US3447477A - Power transmission - Google Patents

Power transmission Download PDF

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Publication number
US3447477A
US3447477A US648161A US3447477DA US3447477A US 3447477 A US3447477 A US 3447477A US 648161 A US648161 A US 648161A US 3447477D A US3447477D A US 3447477DA US 3447477 A US3447477 A US 3447477A
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Prior art keywords
vane
pressure
rotor
vanes
track
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US648161A
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English (en)
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Raymond B Pettibone
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Vickers Inc
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Sperry Rand Corp
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Assigned to SPERRY CORPORATION reassignment SPERRY CORPORATION CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SPERRY RAND CORPORATION
Assigned to VICKERS, INCORPORATED reassignment VICKERS, INCORPORATED ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: SPERRY CORPORATION A DE CORP.
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Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00—Rotary-piston machines or pumps
    • F04C2/30—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C2/3441—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
    • F04C2/3445—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation the vanes having the form of rollers, slippers or the like

Definitions

  • a fluid energy translating device of the sliding vane type having a stator with high pressure and low pressure passages and a vane track with a rotor rotatably mounted within the track and encased between two cheek plates; the rotor having a plurality of radial stepped slots with a vane and pivotal thrust member assembly slidably mounted therein and which form separate expansible pressure'chambers in each slot which, when filled with a pressure fluid, will provide an outward force for maintaining the vanes in contact with the vane track.
  • a pressure porting arrangement in each cheek plate which permits high pressure fluid to enter, from both sides of the rotor, the expansible pressure chambers in those slots associated with the vanes which are traversing the low pressure passages of the device; the same expansible chambers exhausting fluid into a blind port in each cheek plate forcing fluid to flow into the running clearance between the rotor and cheek plate faces when the vanes are traversing the high pressure passages of the device for creating a pressure in the same chambers greater than that existent in the high pressure passages resulting in a favorable unbalanced outward force for maintaining the vanes in contact with the vane track and for minimizing rotor-cheek plate contact by equalizing the pressure in the running clearance between the rotor and cheek plate faces.
  • This invention relates to power transmissions and is particularly applicable to those of the type comprising two or more fluid pressure energy translating devices, one of which may function as a pump and the other as a fluid motor. More particularly, this invention relates to an improvement in sliding vane type pumps and motors such as illustrated in the patent to Harry F. Vickers No. 1,989,900.
  • Still other types of devices have been designed to provide a proper unbalanced condition to meet the requirements of a very high speed and pressure operation. This is. accomplished by having an intermediate pressure chamber associated with a relatively smaller pressure effective surface on each vane in addition to the chambers associated with the inner ends of the vanes, and by providing a pressure transmitting porting arrangement to both chambers such as illustrated in the patents to Duncan B. Gardiner Nos. 2,967,488 and 2,919,651.
  • This invention comprises a rotary fluid energy translating device of the sliding vane type having in combination a plurality of stepped slots and vanes with a thrust member mounted for pivotal movement between each vane and slot with means forming separate pressure chambers in each slot, one of which is associated with a pressure responsive surface on the thrust member, the other associated with a pressure responsive surface on the vane, and means forming a pressure transmitting porting arrangement to both chambers, the said surfaces being effective under pressure to urge the vanes into engagement with the track.
  • FIG. 1 is a longitudinal sectional view of a fluid energy translating device embodying a preferred form of the present invention and taken on line 1-1 of FIG. 2.
  • FIG. 2 is a sectional view taken on line 2-2 of FIG. 1.
  • FIG. 3 is a sectional view 33 of FIG. 1.
  • FIG. 4 is a partial sectional view taken on the line 44 of FIG. 3.
  • FIG. 5 is an enlarged partial sectional view of the vanes as illustrated in FIG. 2.
  • FIGURES 1, 2, and 3 there is shown a rotary fluid pump indicated by the numeral 10, the
  • housing of which comprises a cam ring section 12 sandwiched between a body section 14 having a wear plate 16 and an end cover 18, all of which are suitably connected to each other by bolts 20.
  • the body section 14 is provided with an inlet supply connection port 22 having an inlet passage 24 leading therefrom which is branched and terminates in a pair of fluid openings, one of which is shown in FIG. 1, registering with duplicate opposed fluid openings 26 and 27 extending through the wear plate 16 and which are shown in FIG. 3.
  • An outlet connection port 28 is located in the end cover 18 which leads directly from a pressure delivery chamber 30 formed in an enlarged bore 32 of the end cover 18 where a pressure plate 34 is fioatably mounted in the bore 32.
  • the pressure plate 34 and wear plate 16 are each formed with a flat surface indicated, respectively by the numerals 36 and 38 which abut opposing flat faces 40 and 42 of the cam ring 12 and provide fluid sealing engagement for the immediately adjacent faces of rotor 44 mounted within the cam ring 12.
  • the pressure plate is adapted to be urged against a portion of the flat face 40 of the cam ring 12 and in fluid sealing engagement with the rotor by pressure in the pressure chamber 30.
  • a spring 45 initially biases the pressure plate toward the rotor until pressure builds up in the pressure chamber.
  • the rotor 44 is driven by a shaft 46 provided with a seal 47, and extends from the body for connection to a prime mover, not shown.
  • the shaft is spline connected to the rotor at 48 and is rotatably mounted in bearing 50 and 52, in the body 14.
  • O-ring seals 54 and 56 prevent leakage at the juncture of the end cover 18 and the wear plate 16 with the cam ring 12 while an O-ring seal 58 4 prevents leakage at the juncture of the body 14 and the wear plate 16.
  • the inner surface of the cam ring 12 forms a cam track substantially elliptical in shape, indicated by the number 60, against which the outer tips 62 of vanes 64, the latter of which are slidably mounted in slots 66 of the rotor 44, are adapted to be maintained in contact.
  • the cam track contour and the outer periphery of the rotor define two opposed working chambers, indicated by the numerals 68 and 70, each of which, for the purposes of convenience, may be divided into a fluid inlet zone, and a fluid delivery zone.
  • the fluid inlet zones are those portions of the working chambers 68 and 70 registering with the opposed fluid inlet openings 26 and 27 in the wear plate 16.
  • the fluid delivery zones are those portions of the working chambers 68 and 70 registering respectively with opposed arculate fluid delivery ports 72 and 74 in the pressure plate 34, shown as dotted lines in FIG. 2 which are connected to the pressure chamber 30 by means of duplicate passage 75 leading therefrom, one "of which is shown in FIG. 1.
  • the fluid inlet ports 26 and 27, which extend completely through the wear plate 16, are also duplicated respectively by mirror image ports 76 and 78 in the face 36 of the pressure plate; and fluid delivery ports 72 and 74 in the pressure plate 34 are also duplicated respectively by mirror image pressure ports 80 and 82 in the face 38 of the wear plate 16 to produce filling and balance on opposite sides of the rotor.
  • the vane track 60 includes an inlet Zone ramp extend- :ing from a to b, a true arc portion extending from b to c, a delivery Zone ramp extending from c to d, and another true are portion extending from d to e.
  • the track is symmetrical about both its major and minor axes, thus each of the ramps and true arc portions from a to e are duplicated in the lower portion of the track.
  • the vanes move radially outward with respect to the rotor, and while the vane ends traverse the delivery ramps, the vanes move radially inward. In the true are portions, the vanes partake of no radial movement.
  • the inner ends of the vane slots 66 are enlarged to form with the inner ends 84 of the vane 64, enclosed undervane pressure chambers 86 which undergo cyclic contraction and expansion during rotation of the rotor.
  • a slipper 88 which, as later explained, performs the function of a thrust member is essentially a half round rod equal in length to the van width and is mounted in the vane 64 in a mating half round groove 90 which performs the function of a socket in the vane 64 for providing pivotal movement relative thereto.
  • Each slipper has a flat outer end surface 92 and a pressure responsive intermediate surface 93, the flat outer end surface being extended out from the vane for slidable abutment with a side wall 65 in each slot 66.
  • the wall 65 of each vane slot 66 is formed with a stepped portion indicated by the numeral 94 which together with the intermediate slipper surface 93, forms in each slot an enclosed intermediate expansible pressure chamber 96.
  • the intermediate chamber 96 opens exteriorly to each side face of the rotor while undergoing cyclic expansion and contraction as the rotor revolves.
  • a slipper 88a is pivotally mounted at one end in the vane 64 and at its other end is slidably abutting a wall of slot 66 in which an expansible chamber 96a is formed between an intermediate pressure responsive surface 93a and a step 94a.
  • the dual slipper vane construction will function in the same manner as the single slipper vane construction as described herein.
  • a flow path is formed connecting the high pressure side of the device to the expanding intermediate chambers.
  • the flow path is formed by providing diametrically opposed ports 98 in the face 38 of the wear plate which are adjacent to the inlet ramps and true are portions and are connected to the pressure ports 80 and 82 by drilled passages 181 and 102 and 104 (as shown in FIGURES 3 and 4).
  • the ports 98 are also duplicated by pressure ports 106 in the face 36 of the pressure plate 34 and are connected to the pressure chamber 30 by drilled passages 108.
  • the pressure chamber 30 thus forms with the pressure plate outlet or delivery ports 72 and 74 and passages 75 a continuous outlet passage leading to the outlet port and also form with the diametrically opposed ports 98 and 106 a flow path for connecting the high pressure side of the device to the expanding intermediate chambers.
  • the vanes traversing the inlet ramp 0-]; and it duplicate inlet ramp are extending causing an expansion of their associated intermediate chambers 96.
  • the intermediate chambers of the extending vanes are in communication with the diametrically opposed ports 98 and 106 during the vane extending phase and high pressure fluid will flow from ports 98 and 106 to fill these chambers.
  • the vanes, which are traversing the outlet ramp 0-11 and its duplicate outlet ramp are retracting, causing a contraction of their associated intermediate chambers 96, and the same chambers will displace pressure fluid into the diametrically opposed blind ports 110 and 112.
  • the blind ports from which fluid can flow only into the running clearance formed between the rotor side faces and the face surfaces of the opposed cheek plates 16 and 34, are adapted to create a pressure in the intermediate chambers which is greater than the pressure existent in the fluid outlet zone through which the outer ends of the vanes pass.
  • the pressure in the fluid delivery zones and the associated inner vane chambers are equal, therefore, the higher pressure produced in the intermediate chambers will result in a favorable unbalanced outward force for maintaining the vanes in contact with the vane track during the discharge phase.
  • the effective area of the exposed intermediate surface 93 of the slipper 88 is preselected to create a resultant force sufiicient to maintain the tip of the vanes in contact with the vane track during all phases in a cycle of the device, but low enough top revent excessive ring wear during the suction phase.
  • the excess fluid which is exhausted from the intermediate chamber into the blind ports during the discharge phase, will flow into the running clearance between the adjacent faces of the pressure plate, rotor, and wear plate for providing a film of fluid on both sides of the rotor.
  • the aforesaid unfavorable condition of a pressure differential across the rotor is eliminated, thus permitting the rotor to center itself between the pressure plate and the Wear plate.
  • the rotor is provided with a plurality of angular drilled passages 114, one for each vane slot, which lead from the periphery of the rotor, between the vanes to the enlarged chambers 86 at the inner end of each vane slot.
  • the outer end of each v-ane is constructed with a trailing taper 116 and a relatively small leading taper 118 to form the tip 62 which as aforementioned is adapted to contact the vane track.
  • the outer surface of the vanes comprising the tappers 116 and 118 are exposed to the pressures in the expanding and contracting intervane spaces and by means of the angular passages 114, the cyclically changing intervane pressure is conducted to the inner chambers 86.
  • the wear plate 16 is also provided with auxiliary inlet ports and 122 which are connected to the inlet passage of the body device, and the spacing between the shaft and rotor by slots 124 and 126.
  • Duplicate auxiliary inlet ports 128 and 130 are provided in the face of the pressure plate adjacent the rotor, and are connected respectively by means of slots 132 and 134 to a recess 136 in the pressure plate.
  • Inlet fluid is therefore conducted from the auxiliary inlet porting in the wear plate side of the device through the medium of the spacing between the shaft and rotor splining to the recess 136, and by means of slots 132 and 134, to the duplicate auxiliary ports 128 and 130 of the pressure plate.
  • Dowel pins 138 are utilized to provide proper alignment of the porting located in the Wear and pressure slots with the working chambers of the device.
  • the system pressure imposed on the slipper 88 forces it into contact with the vane to take up any excess or free clearance, permitting a relaxation of the vane and rotor slot machining tolerances.
  • the relative pivotal motion of the slipper 88 and vane 64 provides a mechanical seal which not only reduces the leakage between the intermediate chambers and the Working chambers, but it eliminates the need for close vane-slipper-step slot dimensions.
  • the relative pivotal motion of the slipper and vane also permits the slipper to act as a self-aligning bearing pad for compensating for vane tilt thus reducing rotor vane contact stress resulting from the aforementioned bending forces imposed on the vane.
  • Devices embodying the invention operate at much higher pressure and speeds than conventional devices of the type herebefore mentioned, yet minimizes excessive wear rate While providing utmost efiiciency and long life.
  • a rotary fluid energy translating device of the sliding vane type including low and high pressure operating passages, one of which is an inlet passage and the other an outlet passage, and a vane track;
  • a rotor having means forming a plurality of stepped slots and rotatable within the track;
  • each vane and each thrust member having a surface thereon effective under pressure to urge the vanes toward the track;
  • passage means connecting the high pressure operating passage of the device to at least one of said separate pressure chambers for aiding centrifugal force in maintaining the outer ends of the vanes in engagement with the vane track.
  • a rotary fluid energy translating device of the sliding vane type including low and high pressure operating passages, one of which is an inlet passage and the other an outlet passage, and a vane track having a low pressure and high pressure ramps;
  • a rotor having means forming a plurality of stepped slots and rotatable within the track;
  • each vane being adapted to abut the track and the intervane spaces undergoing alternate phases of expansion and contraction as the vanes traverse the vane track ramps during a cycle of the device;
  • each vane and each thrust member having a surface efiective under pressure to urge the vanes toward the track;
  • a combination as in claim 2 including a restricted flow path in said passage means connecting the high pressure passage to the said other chambers during the intervane contraction phases of the device for creating a pressure in said other chambers during said contraction phase which is greater than is existent in the high pressure passage.
  • a rotary fluid energy translating device of the sliding vane type including low and high pressure operating passages, one of which is an inlet passage and the other an outlet passage, and a vane track having a low and high pressure ramp;
  • a rotor having means forming a plurality of stepped slots and rotatable within the track;
  • each vane is adapted to abut the track and the intervane spaces undergoing alternate phases of expansion and contraction as the vanes traverse the vane track ramps during a cycle of the device;
  • each vane and each thrust member respectively have a vane end surface and a thrust member surface and each vane and each thrust member respectively form an end pressure chamber and an intermediate pressure chamber in each slot, the said surfaces being effective under pressure in said chambers to urge the outer ends of the vanes in engagement with the track;
  • a combination as in claim 4 including said plurality of slots with means forming a step in each Wall therein;
  • thrust members being mounted on opposite sides of each vane between the vane and slot wall for pivotal movement relative thereto.
  • a rotary fluid energy translating device of the sliding vane type including low and high pressure operating passages, one of which is an inlet and the other an outlet passage, and a vane track having inlet pressure and outlet pressure ramps;
  • a rotor having means forming a plurality of stepped slots and rotatable within the track;
  • each vane being adapted to abut the track and the intervane spaces undergoing alternate phases of expansion and contraction as the vanes traverse the vane track ramps during a cycle of the device;
  • each vane and each thrust member having a surface efi'ective under pressure to urge the vanes towards the track; means forming separate pressure chambers in each slot, one of which is associated with the thrust member surface, the other associated with the vane surface;
  • passage means for connecting the cyclically changing intervane pressure to only one of said separate pressure cham ers in each slot in timed relation with the expansion and contraction phases of the intervane spaces;
  • a rotary fluid energy translating device of the sliding vane type including low and high pressure operating passages, one of which is an inlet passage and the other an outlet passage, and a vane track having inlet and outlet pressure ramps;
  • a rotor having means forming a plurality of slots and rotatable within the track;
  • each vane being adapted to abut the track and the intervane spaces undergoing alternate phases of expansion and contraction as the vane traverse the vane track ramps during a cycle of the device;
  • a vane and thrust member assembly comprising:
  • a fiat vane substantially rectangular in cross section
  • a thrust member having a flat outer end surface and a half round inner end surface, the inner end surface being disposed within the vane socket for pivotal movement relative thereto, the flat outer end surface being extended beyond the flat vane surface and adapted to engage a side Wall of the slot and provide a surface effective under pressure for aiding centrifugal force is extending the vane.
  • a rotor having a plurality of substantially radial slots with parallel side walls extending from the periphery of the rotor with a step formed in a wall in each slot, each slot having an enlarged pressure chamber formed at the inner end thereof;
  • each vane having a track engaging outer end surface and an inner end surface said inner end surface being located at the pressure chamber end of the slot;
  • a thrust member having a substantially flat outer end surface, a pressure responsive intermediate surface, and a half round inner end surface the inner end surface being disposed within each vane groove for pivotal movement relative thereto, the flat outer end surface of each member being extended beyond the flat vane surfaces for slidable abutment with a side Wall of each slot to form an intermediate expansible chamber between each stepped portion of each slot and each thrust member intermediate surface, the
  • a rotor having a plurality of substantially radial slots with parallel walls extending from the periphery of the rotor with a step formed in each wall of each slot and having enlarged pressure chambers formed at the inner ends of each slot;
  • each vane having a track engaging outer end surface and an inner end surface, said inner end surface being located at the pressure chamber end of the slot;
  • a thrust member having a substantially fiat outer end surface, a pressure responsive intermediate surface and a half round inner end surface, the inner end surface being disposed within each vane groove for pivotal movement relative thereto, the flat outer end surface of each member being extended beyond the flat vane surface for slidable abutment With the side Walls of each slot to form an intermediate expansible chamber between each stepped portion of each slot, and each thrust member intermediate surface, the said intermediate chambers each opening exteriorly to at least one side of the rotor;
  • each vane slot extending from the periphery of the rotor to the inner pressure chambers of the vane slots.
  • a vane and thrust member assembly comprising: FOREIGN PATENTS a fiat vane, substantially rectangular in cross section 45 993,574 5/1965 Great Britain.
  • a thrust member having a fiat outer end surface and a half round inner end surface, the inner end surface 50 being pivotally disposed within each vane socket for pivotal movement relative thereto, and the flat outer end surface being extended beyond the flat vane sur- ROBERT M. WALKER, Primary Examiner. WILBUR J. GOODLIN, Assistant Examiner.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)
  • Hydraulic Motors (AREA)
US648161A 1967-06-22 1967-06-22 Power transmission Expired - Lifetime US3447477A (en)

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US64816167A 1967-06-22 1967-06-22

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US (1) US3447477A (enrdf_load_stackoverflow)
DE (1) DE1703485A1 (enrdf_load_stackoverflow)
FR (1) FR1562695A (enrdf_load_stackoverflow)
GB (1) GB1230137A (enrdf_load_stackoverflow)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3516768A (en) * 1968-11-01 1970-06-23 Sperry Rand Corp Power transmission
US3516767A (en) * 1968-11-14 1970-06-23 Sperry Rand Corp Power transmission
US3578888A (en) * 1969-04-18 1971-05-18 Abex Corp Fluid pump having internal rate of pressure gain limiting device
DE2157770A1 (de) * 1970-11-25 1972-06-08 Sperry Rand Corp., Troy, Mich. (V.St.A.) Drehschieberpumpe
US3973881A (en) * 1974-02-06 1976-08-10 Daimler-Benz Aktiengesellschaft Vane-type pump or motor with undervane fluid bias
US4498853A (en) * 1979-12-14 1985-02-12 Nippon Piston Ring Co., Ltd. Vane-type compressor
US4611977A (en) * 1982-06-18 1986-09-16 Diesel Kiki Co., Ltd. Vane compressor with vane back pressure adjustment
US4810177A (en) * 1982-06-18 1989-03-07 Diesel Kiki Co., Ltd. Vane compressor with vane back pressure adjustment
EP0363112A3 (en) * 1988-10-05 1990-07-18 Vickers, Incorporated Power transmission
US5100308A (en) * 1989-03-25 1992-03-31 Gebr. Becker Gmbh & Co. Vane pump with adjustable housing and method of assembly
US20100319654A1 (en) * 2009-06-17 2010-12-23 Hans-Peter Messmer Rotary vane engines and methods
CN102606476A (zh) * 2012-04-05 2012-07-25 王汉国 提高叶片式液压油泵工作稳定性方法
RU2739893C2 (ru) * 2018-11-30 2020-12-30 Общество с ограниченной ответственностью научно-исследовательский и проектный институт "ПЕГАЗ" Роторно-поршневая гидравлическая машина со свободными поршнями
RU2744877C2 (ru) * 2018-12-24 2021-03-16 Общество с ограниченной ответственностью научно-исследовательский и проектный институт "ПЕГАЗ" Скважинный насосный агрегат с погружным многоступенчатым насосом роторно-поршневого типа на базе гидравлической машины рыля

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1047261A (ja) * 1996-07-30 1998-02-17 Toyoda Mach Works Ltd ベーンポンプ

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US2919651A (en) * 1954-10-19 1960-01-05 Vickers Inc Power transmission
US2962973A (en) * 1958-07-23 1960-12-06 Vickers Inc Power transmission
US3081706A (en) * 1960-05-09 1963-03-19 Thompson Ramo Wooldridge Inc Slipper sealing means for a dual acting pump
GB993574A (en) * 1961-10-11 1965-05-26 Nsu Motorenwerke Ag Seal for rotary piston machine
US3261334A (en) * 1962-12-11 1966-07-19 Nsu Motorenwerke Ag Lubricating sealing structure for rotary mechanisms
US3277873A (en) * 1962-07-21 1966-10-11 Daimler Benz Ag Sealing structure
US3326454A (en) * 1964-05-09 1967-06-20 Renault Sealing segments for rotary engines

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2919651A (en) * 1954-10-19 1960-01-05 Vickers Inc Power transmission
US2962973A (en) * 1958-07-23 1960-12-06 Vickers Inc Power transmission
US3081706A (en) * 1960-05-09 1963-03-19 Thompson Ramo Wooldridge Inc Slipper sealing means for a dual acting pump
GB993574A (en) * 1961-10-11 1965-05-26 Nsu Motorenwerke Ag Seal for rotary piston machine
US3277873A (en) * 1962-07-21 1966-10-11 Daimler Benz Ag Sealing structure
US3261334A (en) * 1962-12-11 1966-07-19 Nsu Motorenwerke Ag Lubricating sealing structure for rotary mechanisms
US3326454A (en) * 1964-05-09 1967-06-20 Renault Sealing segments for rotary engines

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3516768A (en) * 1968-11-01 1970-06-23 Sperry Rand Corp Power transmission
US3516767A (en) * 1968-11-14 1970-06-23 Sperry Rand Corp Power transmission
US3578888A (en) * 1969-04-18 1971-05-18 Abex Corp Fluid pump having internal rate of pressure gain limiting device
DE2157770A1 (de) * 1970-11-25 1972-06-08 Sperry Rand Corp., Troy, Mich. (V.St.A.) Drehschieberpumpe
US3973881A (en) * 1974-02-06 1976-08-10 Daimler-Benz Aktiengesellschaft Vane-type pump or motor with undervane fluid bias
US4498853A (en) * 1979-12-14 1985-02-12 Nippon Piston Ring Co., Ltd. Vane-type compressor
US4611977A (en) * 1982-06-18 1986-09-16 Diesel Kiki Co., Ltd. Vane compressor with vane back pressure adjustment
US4717321A (en) * 1982-06-18 1988-01-05 Diesel Kiki Co., Ltd. Vane compressor with vane back pressure adjustment
US4810177A (en) * 1982-06-18 1989-03-07 Diesel Kiki Co., Ltd. Vane compressor with vane back pressure adjustment
EP0363112A3 (en) * 1988-10-05 1990-07-18 Vickers, Incorporated Power transmission
US5100308A (en) * 1989-03-25 1992-03-31 Gebr. Becker Gmbh & Co. Vane pump with adjustable housing and method of assembly
US20100319654A1 (en) * 2009-06-17 2010-12-23 Hans-Peter Messmer Rotary vane engines and methods
CN102606476A (zh) * 2012-04-05 2012-07-25 王汉国 提高叶片式液压油泵工作稳定性方法
RU2739893C2 (ru) * 2018-11-30 2020-12-30 Общество с ограниченной ответственностью научно-исследовательский и проектный институт "ПЕГАЗ" Роторно-поршневая гидравлическая машина со свободными поршнями
RU2744877C2 (ru) * 2018-12-24 2021-03-16 Общество с ограниченной ответственностью научно-исследовательский и проектный институт "ПЕГАЗ" Скважинный насосный агрегат с погружным многоступенчатым насосом роторно-поршневого типа на базе гидравлической машины рыля

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FR1562695A (enrdf_load_stackoverflow) 1969-04-04
GB1230137A (enrdf_load_stackoverflow) 1971-04-28
DE1703485A1 (de) 1971-11-25

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