helix. -although a "c'o'nductor length of only one-half a turn is perfectly feasible, the use of longer conductors improves the directivity, that is, accentuates the end-fire characteristic of the antenna. Also, longer conduotors tend to make the directivity of the antenna more selectiveasto 'ireque'ncy.
  • each conductor length is an integral multiple of 'one half turnof the helix, but as “the length L approaches a large number of half turns, the "integral relationship of length to half turns of t hehelixbecom'es less critical.
  • the antenna system under consideration has means for terminating one pair of the adjacent ends of conductors I 0 and I l in the characteristic impedance of these conductors.
  • 'Th'is'means is represented by the terminating impedance [3 of Fig. 1.
  • means are provided for-connecting signal-translating apparatus to the antenna system at the-opposite ends of its condiictors, this means being repre'se'nted'by a block diagram Id.
  • the impedance 15 within the unit I I is intended "to signify 'a terminal impedance applied thereby to conductors in and l'-l for'connecting to'the endsthereof,preierably'with impedance matching.
  • antenna systems have identical characteristics when employed 'for wave-signal transmission or reception, andit i's'forthis'reason that the block representation of unit id is 'sufli'cient as a disclosure of-either use. Whileit may designate-any wave-signal translating apparatus connected with the antenna system, it will be assumed for the purposes of the present discussion that unit I l constitutes a wave-signal transmitter.
  • the vector E1 indicates the electric field intensity, or a component of radiation with vertical plane polarization originating 'atthe point A of the conductor system I'll, ll.
  • the currents in conductors l8 and II have vertical components which add and horizontal components which oppose one an other. This gives rise to the component E1 of vertically polarized plane radiation.
  • the time delay of a current component at the point B is substantially the same as the propagation time be" tween these points. Consequently, for radiation in the direction of the excited end of the antenna there is effectively a'haIf-wave delay or half-wave path difference between the points A and B.
  • a delay or path difference of one-quarter of the operating'wave length is introduced by "the conductor length between the points A and B, and another delay is caused by the propagation time in space from the point B back to the point A.
  • the radiation component E2 from the point B in traveling toward the excited end of the antenna structure ai'rives'in phasewith the instant radiation at the point A. Therefore, radiation from the points A-and B is additive inthe direction of the excited end'of the antenna.
  • Radiation toward the end of the antenna which is terminated by the impedance I3 is quite different. Specifically, by the time the travelingwave current arrives at the point B to establish the radiation'component E2, the radiation com ponent "E1 originating at point A also arrive; at the point 'B. These radiations, being of opposite polarity or hase, tend to suppress one another. When the conductors l9 and l are symmetrical with reference to their common axis, substantially complete cancellation is obtained and radiation with vertical plane polarizatio v toward the unexcited end of the antenna is effectively nullified.
  • Aprojection of the antenna system of Fig. l in a horizontal plane would show crossover or transposition points at 'C and D.
  • a component E: of electric field radiation with horizontal plane polarization is obtained while a similar component E4 of opposite phase is established at the point D. It may be shown, in a manner similar to the treatment of the radiation from the points A and B, that the components oi'radiation with horizontal plane polarization add in the direction of the excitation end of the antenna and cancel in the direction of the opposite end.
  • the an tenna is predominantly directive in the direction of the end at which it is excited.
  • the points A and C have a separation of approximately one-eighth of the operating wave length. Therefore, radiation from the point C, referred to the point A, has a delay time or a path difference of one-quarter of the operating wave length.
  • This eiiect causes the components of radiation with horizontal plane polarization to have a phase-quadrature relation in time with reference to the components of radiation with vertical plane polarization.
  • the horizontal and vertical radiations are of the same magnitude so that the antenna system exhibits the property of radiation with approximately circular polariza tion in a direction of rotation determined by the sense of the pitch of its helical conductors l0 and II.
  • a signal from a transmitting antenna is directly intercepted by a receiving antenna without any intervening reflection
  • like antennas are to be employed. That is, the helical conductors of the receiving antenna are to be pitched in the same sense as those of the transmitting antenna.
  • the conductors of the receiving and transmitting antennas are to have opposite pitches. The discrimination between direct and reflected signals results from the fact that a circularly polarized radiation reverses its direction of rotation upon reflection.
  • Reception of signals of various origins and over various transmission paths may be accomplished in a diversity receiving system, employing a pair of spaced directive antennas, similar to the arrangement of Fig. l but having helical conductors with opposed pitches.
  • a pair of spaced directive antennas similar to the arrangement of Fig. l but having helical conductors with opposed pitches.
  • Such an arrangement is represented in Fig. l. where one antenna includes the conductors 253 and 2! having a right-hand pitch. This antenna is terminated at one end in a resistor 22 corresponding to its characteristic impedance and is terminated at the opposite end in a first diversity receiver 23.
  • the second spaced antenna includes the condu tors 24 and 25 having an opposite pitch, terminated at the remote end in its characteristic impedance by a resistor 26, and terminated at the near end in a second diversity receiver 21.
  • the pitch, helical diameter, thickness and length of the conductors of each separate antenna are as described in connection with the arrangement of Fig. l.
  • the receiving units 23 and 2? include the usual signal-translating stages through the wave-signal detector and are paralleled with the input circuit of the common signal reoroducer 2B in conventional manner.
  • the overall system is directive in the direction of the ends to which the receiving components are connected and is suited to receiving wave signals approaching as indicated by the arrow P. Since its individual antennas 21!, 2! and 2d, 25 are reversely pitched. the system may respond to wave signals of circular polarization having either direction of rotation, as well as signals of plane polarization at any angle.
  • an aperiodic antenna system in accordance with the invention may, if desired, include but a single helical conductor.
  • the antenna system has a linear conductor 39 and a helical conductor 3!. The latter is coaxially disposed about the former and their projected lengths in the vertical or horizontal plane are equal.
  • An impedance 32 connects one pair of the adjacent ends of the conductors in the characteristic impedance thereof and an impedance 33 of the same value terminates the opposite pair of conductor ends. Connections to the antenna may be made at either pair of the conductor ends. Where a directivity similar to that described for the arrangements of Figs. 1
  • the impedance 33 represents signal-translating apparatus connected to the antenna.
  • has the same pitch, helical diameter, thickness and length re- 6 cited in the discussion of conductors l0 and II of Fig.1.
  • Fig. 6 The embodiment of Fig. 6 is generally similar to that of Fig. 5 and corresponding components thereof are designated by the same reference characters primed.
  • two spiders 34 and 35 provide a space ground for the antenna system, each spider including several radially extending conductors having a length approximately equal to one-quarter of the operating wave length.
  • the spokes are preferably perpendicular to the axis of the helix.
  • the impedances 32, 33' provide critical damping terminations at the opposite ends of radiating conductor 3!. This is the same as terminating the conductor with its characteristic impedance.
  • a pair of antennas constructed in accordance with Fig. 5 or 6, may be utilized in a diversity receiving system of the type represented in Fig. 4.
  • Each of the described embodiments of the invention comprises an aperiodic directive antenna system of simplified mechanical construction.
  • the antenna is of the end-fire type and exhibits the property of radiation with approximately circular polarization in a sense related to the pitch of its helical conductor or conduc tors.
  • a very long antenna of this type has a limiting value of directivity because of its attenuation resulting from radiation and dissipation.
  • the cancellation of radiation toward the unexcited end of the antenna is maintained if the attenuation in napiers per radian length of antenna is much less than unity.
  • the power ratio of directive gain is about equal to the number of half-wave lengths in the length of the radiating conductors, if the total attenuation is less than one napier.
  • each embodiment has been considered as excited from the same end, namely. the left-hand end, as represented in the drawing.
  • the directivity may be reversed by exciting the opposite end of the antenna, so a single structure may be used for opposite directions.
  • the structures of Figs. 1, 5 and 6 have been described principally in con nection with wave-signal transmission.
  • the functions of reception and transmission with any such antenna are unavoidably associated by the reciprocity theorem. Therefore, such expressions as radiating conductor and property of radiation and the like are used in the text and in the appended claims in a generic sense to define an antenna structure in accordance with the invention whether that antenna be utilized for signal transmission or reception.
  • An aperiodic directive antenna system comprising: a helical radiating conductor having a jpitch substantially equal to :on'e-fhalfcof sthe operating wave length, a helical diameter muchiless than one-quarter of said wave length, :and a length of at least substantially one-half a turn; means for terminating one end of said conductor :in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna systemat the opposite end of said conductorywhereby said antenna system i predominantly directive in the direction -of said opposite end and exhibits 'the property of radiation with substantially circular polarization.
  • An aperiodic directive antenna system comprising: a helical radiating conductor having a pitch'substantially equal to one-half of the operating wave length, a helical diameter such less than one-quarter of said-wave length, a conductor thickness much less than said diameter, and a length of at least substantially one-half a turn; means for terminating one end of said conductor in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna system at the opposite end of said conductor, whereby said antenna system is predominantly directive in the direction of said opposite end and exhibits the property of radiation with substantially circular polarization.
  • An aperiodic directive antenna system comprising: a helical radiating conductor :having a pitchsubstantially equal to ,one-halfof .theioperating wave length, a helical diameter-much less than one-quarterofsaid wave length so that the transmission .time along a given section of said-conductor issubstantially the-same as the wave-propagation time along a corresponding space path, and havinga length oi -at least substantially-one-half a, .turn; means v-for terminating one .end of said conductor in its characteristic impedance; and means for .connecting Signail-translating apparatus to said antenna systematthe opposite end of said conductor, whereby said antenna system is predominantly-directive in the direction oi said'oppositeend and exhibits the property of:radiation:with substantially: circular polarization.
  • .-An .aperiodic directive antenna system “comprising: a helical eradiating conductor having a pitch substantiallyequal tonne-half of the operating wave length, a helicaldiameter much less than one-quarter of said wave length, and a length substantially equal -to'an integral multiple of one-half a turn; means for terminatingone end of said "conductor in "its characteristic impedance; and 'means for connecting signaltranslating apparatus 'to'said antenna system at the oppositeend of said conductor, whereby said antennasystem is predominantly'directive in the direction "of said *opposite end and exhibits the property of radiation with substantially circular polarization.
  • An aperiodic directive antenna system comprising: a helical radiating conductor'having a pitch substantially equal to one-half of the operating'wave length, a helical diameter much less than one-quarter of said wave length, and a length of at least substantially one-halfa'turn; means for terminating one end of said conductor in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna system with impedance matching at the opposite end of saidconductor, whereby said antenna system is predominantly directive in the direction of said opposite end and exhibits in its characteristic impedance; and means forconnecting signal-translating apparatus to said antenna'systematthe opposite end of said 'conductor, whereby-said antenna system ispredominantlydirective in the directionof said oppositeend and "exhibits the property of radiation with substantiallypircular polarization.
  • Anraperio'dic "directive :antennasystem comprising: a linear conductor; a single helical radiating conductor coaxially disposed about "said linear conductor, having a pitch substantially equal to one-half of :the operati-ngwave length,
  • Anaperiodic directive antenna system comprising: a'singlehelical radiating conductorhaving a pitch substantially equal to one-half of the operating wave length, a helical diameter muchlessthan-one quarter of said wave length, and :a length of at'least substantially one-half a turnymeans for providing a space ground for said antenna system; an impedance, having a value equal to the characteristic impedance of said conductor, vfor connecting one end of said conductor tosaid space ground; and-means-ccw pled between theopposite end of said'conductor and said space ground, for connecting signaltranslating apparatus to said antenna system,
  • said :antenna system is predominantly directive in the direction -of .said opposite end and exhibits the-property of radiation .with substantially circular polarization.
  • . 9. .An .aperiodicdirective antenna system comprising: a pair of similar, coaxial helical :radiating conductors rotationally displaced with .reference .to one another about the common .axis, having a pitch substantially equal -.to one-half of the operating wave length, aspacing much. less than one-quarter of said .wave length, and a lengthof at leastsubstantially,one-halfa turn; 'means for.terminating one .pair of adjacent ends I of said conductors in the characteristic impedance of said pair of conductors; and means for connecting signal-translating apparatus to said antenna system atithe opposite ends of. said conductors, .whereby said antenna system is .predominantlyrdirectivein .the direction .of said .op-.
  • An aperiodicdirective. antenna system comprising: a pairof -similar,.coaxial helical radiating conductors positioned symmetrically with reference .to the-common .axis, having .-a pitch substantially equal to .one-half of the operating I wavelength, a spacing much less than one-quar- REFERENCES CITED
  • the following references are of record in the 15 file of this patent:

Description

June 13, I950 H. A. WHE LER APERIODIC nIRE'cTfvx: ANTENNA SYSTEM Filed, sept Ir', 194s INVENTOR. F166 HAROLD A WHEELER ATTORNE Patented June 13, 1950 UNITED STATES PATENT OFFICE APERIODIC DIRECTIVE ANTENNA SYSTEM Harold A. Wheeler, Great Neck, N. Y., assignor to Hazeltine Research, Inc., Chicago, 111., a. corporation of Illinois Application September 1'7, 1946, Serial No. 697,453
Claims. (Cl. 250-3351) the present invention. The disclosure of the copending application is specifically concerned with directional-coupling arrangements but teaches how such an arrangement may be employed as a directive or end-fire antenna. In its simplest form, it includes a pair of coplanar conductors having a spacing that is small relative to theoperating wave length and terminated to achieve a desired directivity. This antenna, however, exhibits plane polarization, whereas it may be desirable in certain installations to have an endfire antenna characterized by circular polarization. The present invention, which constitutes an extension of the development upon which the above-mentioned copending application is predicated, proposes such an end-fire antenna featuring circular polarization.
It is an object of the invention to provide a new and improved aperiodic antenna system which is predominantly directive toward one end and exhibits the property of radiation with approximately circular polarization.
It is another object of the invention to provide an improved and simplified aperiodic antenna system of the end-fire type which radiates wave signals with substantially circular polarization.
It is a further object of the invention toprovide an end-fire antenna system for a diversity receiver, featuring two directive aperiodic antennas individually responsive to received wave signals circularly polarized in one of two directions of rotation.
In accordance with the invention, an aperiodic directive antenna system comprises a helical radiating conductor having a pitch substantially equal to one-half of the operating wave length, a helical diameter much less than one-quarter of the operating wave length and a length of at least substantially one-half a turn. The system has means for terminating one end of the conductor in its characteristic impedance and means for connecting signal-translating apparatus to the antenna system at the opposite end of the conductor, whereby the antenna system is predominantly directive in the direction of the I aforesaid opposite end and exhibits the property of radiation with substantially circular polarlzation.
For a better understanding of the present invention, together with other and further objects thereof, reference is had to the following description taken in connection with the accompanying drawing, and its scope will be pointed out in the appended claims.
In the drawing, Fig. 1 is a representation of a I two-conductor directive antenna system embodying the invention; Fig. 2 is an end view of the Fig.
l arrangement; Fig. 3 is a vector diagram utilized in explaining the directive properties of the antenna system of Fig. 1; Fig. 4 is a schematicrepresentation of a diversity receiver employing the present invention; while Figs. 5 and 6 represent modified forms of the invention utilizing a.
single conductor of helical configuration.
Referring now more particularly to Figs. 1.
and 2, the arrangement there represented includes an aperiodic directive antenna system of.
the end-fire type. The antenna structure comprises a pair of similar radiating conductors Ill and H. Each conductor is in the form of a helix, both being pitched in the same sense. The
helical conductors in and II are positioned coaxially but are rotationally displaced with reference to one another about their common axis. There is a wide latitude permissible in connection with the relative displacement of the conductors.
The displacement affects the total radiation of. the system, producing a-maximum when radia-.-
tion from one conductor aids that from the other to the fullest and minimizing radiation where the conductor arrangement causes the components of radiation from the two conductors to cancel. For optimum results one conductor is displaced half a turn relative to the other so that they are positioned symmetrically with respect totheir common axis. This symmetrical relaductor structure.
line d, Fig. l. The conductor thickness or crosssectional diameter is very much less than the diameter d of the helix defined by theconductor.
The conductor thickness and conductor. spacing determine the radiation resistance as well as the reactance of the antenna structure, the radiation resistance being primarily a function of spacing and the reactance being a function of spacing as well as thickness. Usually, the thickness is very small in relation to a quarter of the operatin wave length as already indicated and its upper limit is approximately determined by one-half of the conductor spacing or one-half a radian length, whichever is the smaller. The dimension radian length is the wave length divided by two pi.
The length, indicated by dimension line L, of each conductor I and l I is atlea's't 'approximately one-half a turn of the helix. -While a "c'o'nductor length of only one-half a turn is perfectly feasible, the use of longer conductors improves the directivity, that is, accentuates the end-fire characteristic of the antenna. Also, longer conduotors tend to make the directivity of the antenna more selectiveasto 'ireque'ncy. For the mos'tpart, "each conductor length is an integral multiple of 'one half turnof the helix, but as "the length L approaches a large number of half turns, the "integral relationship of length to half turns of t hehelixbecom'es less critical. I p
The antenna system under consideration has means for terminating one pair of the adjacent ends of conductors I 0 and I l in the characteristic impedance of these conductors. 'Th'is'means is represented by the terminating impedance [3 of Fig. 1. Additionally, means are provided for-connecting signal-translating apparatus to the antenna system at the-opposite ends of its condiictors, this means being repre'se'nted'by a block diagram Id. The impedance 15 within the unit I I is intended "to signify 'a terminal impedance applied thereby to conductors in and l'-l for'connecting to'the endsthereof,preierably'with impedance matching. is well understood, antenna systems have identical characteristics when employed 'for wave-signal transmission or reception, andit i's'forthis'reason that the block representation of unit id is 'sufli'cient as a disclosure of-either use. Whileit may designate-any wave-signal translating apparatus connected with the antenna system, it will be assumed for the purposes of the present discussion that unit I l constitutes a wave-signal transmitter.
In considering the operation of the Fig. 1 arrangement and 'theman'ner in which'it attains a directive I radiation characteristic, reference is mad'eto the vector diagram'o'f Fig. 3-. "The vector E1 indicates the electric field intensity, or a component of radiation with vertical plane polarization originating 'atthe point A of the conductor system I'll, ll. At this point, for the instantaneous current condition indicated by the arrowsIi and I the currents in conductors l8 and II have vertical components which add and horizontal components which oppose one an other. This gives rise to the component E1 of vertically polarized plane radiation. At the point B, a quarter wave distant from the first reference point A, the currents in conductors I 0 and I] again present vertical components in adding relation and horizontal componentswhi'ch are opposed. However, the transposition of the conductors due'to the helical configuration causes the electric field intensity or radiation component E2 originating at the 'p'o intB 'to be in phase opposition "with the first-mentioned radiation compon'ent-Ei. In similar fashion, it "may be demonstrated that at each transposition point of the conductors in a vertical plane similar radiation "path of corresponding length.
for the traveling wave of current along a given section of the conductors that is substantially the sameas the wave-propagation time along a space In other words, the time delay of a current component at the point B, relate'd'tothe reference point A, is substantially the same as the propagation time be" tween these points. Consequently, for radiation in the direction of the excited end of the antenna there is effectively a'haIf-wave delay or half-wave path difference between the points A and B. A delay or path difference of one-quarter of the operating'wave length is introduced by "the conductor length between the points A and B, and another delay is caused by the propagation time in space from the point B back to the point A. In view of this delay or path diiierence, the radiation component E2 from the point B in traveling toward the excited end of the antenna structure ai'rives'in phasewith the instant radiation at the point A. Therefore, radiation from the points A-and B is additive inthe direction of the excited end'of the antenna.
Radiation toward the end of the antenna which is terminated by the impedance I3 is quite different. Specifically, by the time the travelingwave current arrives at the point B to establish the radiation'component E2, the radiation com ponent "E1 originating at point A also arrive; at the point 'B. These radiations, being of opposite polarity or hase, tend to suppress one another. When the conductors l9 and l are symmetrical with reference to their common axis, substantially complete cancellation is obtained and radiation with vertical plane polarizatio v toward the unexcited end of the antenna is effectively nullified.
Aprojection of the antenna system of Fig. l in a horizontal plane would show crossover or transposition points at 'C and D. At the point C, a component E: of electric field radiation with horizontal plane polarization is obtained while a similar component E4 of opposite phase is established at the point D. It may be shown, in a manner similar to the treatment of the radiation from the points A and B, that the components oi'radiation with horizontal plane polarization add in the direction of the excitation end of the antenna and cancel in the direction of the opposite end. Thus, it is apparent that the an tenna is predominantly directive in the direction of the end at which it is excited.
The points A and C have a separation of approximately one-eighth of the operating wave length. Therefore, radiation from the point C, referred to the point A, has a delay time or a path difference of one-quarter of the operating wave length. This eiiect causes the components of radiation with horizontal plane polarization to have a phase-quadrature relation in time with reference to the components of radiation with vertical plane polarization. The horizontal and vertical radiations are of the same magnitude so that the antenna system exhibits the property of radiation with approximately circular polariza tion in a direction of rotation determined by the sense of the pitch of its helical conductors l0 and II.
In a complete communication system of the direct signal type, wherein a, signal from a transmitting antenna is directly intercepted by a receiving antenna without any intervening reflection, like antennas are to be employed. That is, the helical conductors of the receiving antenna are to be pitched in the same sense as those of the transmitting antenna. On the other hand, where it is desired to detect reflected signals and to reject direct ones, the conductors of the receiving and transmitting antennas are to have opposite pitches. The discrimination between direct and reflected signals results from the fact that a circularly polarized radiation reverses its direction of rotation upon reflection.
Reception of signals of various origins and over various transmission paths may be accomplished in a diversity receiving system, employing a pair of spaced directive antennas, similar to the arrangement of Fig. l but having helical conductors with opposed pitches. Such an arrangement is represented in Fig. l. where one antenna includes the conductors 253 and 2! having a right-hand pitch. This antenna is terminated at one end in a resistor 22 corresponding to its characteristic impedance and is terminated at the opposite end in a first diversity receiver 23. The second spaced antenna includes the condu tors 24 and 25 having an opposite pitch, terminated at the remote end in its characteristic impedance by a resistor 26, and terminated at the near end in a second diversity receiver 21. The pitch, helical diameter, thickness and length of the conductors of each separate antenna are as described in connection with the arrangement of Fig. l. The receiving units 23 and 2? include the usual signal-translating stages through the wave-signal detector and are paralleled with the input circuit of the common signal reoroducer 2B in conventional manner. The overall system is directive in the direction of the ends to which the receiving components are connected and is suited to receiving wave signals approaching as indicated by the arrow P. Since its individual antennas 21!, 2! and 2d, 25 are reversely pitched. the system may respond to wave signals of circular polarization having either direction of rotation, as well as signals of plane polarization at any angle.
While the arrangements thus far described utilize two rotationally displaced helical conductors, an aperiodic antenna system in accordance with the invention may, if desired, include but a single helical conductor. In Fig. 5, for example, the antenna system has a linear conductor 39 and a helical conductor 3!. The latter is coaxially disposed about the former and their projected lengths in the vertical or horizontal plane are equal. An impedance 32 connects one pair of the adjacent ends of the conductors in the characteristic impedance thereof and an impedance 33 of the same value terminates the opposite pair of conductor ends. Connections to the antenna may be made at either pair of the conductor ends. Where a directivity similar to that described for the arrangements of Figs. 1
and 4 is desired, the impedance 33 represents signal-translating apparatus connected to the antenna. The helical conductor 3| has the same pitch, helical diameter, thickness and length re- 6 cited in the discussion of conductors l0 and II of Fig.1.
The embodiment of Fig. 6 is generally similar to that of Fig. 5 and corresponding components thereof are designated by the same reference characters primed. In this case, two spiders 34 and 35 provide a space ground for the antenna system, each spider including several radially extending conductors having a length approximately equal to one-quarter of the operating wave length. The spokes are preferably perpendicular to the axis of the helix. The impedances 32, 33' provide critical damping terminations at the opposite ends of radiating conductor 3!. This is the same as terminating the conductor with its characteristic impedance. The characteristic impedance of the conductor 3! is determined by a pseudo-shield or equipotential surface established around the conductor by capacitive currents which leave and enter the conductor along spaced portions of its length. This pseudo-shield, however, does not impede radiation from the conductor. A pair of antennas, constructed in accordance with Fig. 5 or 6, may be utilized in a diversity receiving system of the type represented in Fig. 4.
Each of the described embodiments of the invention comprises an aperiodic directive antenna system of simplified mechanical construction. In each case the antenna is of the end-fire type and exhibits the property of radiation with approximately circular polarization in a sense related to the pitch of its helical conductor or conduc tors. A very long antenna of this type has a limiting value of directivity because of its attenuation resulting from radiation and dissipation. The cancellation of radiation toward the unexcited end of the antenna is maintained if the attenuation in napiers per radian length of antenna is much less than unity. The power ratio of directive gain is about equal to the number of half-wave lengths in the length of the radiating conductors, if the total attenuation is less than one napier.
For convenience, each embodiment has been considered as excited from the same end, namely. the left-hand end, as represented in the drawing. The directivity may be reversed by exciting the opposite end of the antenna, so a single structure may be used for opposite directions. Also for convenience, the structures of Figs. 1, 5 and 6 have been described principally in con nection with wave-signal transmission. As already indicated, the functions of reception and transmission with any such antenna are unavoidably associated by the reciprocity theorem. Therefore, such expressions as radiating conductor and property of radiation and the like are used in the text and in the appended claims in a generic sense to define an antenna structure in accordance with the invention whether that antenna be utilized for signal transmission or reception.
While there have been described what are at present considered to be the preferred embodiments ofthisinvention, it will be obvious to those skilled in the art that various changes and modifications may be made therein without departing from the invention, and it is, therefore, aimed to cover all such changes and modifications as fall within the true spirit and scope of the invention.
What is claimed is:
1. An aperiodic directive antenna system comprising: a helical radiating conductor having a jpitch substantially equal to :on'e-fhalfcof sthe operating wave length, a helical diameter muchiless than one-quarter of said wave length, :and a length of at least substantially one-half a turn; means for terminating one end of said conductor :in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna systemat the opposite end of said conductorywhereby said antenna system i predominantly directive in the direction -of said opposite end and exhibits 'the property of radiation with substantially circular polarization.
2. An aperiodic directive antenna system comprising: a helical radiating conductor having a pitch'substantially equal to one-half of the operating wave length, a helical diameter such less than one-quarter of said-wave length, a conductor thickness much less than said diameter, and a length of at least substantially one-half a turn; means for terminating one end of said conductor in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna system at the opposite end of said conductor, whereby said antenna system is predominantly directive in the direction of said opposite end and exhibits the property of radiation with substantially circular polarization.
3. An aperiodic directive antenna systemcomprising: a helical radiating conductor :having a pitchsubstantially equal to ,one-halfof .theioperating wave length, a helical diameter-much less than one-quarterofsaid wave length so that the transmission .time along a given section of said-conductor issubstantially the-same as the wave-propagation time along a corresponding space path, and havinga length oi -at least substantially-one-half a, .turn; means v-for terminating one .end of said conductor in its characteristic impedance; and means for .connecting Signail-translating apparatus to said antenna systematthe opposite end of said conductor, whereby said antenna system is predominantly-directive in the direction oi said'oppositeend and exhibits the property of:radiation:with substantially: circular polarization.
4. .-An .aperiodic directive antenna system "comprising: a helical eradiating conductor having a pitch substantiallyequal tonne-half of the operating wave length, a helicaldiameter much less than one-quarter of said wave length, and a length substantially equal -to'an integral multiple of one-half a turn; means for terminatingone end of said "conductor in "its characteristic impedance; and 'means for connecting signaltranslating apparatus 'to'said antenna system at the oppositeend of said conductor, whereby said antennasystem is predominantly'directive in the direction "of said *opposite end and exhibits the property of radiation with substantially circular polarization.
An aperiodic directive antenna system comprising: a helical radiating conductor'having a pitch substantially equal to one-half of the operating'wave length, a helical diameter much less than one-quarter of said wave length, and a length of at least substantially one-halfa'turn; means for terminating one end of said conductor in its characteristic impedance; and means for connecting signal-translating apparatus to said antenna system with impedance matching at the opposite end of saidconductor, whereby said antenna system is predominantly directive in the direction of said opposite end and exhibits in its characteristic impedance; and means forconnecting signal-translating apparatus to said antenna'systematthe opposite end of said 'conductor, whereby-said antenna system ispredominantlydirective in the directionof said oppositeend and "exhibits the property of radiation with substantiallypircular polarization.
-7. Anraperio'dic "directive :antennasystem comprising: a linear conductor; a single helical radiating conductor coaxially disposed about "said linear conductor, having a pitch substantially equal to one-half of :the operati-ngwave length,
arheli-cal diameter-muc'hless than one-quarter of said wavelength, a thickness muchless than said helical'diameteran'd 'a length of atleast'substantially'one- 'half a turn; 'meansfor terminating'one pair of the adjacent ends of 'said'conductors'inthe characteristic impedance thereof; and means for connecting signal-translating apparatus to said antenna system at the opposite ends of said conductorawhereby said antenna systemis predominantly directive in the direction of said opposite ends 'and exhibits the property of radia-' tionwith substantially circular polarization.
'8. Anaperiodic directive antenna system comprising: a'singlehelical radiating conductorhaving a pitch substantially equal to one-half of the operating wave length, a helical diameter muchlessthan-one quarter of said wave length, and :a length of at'least substantially one-half a turnymeans for providing a space ground for said antenna system; an impedance, having a value equal to the characteristic impedance of said conductor, vfor connecting one end of said conductor tosaid space ground; and-means-ccw pled between theopposite end of said'conductor and said space ground, for connecting signaltranslating apparatus to said antenna system,
whereby said :antenna system is predominantly directive in the direction -of .said opposite end and exhibits the-property of radiation .with substantially circular polarization.
. 9. .An .aperiodicdirective antenna system comprising: a pair of similar, coaxial helical :radiating conductors rotationally displaced with .reference .to one another about the common .axis, having a pitch substantially equal -.to one-half of the operating wave length, aspacing much. less than one-quarter of said .wave length, and a lengthof at leastsubstantially,one-halfa turn; 'means for.terminating one .pair of adjacent ends I of said conductors in the characteristic impedance of said pair of conductors; and means for connecting signal-translating apparatus to said antenna system atithe opposite ends of. said conductors, .whereby said antenna system is .predominantlyrdirectivein .the direction .of said .op-.
posite ends of .said conductors andexhibits the,
property of radiation with substantially circular polarization.
.10. An aperiodicdirective. antenna system comprising: a pairof -similar,.coaxial helical radiating conductors positioned symmetrically with reference .to the-common .axis, having .-a pitch substantially equal to .one-half of the operating I wavelength, a spacing much less than one-quar- REFERENCES CITED The following references are of record in the 15 file of this patent:
UNITED STATES PATENTS Number Name Date Affel Feb. 1, 1927 Hagen Feb. 21, 1933 Warren Aug. 9, 1938 Peterson Apr. 11, 1939 Beverage July 1, 1941 Bailey Oct. 13, 1942 Kandoian Jan. 2, 1945
US697453A 1946-09-17 1946-09-17 Aperiodic directive antenna system Expired - Lifetime US2511611A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US697453A US2511611A (en) 1946-09-17 1946-09-17 Aperiodic directive antenna system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US697453A US2511611A (en) 1946-09-17 1946-09-17 Aperiodic directive antenna system

Publications (1)

Publication Number Publication Date
US2511611A true US2511611A (en) 1950-06-13

Family

ID=24801170

Family Applications (1)

Application Number Title Priority Date Filing Date
US697453A Expired - Lifetime US2511611A (en) 1946-09-17 1946-09-17 Aperiodic directive antenna system

Country Status (1)

Country Link
US (1) US2511611A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663869A (en) * 1950-07-07 1953-12-22 Adcock Mack Donald Helical antenna scanning system
US2985878A (en) * 1952-02-13 1961-05-23 Gen Electric Wound antenna with conductive support
US3019438A (en) * 1957-03-18 1962-01-30 Gen Electric Antenna structure
US3083364A (en) * 1958-07-23 1963-03-26 Andrew Corp Bifilar wound quarter-wave helical antenna having broadside radiation
US3113456A (en) * 1956-06-15 1963-12-10 Acoustica Associates Inc Liquid volume sensing system
US3617890A (en) * 1967-01-12 1971-11-02 Sumitomo Electric Industries Induction radio system for vehicles
US4270128A (en) * 1976-06-21 1981-05-26 National Research Development Corporation Radio antennae
US5329287A (en) * 1992-02-24 1994-07-12 Cal Corporation End loaded helix antenna
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
US11349201B1 (en) * 2019-01-24 2022-05-31 Northrop Grumman Systems Corporation Compact antenna system for munition

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1615896A (en) * 1922-12-15 1927-02-01 American Telephone & Telegraph High-frequency signaling system
US1898661A (en) * 1930-10-13 1933-02-21 Telefunken Gmbh Antenna system
US2126295A (en) * 1934-04-25 1938-08-09 Western Electric Co Antenna system
US2153589A (en) * 1936-05-19 1939-04-11 Rca Corp Antenna
US2247743A (en) * 1938-12-10 1941-07-01 Rca Corp Antenna
US2298449A (en) * 1941-11-08 1942-10-13 Bell Telephone Labor Inc Antenna
US2366195A (en) * 1942-11-23 1945-01-02 Standard Telephones Cables Ltd Antenna array

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1615896A (en) * 1922-12-15 1927-02-01 American Telephone & Telegraph High-frequency signaling system
US1898661A (en) * 1930-10-13 1933-02-21 Telefunken Gmbh Antenna system
US2126295A (en) * 1934-04-25 1938-08-09 Western Electric Co Antenna system
US2153589A (en) * 1936-05-19 1939-04-11 Rca Corp Antenna
US2247743A (en) * 1938-12-10 1941-07-01 Rca Corp Antenna
US2298449A (en) * 1941-11-08 1942-10-13 Bell Telephone Labor Inc Antenna
US2366195A (en) * 1942-11-23 1945-01-02 Standard Telephones Cables Ltd Antenna array

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663869A (en) * 1950-07-07 1953-12-22 Adcock Mack Donald Helical antenna scanning system
US2985878A (en) * 1952-02-13 1961-05-23 Gen Electric Wound antenna with conductive support
US3113456A (en) * 1956-06-15 1963-12-10 Acoustica Associates Inc Liquid volume sensing system
US3019438A (en) * 1957-03-18 1962-01-30 Gen Electric Antenna structure
US3083364A (en) * 1958-07-23 1963-03-26 Andrew Corp Bifilar wound quarter-wave helical antenna having broadside radiation
US3617890A (en) * 1967-01-12 1971-11-02 Sumitomo Electric Industries Induction radio system for vehicles
US4270128A (en) * 1976-06-21 1981-05-26 National Research Development Corporation Radio antennae
US5329287A (en) * 1992-02-24 1994-07-12 Cal Corporation End loaded helix antenna
US20100277389A1 (en) * 2009-05-01 2010-11-04 Applied Wireless Identification Group, Inc. Compact circular polarized antenna
US8106846B2 (en) 2009-05-01 2012-01-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna
US8618998B2 (en) 2009-07-21 2013-12-31 Applied Wireless Identifications Group, Inc. Compact circular polarized antenna with cavity for additional devices
US11349201B1 (en) * 2019-01-24 2022-05-31 Northrop Grumman Systems Corporation Compact antenna system for munition

Similar Documents

Publication Publication Date Title
US2507528A (en) Antenna
US5264862A (en) High-isolation collocated antenna systems
US2238770A (en) High frequency electrical conductor or radiator
US3740754A (en) Broadband cup-dipole and cup-turnstile antennas
US2283914A (en) Antenna
US2184729A (en) Antenna system
US2511611A (en) Aperiodic directive antenna system
US2425336A (en) Microwave directive antenna
US2648768A (en) Dipole antenna
US2953786A (en) Antenna for polarized propagation
US2495399A (en) Antenna system
US2235163A (en) Broad band antenna
US3373433A (en) Dual linear/circular polarization spiral antenna
US2281429A (en) Antenna
US3044063A (en) Directional antenna system
US2095083A (en) Directional antenna system
US2210491A (en) High frequency antenna
US2618746A (en) Antenna system
US1874983A (en) Ultra short wave antenna system
US2643334A (en) Turnstile antenna
US2174353A (en) Transmission of waves with rotary polarization
US2153768A (en) Antenna system
US2503952A (en) Traveling wave antenna
US2594839A (en) Electrical apparatus
US2283617A (en) Antenna