US2271826A - Plant for pneumatic, hydraulic, or like fluid control - Google Patents
Plant for pneumatic, hydraulic, or like fluid control Download PDFInfo
- Publication number
- US2271826A US2271826A US11122336A US2271826A US 2271826 A US2271826 A US 2271826A US 11122336 A US11122336 A US 11122336A US 2271826 A US2271826 A US 2271826A
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- US
- United States
- Prior art keywords
- tank
- pump
- liquid
- pipe
- pressure
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-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/85978—With pump
- Y10T137/85986—Pumped fluid control
- Y10T137/86002—Fluid pressure responsive
Definitions
- One or more tanks for the storage of the de-' livered fluid said tank or tanks being provided with a check-valve;
- the pressure prevailing in the tank may be conserved.
- This pressure may serve to control several times in succession the jacks or like parts which are to be displaced, notwithstanding a breakage of the pipes on the upstream side of the check-valve or a breakdown of the pump or a breakdown of the motor which drives the pump.
- one or more distributers can be connected directly with the delivery end of the pump, without being fed by said storage tank or according to another feature of the invention.
- the pump comprises a pipe for the evacuation of air and for re-priming, said pipe connecting the intake end of the pump to the top of the feeding tank, which latter is in tree connection with the atmosphere.
- a submerged pump i. e., a pump located in immediate proximity to the aforesaid tank to which it is connected in this
- the Jacks may discharge into the atmosphere.
- the distributing valves are preferably situated at the lowest points of the circuits.
- a small amount of oil or other liquid is provided in these circuits and collects at these lowest points, thus insuring absolutely non-leakin: conditions for the said valves; the oil which is drawn along with the air or other gas will again enter the intake pipe of the compressor.
- Fig. l is a diagrammatic general view of the improved hydraulic or pneumatic control in accordance with the invention.
- Fig. 1a shows a modification
- Fig. 2 is a like view of a modification
- Fig. 3 is a like view, showing a preferred modification of a pneumatic plant.
- the plant comprises a pump I, which may be of any type.
- This pump withdraws the liquid, such as oil or the like, through a pipe 2, from a feeding tank 3, which is at a higher level than the pump.
- a pipe I This pipe, if necessary, may be provided with any usual check-valve which will prevent all loss of liquid, for instance when the entire plant stands upside down or when the aircraft upon which the said plant is mounted osciilates or is inclined.
- the inlet end of the pump is connected by a pipe 5 to the top of the said tank thus insuring the automatic priming of the pump after the whole system has been turned upside down, since any amount of air that has been trapped in the pump escapes through pipe 5 and is replaced by a corresponding amount of liquid present in the lower portion 0! said pipe 5, connected to the inlet side of the pump.
- the pump may be placed at I (Fig. .la) in imme- .is separated into two chambers 8 and 9 by a piston III, which is guided, for instance, by a guide Ii. Between the-piston l0 and the cylinder 1 are provided one or more packing pieces I2,
- the bypass may be of any known type, and in the construction represented in the figure, it comprises a piston is which is urged to the right by a spring 28.
- the chamber 8 of the storage device 1' is connected by a pipe 28 (provided with a pressuregauge 28), and by branch pipes 8I8i'- 8i" to distributers 28-28'28" which control the delivery of compressed'liquid to one or'more Jacks 21-21 21' and 21", respectively.
- the distributors also direct fluid to pipes 28, 28 and 28, while return is permitted through 28, 28, and 28* respectively to pipes 28, 28', and 28" leading to return pipe II, as shown by Fig. 1. Or the fluid may be directed to pipes 28 28' and 28' while return is permitted through 28*, 28 and 28, respectively.
- the jacks 21'-21, 21' 21" serve to actuate any element which is to be moved. For instance, the jacks 21-21 may be used to lift the landing gear of an aeroplane, the jack 21' may control the body flaps, and the jack 21" may operate the cooling radiators 28 which can extend more or less out of the fuselage II.
- the operation of the said plant is as follows:
- the pump withdraws liquid through the pipe 2 from the tank 8 and delivers it through the pipe 8 into the chamber 8 of the storage device 1. Thisdelivery continues up to the moment where the maximum pressure is attained. As soon as this maximum has been reached, the by-pass short-circuits'the pump.
- the pilot has at any time a reserve supply of compressed liquid contained in the-said storage device, and hence he may at any time, by operating one of the distributers 2828'28", act in the desired direction upon any of the jacks 21-21, 21', 21", and in this manner upon the parts to be displaced.
- the storage device 1 will be cut off from the upstream part which is under the pressure of the plant, so that a breakage of one of the pipes 2 or 8 will not deprive the pilot of the reserve supply of compressed liquid, and thus will be sumcient to provide for all desired operations for a safe landing on ground or on water.
- Fig. 2 represents a modification in which the delivery pipe 8 of the pump I, forwardly of the by-pass l8, comprises a branch at 88.
- " leads directly to a distributer 28" adapted to supply a Jack 21" which may perform any desired operation of any pivotally or slidably mounted elements of the aircraft.
- the control of the said distributer is insured, for instance, by a thermostat 82.
- Another branch 88 of the delivery pipe leads to two storage devices 1--1' which are disposed in parallel, and are provided with check-valves H-ll
- Each of the said storage devices is connected to one or more distributers 28-28 supplying jacks 2121'-,'21'
- the first two jacks (21-21") may serve tooperate the disappearing landing gear of an aeroplane, and jack 21' may operate a device of any kind, such as super planing device, an aerodynamic brake, a body flap, etc.
- the return of fluid to the tank 8 takes place in parallel by the pipes 2828'--28", as in the previous construction.
- the part 28"21" is not provided with storage devices, but this part controls the movement of auxiliary devices, 1. e., it performs an operation which is in fact auxiliary and whose stopping will not have any serious consequences, at least for the moment.
- the jacks or other apparatus may discharge into the atmosphere or into the inlet pipe of the compressor, and thus the necessary power can be greatly reduced. This latter method which results in the use of a closed circult, will be naturally employed whenever use is made of a gas other than air.
- the plant comprises a compressor I in two stages.
- the air or other gas is for instance withdrawn at 88, compressed in a cylinder 88 and then driven through the cooling worm 88 into a second cylinder 81 in which it is again compressed.
- the compressed air or other fluid
- the compressed air is caused to flow into a storage device 1 wherefrom a portion thereof through a pipe 88 into a distributer 88; another pipe 88' leads to two storage devices 1' and 1' connected in parallel.
- Each of the storage devices 111 is provided at its lowest part, with a corresponding check-valve M-lh-ll".
- the circuit is closed, 1. e., the discharge endof the Jacks, or like devices, supplied by the storage devices, is connected to the suction pipe 84 of the compressor.
- an interinediary tank 88 is interposed between 28 and In the case of a closed circuit, this circuit will preferably contain a small quantity of oil or other liquid, which will collect at the lower points of the plant, at which points the check-valves "-10-" are located, and the said liquid will form tight hydraulic joints in these places.
- a small quantity of oil or other liquid will of course be drawn into the jacks. but this will proceed from the discharge end of the jacks to the inlet end of the compressor, and will finally arrive at the lowest points, where it can again act in its sealing capacity.
- the compressor is preferably provided with a valve 88 (Fig. 3) of any known type for the admission of air. which can be adjusted for any desired pressure, for instance slightly above the discharge pressure of the jack or Jacks.-
- , directly connected with the delivery end of the pump may lead directly to one or more distributers, without the use of a storage device in this circuit.
- a storage tank for liquid under pressure for liquid under pressure
- resilient means associated with said tank for varying the pressure therein in accordance with the amount of liquid present in said tank
- delivery means for supplying liquid under pressure for replenishing said storage tank including a circuit adapted to communicate with said storage tank for the feed of liquid thereto when the pressure in said tank is lowerthan the pressure of liquid in said feed circuit, means for limiting the pressure of the liquid supplied by said circuit to a given value, means for cutting off said storage tank from said feed circuit when the pressure in said delivery means drops below the pressure in said storage tank, and means, wholly independent of said feed circuit, for connecting said storage tank with said device to be operated.
- a storage tank for liquid under pressure for liquid under pressure
- resilient means associated with said tank for varying the pressure therein. in accordance with the amount of liquid present in said tank, a feeding tank, a pump system connected to said tank including a delivery chamber, a spring relief valve in said chamber 'for discharge of liquid therefrom, whereby the pressure in said chamber is limited to a predetermined value, a communication between said delivery chamber and said storage tank, a check valve mounted in said communi- 2.
- a storage tank for liquid under pressure a storage tank for liquid under pressure
- resilient means associated with said tank for varying thepressure therein in accordance with the amount of liquid present in said tank
- delivery means for constantly holding liquid under pressure available for replenishing said storage tank, including a circuit adapted to communicate with said storage tank for the feed of liquid thereto when the pressure in said tank is lower than the pressure of liquid in said feed circuit, means for limiting to a given value the pressure of the liquid in said feed circuit, a check valve interposed between said feed circuit and said storage tank adapted to open in the direction of said storage tank, and conduit means, wholl independent of said feedcircuit, for connecting said storage tank with said device to be operated.
- a main conduit connecting the inlet of said pump with the bottom of said tank, a supplementary conduit connecting the inlet of said pump with the top of said tank, a delivery chamber connected with the outlet of said pump, pressure relief means in said chamber for the discharge of liquid therefrom, whereby the pressure in said chamber is limited to a predetermined value, a communication between said delivery chamber and said storage tank, a checkfvalve mounted in said communication adapted to open only in the direction of said storage tank, and conduit means, wholly independent of said pump chamber and the pump conduits, for connecting said storage tank with said device to be operated.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Pressure Circuits (AREA)
Description
, J. IMERCIER Feb. 3, 1942.
PLANT FOR PNEUMATIC, HYDRAULIC, 0R LIKE FLUID CONTROL 2 Sheets-Shed 1 Filed Nov. 17, 1936 Feb. 3, 1942. J. MERCIER 2,271,826v
PLANT FOR PNEUMATIC, HYDRAULIC, 0R LIKE FLUID CONTROL Filed Nov. 17, 1956 2 Sheets-Sheet 2 J EM/ 445/705,?
Patented Feb. 3, 1942 amaze PLANT FOB PNEUMATIC, HYDRAULIC, B
LIKE FLUID CONTROL Jean Mercier, Nenilly-sur-Seine, France Application November 11, ms, Serial No. 111,223 In France November 27, 1935 Claims. (01. its-4:)
One or more tanks for the storage of the de-' livered fluid, said tank or tanks being provided with a check-valve;
Distributers tor the fluid under pressure supplied by the said storage tanks, and Jacks or like devices supplied with fluid under pressure by the distributers.
By means of the check-valve, which is located between the outlet of the pump and each of the said storage tanks the pressure prevailing in the tank may be conserved. This pressure may serve to control several times in succession the jacks or like parts which are to be displaced, notwithstanding a breakage of the pipes on the upstream side of the check-valve or a breakdown of the pump or a breakdown of the motor which drives the pump.
If necessary, one or more distributers can be connected directly with the delivery end of the pump, without being fed by said storage tank or According to another feature of the invention,
the pump comprises a pipe for the evacuation of air and for re-priming, said pipe connecting the intake end of the pump to the top of the feeding tank, which latter is in tree connection with the atmosphere.
Instead of using a pipe for evacuation of air, use can be made of a submerged pump, i. e., a pump located in immediate proximity to the aforesaid tank to which it is connected in this In the case in which the fluid' employed is air, the Jacks may discharge into the atmosphere.
It is also feasible, in the case of air or any other gas, to use an arrangement in closed circuit, and herein the distributing valves are preferably situated at the lowest points of the circuits. A small amount of oil or other liquid is provided in these circuits and collects at these lowest points, thus insuring absolutely non-leakin: conditions for the said valves; the oil which is drawn along with the air or other gas will again enter the intake pipe of the compressor.
In the accompanying drawings, which are given solely byway of example,
Fig. l isa diagrammatic general view of the improved hydraulic or pneumatic control in accordance with the invention;
Fig. 1a shows a modification;
Fig. 2 is a like view of a modification;
Fig. 3 is a like view, showing a preferred modification of a pneumatic plant.
In the embodiment shown in Fig. 1, the plant comprises a pump I, which may be of any type. This pump withdraws the liquid, such as oil or the like, through a pipe 2, from a feeding tank 3, which is at a higher level than the pump. The
top of tank 3 is connected with the atmosphere 1 by a pipe I. This pipe, if necessary, may be provided with any usual check-valve which will prevent all loss of liquid, for instance when the entire plant stands upside down or when the aircraft upon which the said plant is mounted osciilates or is inclined. I
The inlet end of the pump is connected by a pipe 5 to the top of the said tank thus insuring the automatic priming of the pump after the whole system has been turned upside down, since any amount of air that has been trapped in the pump escapes through pipe 5 and is replaced by a corresponding amount of liquid present in the lower portion 0! said pipe 5, connected to the inlet side of the pump. 1
Instead of using the aforesaid arrangement,
the pump may be placed at I (Fig. .la) in imme- .is separated into two chambers 8 and 9 by a piston III, which is guided, for instance, by a guide Ii. Between the-piston l0 and the cylinder 1 are provided one or more packing pieces I2,
, for instance of the elastic type, and thus there pump when the delivery pressure attains a given maximum value, by directly connecting the pipe 8, by means of a pipe Hi, to the pipe l1 serving for the general return of the liquid to the top of the feeding tank 8 (a check-valve may be provided at II at the point where the pipe I1 opens into the tank). The bypass may be of any known type, and in the construction represented in the figure, it comprises a piston is which is urged to the right by a spring 28.
The chamber 8 of the storage device 1'is connected by a pipe 28 (provided with a pressuregauge 28), and by branch pipes 8I8i'- 8i" to distributers 28-28'28" which control the delivery of compressed'liquid to one or'more Jacks 21-21 21' and 21", respectively. The distributors also direct fluid to pipes 28, 28 and 28, while return is permitted through 28, 28, and 28* respectively to pipes 28, 28', and 28" leading to return pipe II, as shown by Fig. 1. Or the fluid may be directed to pipes 28 28' and 28' while return is permitted through 28*, 28 and 28, respectively. The jacks 21'-21, 21' 21" serve to actuate any element which is to be moved. For instance, the jacks 21-21 may be used to lift the landing gear of an aeroplane, the jack 21' may control the body flaps, and the jack 21" may operate the cooling radiators 28 which can extend more or less out of the fuselage II.
The operation of the said plant is as follows: The pump withdraws liquid through the pipe 2 from the tank 8 and delivers it through the pipe 8 into the chamber 8 of the storage device 1. Thisdelivery continues up to the moment where the maximum pressure is attained. As soon as this maximum has been reached, the by-pass short-circuits'the pump. Thus the pilot has at any time a reserve supply of compressed liquid contained in the-said storage device, and hence he may at any time, by operating one of the distributers 2828'28", act in the desired direction upon any of the jacks 21-21, 21', 21", and in this manner upon the parts to be displaced.
As above indicated, owing to the check-valve H, the storage device 1 will be cut off from the upstream part which is under the pressure of the plant, so that a breakage of one of the pipes 2 or 8 will not deprive the pilot of the reserve supply of compressed liquid, and thus will be sumcient to provide for all desired operations for a safe landing on ground or on water.
Obviously, the by-pass I! can be replaced by any other suitable device.
Fig. 2 represents a modification in which the delivery pipe 8 of the pump I, forwardly of the by-pass l8, comprises a branch at 88.
A branch pipe 8|" leads directly to a distributer 28" adapted to supply a Jack 21" which may perform any desired operation of any pivotally or slidably mounted elements of the aircraft. The control of the said distributer is insured, for instance, by a thermostat 82.
Another branch 88 of the delivery pipe leads to two storage devices 1--1' which are disposed in parallel, and are provided with check-valves H-ll Each of the said storage devices is connected to one or more distributers 28-28 supplying jacks 2121'-,'21' The first two jacks (21-21") may serve tooperate the disappearing landing gear of an aeroplane, and jack 21' may operate a device of any kind, such as super planing device, an aerodynamic brake, a body flap, etc. The return of fluid to the tank 8 takes place in parallel by the pipes 2828'--28", as in the previous construction.
This arrangement of several storage devices permits of'reducing the length of the different pipes and of making the various parts of the plant independent. As will be noted, the part 28"21" is not provided with storage devices, but this part controls the movement of auxiliary devices, 1. e., it performs an operation which is in fact auxiliary and whose stopping will not have any serious consequences, at least for the moment.
The aforesaid arrangements can be actuated quite as well by liquids as by air or gas.
In the case of air, the jacks or other apparatus may discharge into the atmosphere or into the inlet pipe of the compressor, and thus the necessary power can be greatly reduced. This latter method which results in the use of a closed circult, will be naturally employed whenever use is made of a gas other than air.
Whether air orother gas be used, it will be advantageous to employ preferably an arrangement analogous to the one shown in Fig. 3.
In this embodiment, the plant comprises a compressor I in two stages. The air or other gas is for instance withdrawn at 88, compressed in a cylinder 88 and then driven through the cooling worm 88 into a second cylinder 81 in which it is again compressed. From this cylinder 81 the compressed air (or other fluid) is caused to flow into a storage device 1 wherefrom a portion thereof through a pipe 88 into a distributer 88; another pipe 88' leads to two storage devices 1' and 1' connected in parallel.
Each of the storage devices 111 is provided at its lowest part, with a corresponding check-valve M-lh-ll".
Preferably the circuit is closed, 1. e., the discharge endof the Jacks, or like devices, supplied by the storage devices, is connected to the suction pipe 84 of the compressor. Preferably an interinediary tank 88 is interposed between 28 and In the case of a closed circuit, this circuit will preferably contain a small quantity of oil or other liquid, which will collect at the lower points of the plant, at which points the check-valves "-10-" are located, and the said liquid will form tight hydraulic joints in these places. A small quantity of oil or other liquid will of course be drawn into the jacks. but this will proceed from the discharge end of the jacks to the inlet end of the compressor, and will finally arrive at the lowest points, where it can again act in its sealing capacity. I
The compressor is preferably provided with a valve 88 (Fig. 3) of any known type for the admission of air. which can be adjusted for any desired pressure, for instance slightly above the discharge pressure of the jack or Jacks.-
Obviously, as in the preceding case, one or more pipes 3|, directly connected with the delivery end of the pump, may lead directly to one or more distributers, without the use of a storage device in this circuit.
It is evident that the said invention is not limited to the embodiments herein described and represented, which are given solely by way of example. 7 i
Having now described my invention, what I claim as new and desire to secure by Letters Patent, is:
1. In a system for controlling a hydraulically operated device, the combination of a storage tank for liquid under pressure, resilient means associated with said tank for varying the pressure therein in accordance with the amount of liquid present in said tank, delivery means for supplying liquid under pressure for replenishing said storage tank, including a circuit adapted to communicate with said storage tank for the feed of liquid thereto when the pressure in said tank is lowerthan the pressure of liquid in said feed circuit, means for limiting the pressure of the liquid supplied by said circuit to a given value, means for cutting off said storage tank from said feed circuit when the pressure in said delivery means drops below the pressure in said storage tank, and means, wholly independent of said feed circuit, for connecting said storage tank with said device to be operated.
4. In a system for controlling a hydraulically operated device, the combination of a storage tank for liquid under pressure, resilient means associated with said tank for varying the pressure therein. in accordance with the amount of liquid present in said tank, a feeding tank, a pump system connected to said tank including a delivery chamber, a spring relief valve in said chamber 'for discharge of liquid therefrom, whereby the pressure in said chamber is limited to a predetermined value, a communication between said delivery chamber and said storage tank, a check valve mounted in said communi- 2. In a system for controlling a hydraulically I operated device, the combination of a storage tank for liquid under pressure, resilient means associated with said tank for varying thepressure therein in accordance with the amount of liquid present in said tank, delivery means for constantly holding liquid under pressure available for replenishing said storage tank, including a circuit adapted to communicate with said storage tank for the feed of liquid thereto when the pressure in said tank is lower than the pressure of liquid in said feed circuit, means for limiting to a given value the pressure of the liquid in said feed circuit, a check valve interposed between said feed circuit and said storage tank adapted to open in the direction of said storage tank, and conduit means, wholl independent of said feedcircuit, for connecting said storage tank with said device to be operated.
3. In a system for controlling a hydraulically operated device, the combination of a storage tank for liquid under pressure, resilient means cation adapted to open only in the direction of said storage tank, and conduit means, wholly independent of said feed delivery chamber and said pump system, for connecting said storage tank with the above mentioned device to be operated.
5. In a system for controlling a hydraulically operated device, the combination of a storage tank for liquid under pressure, resilient means associated with said tank for varying the pressure therein in accordance with the amount of liquid present in saidtank, a feeding tank, a
' pump, a main conduit connecting the inlet of said pump with the bottom of said tank, a supplementary conduit connecting the inlet of said pump with the top of said tank, a delivery chamber connected with the outlet of said pump, pressure relief means in said chamber for the discharge of liquid therefrom, whereby the pressure in said chamber is limited to a predetermined value, a communication between said delivery chamber and said storage tank, a checkfvalve mounted in said communication adapted to open only in the direction of said storage tank, and conduit means, wholly independent of said pump chamber and the pump conduits, for connecting said storage tank with said device to be operated.
JEAN MERCIER.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2271826X | 1935-11-27 |
Publications (1)
Publication Number | Publication Date |
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US2271826A true US2271826A (en) | 1942-02-03 |
Family
ID=9684827
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11122336 Expired - Lifetime US2271826A (en) | 1935-11-27 | 1936-11-17 | Plant for pneumatic, hydraulic, or like fluid control |
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US (1) | US2271826A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2436544A (en) * | 1942-08-20 | 1948-02-24 | Beacham Thomas Edward | Control gear for hydraulic pumps |
US2645183A (en) * | 1952-02-18 | 1953-07-14 | John B Parsons | Starter motor-driven hydraulic pump |
US2724335A (en) * | 1951-12-14 | 1955-11-22 | Eaton Mfg Co | Pumping unit with flow director |
US2752853A (en) * | 1951-12-14 | 1956-07-03 | Eaton Mfg Co | Rotary pump with flow control valves |
-
1936
- 1936-11-17 US US11122336 patent/US2271826A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2436544A (en) * | 1942-08-20 | 1948-02-24 | Beacham Thomas Edward | Control gear for hydraulic pumps |
US2724335A (en) * | 1951-12-14 | 1955-11-22 | Eaton Mfg Co | Pumping unit with flow director |
US2752853A (en) * | 1951-12-14 | 1956-07-03 | Eaton Mfg Co | Rotary pump with flow control valves |
US2645183A (en) * | 1952-02-18 | 1953-07-14 | John B Parsons | Starter motor-driven hydraulic pump |
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