US1575359A - Lubrication system for aeronautical motors - Google Patents
Lubrication system for aeronautical motors Download PDFInfo
- Publication number
- US1575359A US1575359A US693473A US69347324A US1575359A US 1575359 A US1575359 A US 1575359A US 693473 A US693473 A US 693473A US 69347324 A US69347324 A US 69347324A US 1575359 A US1575359 A US 1575359A
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- oil
- reservoir
- pump
- motor
- supply
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16N—LUBRICATING
- F16N13/00—Lubricating-pumps
- F16N13/22—Lubricating-pumps with distributing equipment
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Description
March 2 1926.
Filed Feb. 18 1924 INVENTOR JETHUE NUTT BY- Patented Mar. 2, 1926.
M01103 COMPANY, INC., .A CORPORA'IION OF NEW YORK.
nonnronrron sYsrnM non nnnonnurrcnn MOTORS.
Application filed-February 18, 1924. Serial No. 693,473.
To all whom z't-may concern: Be it known that I, ARTHUR NUTT, a citizen of the United States, residing at Buiialo, in the county of Erie and State of New York, have invented certain new and useful Improvements in Lubrication Systems for Aeronautical Motors, of which the following is a specification.
My invention relates to motors and more particularly to motor lubrication.
In motor lubrication systems of the type disclosed in Patent No. 1,529,038, issued January 27, 1920, a serious and oft-times dangerous drawback has been found to exist, 1 to wit: the tendency to build up air under pressure within the oil supply tank or reservoir. ture it is the present practise to provide an extremely large air vent pipe leading back from said supply tank to the crank case of the motor. Such an arrangement, while relieving the situation, does not in any way attempt to avoid the cause. The presence of air in the supply tank or reservoir is due 2 entirely to the fact that an aeronautical motor in operation, is required to assume, for periods of varying duration, difi'erent angular positions, which changes in the position of the motor with respect to the horizontal, 3 cause the oil draining from the various parts oi the motor reqniring lubrication to shift constantly back and forth from end to end of the crank case or drainage reservoir.
Normally the oil draining toward the bottom of the crank case is removed therefrom as fast as it accumulates in order that the crank case ior drainage reservoir may be maintained substantially dry. For this purpose either a duplex scavenging oil pump or two independently operating oil pumps are proi vided, one of which pumps draws its supply of oil from one end of the drainage reservoir and the other of which pumps draws its supply of oil from theopposite end thereof, and both of which pumps independently return such oilby separate paths to the outside oil tank or supply reservoir. As long as both scavenging oil pumps (or at least the intake portions thereof) are immersed in oil such a system of motor lubrication works perfectly. Unfortunately however, when the motor is appreciably inclined to the horizontal, one or the other of the pumps, instead of pumping oil, pumps either oil and air mixed or air alone; and since both pumps deliver To overcome this objectionable feaseparately to the-outside oil tank or-reser- "PATENT- OFFICE, w
ARTHUR NUTT, or nurmn nnw YORK, ASSIGNOR T0 o'on'rrss Annormnn- & I
V011, obviously either one or the other oftwo things are bound to occur i. e. either the air builds up under pressure within the outside supply tank or reservoir or it is vented back,
as suggested, again to the crank case of the motor.
The object of the present invention'is to overcome entirely the objectionable features above pointed out. In attaining this object I merely so arrange the two scavenging oil pumps as to admit vof their operation in series as distinguished from the heretofore independent operation thereof. Instead ofone scavenging pump drawing its supply of oil from one end of the motor crank case or drainage reservoir and the other scavenging oil pump drawing its supply from the opposite end of said reservoir and each independently returning such oil to the supply tank, one of said pumps draws its supply of oil from one end of the motor crank case and delivers it to the opposite end thereof whereas the other of said pumps picks up the oil from said last mentioned crank caseend and delivers it to the supply tank. In all other respects the operation of the two systems is in principle the same. Moreover, by a series arrangement of the I two scavenging oil pumps I find that instead of an emulsion of oil and air being constantly delivered to the supply tank from the motor, a solid steady Stream-0f oil ispr'oduced and delivered at all times. a
In the drawing, wherein my improved sys-\ tem of motor lubrication is diagranomatical- 'ly illustrated, 10 designates the bottom half 1 s of the motor crank case or the drainage resa ervoir, 11.1 the outside'oil tank or supply reservoir, 12 the pressure or delivery oil pump, 13 and 14.- the two scavenging oil pumps, and 15 and 16 the two oil sumps or crank case depressions formed at the base of the drainage reservoir and into which the induction'pipes leading respectively to the two soavenglng pumps 13 and '14 extend. The arrows lndicate the direction of the flow of the oil.
scavenging oil pump 14 picks up :theoil as it falls by gravity into the oil sump. 15 at or near the propeller end of the motor and delivers it to-the oil sump 16:at or near the:
' picks up the 011 in t e oil sump 16 and delivers it to the outside oil tank or supply reservoir 11. Both oil intakes i. e. the oil intake for the pump 13 and the oil'intake for the v r duct havlng its inlet end within and at one pump 14, being immersed in oil, a steady solid stream of oil is delivered to thetank 11 by the pum 13 and a steady stream of oil is delivere from the sump 15 to the sump 16 by the pump la'. :In flylng at a steep climbing angle, except for the fact 7 that the pump 14 is pumping either oil and air mixed or air alone, the operation of the system is thesame. Air however,.tho admitted to the pump 14 under the conditions stated, is of no moment since the pump 14 discharges into the sump 16 where the pumped air is liberated and immediately permitted to again enter the crankcase from which it was originally withdrawn. Meanwhile the pump 13 is constantly pumping oil from the crank case to the tank 11, and since the pumping capacity of each scavenging pump is equal to or greater than the pumping capacity of the pressure or delivery pump 12, obviously a substantially dry crank case is maintained.
. If desired, the disposition of the pumps may be otherwise than shown, and likewise, if desired, the pump 13 may be placed at the propeller end of themotor and the pump 14 made to withdraw oil from the anti-propeller end. Moreover plunger pumps'may beused instead of gear pumps and the supply tank made apart of the motor crank case by partitioning it ofi.
,While I have described my invention in detail in its present preferred embodiment, it will be obvious to those skilled in the art after understanding my invention, that va-a rious changes and modifications may be made" therein without departing from the spirit or scope thereof. I- aim in the appended claims to cover all such modifications and changes. 7
What is claimed is:
1. A lubrication system for traveling motors including a drainage reservoir, an oil duct having its inlet end within said reservoir and its outlet end likewise within said reservoir but at a-point remote from said inlet end, a scavenging oil ump operable to withdraw oil from said rainage reservoir at the inlet end of said oil duct and to deliver it again to said' reservoir at the outlet cnd thereof a supply reservoir, a second scavenging oil" pump operable to withdraw oil from said draina e reservoir and to deliver it to-said su p y reservoir, and a delivery pump opera le to withdraw oil from said supply reservoir and to deliver it again to the motor. p
' 2. A lubrication system for traveling motors including a drainage reservoir, an oil 1 end of said reservoir and itsoutlet end likewise within and at the opposite end of said reservoir, a s'cavengin oil pump operable to withdrawoil from sai drain-age reservoir at the inlet end of, said oil duct and to deliver it again to said reservoir at the outlet end thereof, a supply reservoir, a second scavenging oil pump operable to withdraw oil from said drainage reservoir and to deliver it to said supply reservoir, and a delivery pum operable to withdraw oil from said supp y reservoir and to deliver it again to the motor.
3. A lubrication system for traveling motors including a drainage reservoir, a supply reservoir, a scavenging oil pump operable to withdraw oil from one end of said draina e reservoir and to deliver it to said supply reservoir, an oil duct having its inlet end at the opposite end of said drainage reservoir and its outlet end at the end of said reservoir from which the oil is withdrawn by said scavenging oil pump, a second scavenging oil pump operable to withdraw oil from said drainage reservoir at, the inlet end of said oil duct and to deliver it again to said reservoir at the outlet end thereof, and a delivery oil pump operable to withdraw oil from said supply reservoir and to deliver it again to the motor.
4. A lubrication system for traveling motors including a drainage reservoir having depressions formed therein at or near its opposite ends, an oil duct having its inlet end within one of said depressions and its outlet end within-the other of said depressions, a scavenging oil pump operable to withdraw oil from said drainage reservoir at the inlet end of said oil duct and to deliver it again to said reservoir at the outlet end thereof, a supply reservoir, a second scavenging oil pump operable to withdraw oil from the depresslon in said drainage reservoir at the outlet end of said oil duct and to deliver it to said supply reservoir, and a delivery oil pump operable to withdraw oil from said supply reservoir and to deliver it again to the motor.
In testimony whereof I hereunto aflix my signature.
ARTHUR NUTT.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US693473A US1575359A (en) | 1924-02-18 | 1924-02-18 | Lubrication system for aeronautical motors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US693473A US1575359A (en) | 1924-02-18 | 1924-02-18 | Lubrication system for aeronautical motors |
Publications (1)
Publication Number | Publication Date |
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US1575359A true US1575359A (en) | 1926-03-02 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US693473A Expired - Lifetime US1575359A (en) | 1924-02-18 | 1924-02-18 | Lubrication system for aeronautical motors |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5755194A (en) * | 1995-07-06 | 1998-05-26 | Tecumseh Products Company | Overhead cam engine with dry sump lubrication system |
US6223713B1 (en) | 1996-07-01 | 2001-05-01 | Tecumseh Products Company | Overhead cam engine with cast-in valve seats |
-
1924
- 1924-02-18 US US693473A patent/US1575359A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5755194A (en) * | 1995-07-06 | 1998-05-26 | Tecumseh Products Company | Overhead cam engine with dry sump lubrication system |
US5979392A (en) * | 1995-07-06 | 1999-11-09 | Tecumseh Products Company | Overhead cam engine with integral head |
US5988135A (en) * | 1995-07-06 | 1999-11-23 | Tecumseh Products Company | Overhead vertical camshaft engine with external camshaft drive |
US6032635A (en) * | 1995-07-06 | 2000-03-07 | Tecumseh Products Company | Overhead cam engine with integral head |
US6223713B1 (en) | 1996-07-01 | 2001-05-01 | Tecumseh Products Company | Overhead cam engine with cast-in valve seats |
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