US2705459A - Pump - Google Patents

Pump Download PDF

Info

Publication number
US2705459A
US2705459A US194891A US19489150A US2705459A US 2705459 A US2705459 A US 2705459A US 194891 A US194891 A US 194891A US 19489150 A US19489150 A US 19489150A US 2705459 A US2705459 A US 2705459A
Authority
US
United States
Prior art keywords
rotor
casing
vanes
bore
inlet
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
US194891A
Inventor
Dunning Leighton
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.)
WILLIAM M WILSON'S SONS Inc
WILSONS SONS Inc WILLIAM M
Original Assignee
WILSONS SONS Inc WILLIAM M
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 WILSONS SONS Inc WILLIAM M filed Critical WILSONS SONS Inc WILLIAM M
Priority to US194891A priority Critical patent/US2705459A/en
Application granted granted Critical
Publication of US2705459A publication Critical patent/US2705459A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders
    • F01C21/0818Vane tracking; control therefor

Definitions

  • This invention relates to pumps. More specifically, it is concerned with rotary pumps of the type wherein fluid displacement is accomplished by vanes constrained to sliding movement in radial grooves of a rotor eccentrically disposed within a cylindric casing, and wherein the vanes are yieldingly urged outward of the rotor slots by spring pressure for maintenance of their distal edges in contact with the inner circumferential surface of said casing.
  • My invention is directed more especially toward overcoming the above mentioned drawbacks.
  • This desideratum is attained, as hereinafter more fully disclosed, through provision of means whereby the rotor and the vanes are interconnected in such a manner as to be free to adapt themselves to each other and to the casing, with their contiguous contacting surfaces in true meeting relation; and through the further provision of channelling by which some of the fluid being pumped is diverted to act with the springs as the vanes successively traverse the first half of the pumping zone within the casing, and to partially counteract the effect of the springs as the vanes are forced inward of their guide slots in the rotor by camming action with the casing in traversing the remaining half of the pumping zone, for
  • FIG. 1 is a view in longitudinal axial section of a rotary pump conveniently embodying my invention.
  • Fig. 2 is a view in cross section taken as indicated by the angled arrows II-II in Fig. 1.
  • Fig. 3 is a view corresponding to Fig. 2 with the moving parts of the pump differently positioned.
  • Fig. 4 is a perspective view of the pump rotor.
  • Fig. 5 is a broken out perspective view of one of the rotor vanes.
  • Fig. 6 shows the drive shaft of the pump in perspective
  • my improved rotary pump has a cylindric casing 10 with one of its side walls 11 integrally formed, and the other side wall 12 removably secured by screw bolts 13.
  • the side wall 12 has recesses 14 and 15 or ports in its inner face respectively in communication with diametrically-opposite inlets and outlets 16 and 17 into which flow pipes 18 and 19 are respectively screwed, each of said recesses or ports being, in this instance, approximately equal to a sextant in circumferential extent.
  • Eccentrically disposed within the casing is a hollow spoked rotor 20 of smaller diameter with its opposite ends contacting the inner faces of the side walls 11 and 12; and slidable in full length radial slots 21 of the rotor are blades, whereof there are three in this instance, respectively designated 22, 23 and 24 and having a working fit between the side walls of the casing.
  • Individual helical springs 25 yieldingly urge the blades 2224 outwardly of the rotor slots 21 for maintenance of their distal ends in pressure engagement with the inner circumferential surface of the casing 10.
  • each blade 22-24 has a centrally-located socket hole 26 to receive one end of the corresponding spring 25 with liberal circumferential clearance, the other end of the spring bearing against the head of an inserted pin 27 which latter bears in turn upon the bottom of the corresponding slot 21 of the rotor.
  • the shanks of pins 27 extend outward through the unsupported portions of the springs 25 beyond the inner ends of the blades. These pins thus serve as guides to prevent lateral flexure of the springs 25 as the blades move inwardly of the rotor slots.
  • a drive shaft 29 Extending inwardly through a stuffed bearing 28 in the removable side wall 12 of the casing 10 is a drive shaft 29, whereof the inner end is rotatively supported in a bearing boss 30 on the opposite wall 11 of said casing.
  • the shaft receiving bore of the rotor is enlarged at the ends as at 31 and has contact at the center only with the shaft 29 as at 32, said shaft being provided with diametral stud projections 33 which engage correspondingly located groove indentations 34 in the face of a small concentric recess 35 in one end of the rotor as shown in Figs. 1, 2 and 4.
  • the rotor is thus positively connected to the shaft 29 with freedom to adapt itself positionally within the casing 10 so that friction of its ends with the inner faces of said casing is reduced to a minimum and rapid wear here also effectively counteracted.
  • a spacing washer 36 surrounds the shaft 29 between the inner face of the wall 12 and the face of the recess 35 in the contiguous end of the rotor 20.
  • the bore of the rotor may be enlarged throughout as shown in Fig. 7, and the shaft 29 provided with a narrow circumferential enlargement 32a to fit within said bore and engage it only at the center; or, as shown in Fig. 8, a semi-circular lIWoodrutl) key 38 may be used to drive connect the rotor to the shaft the the region 32 and to hold it against shifting axially.
  • the recess 35 in the end of the rotor is cut somewhat deeper and radial grooves such. as shown at 34 in Fig. 4, are here omitted, the pin 33 thereby serving now only as a means to prevent the shaft 29 from being withdrawn.
  • the effect of either of these alternative constructions will obviously be the same as that described in connection with Fig. 1.
  • the vane 22 has finished pumping, and passed through the outlet neutral zone -D, and is just entering the sealing zone DA between the recesses 14 and 15 and opposite the pumping zone B-C, and vane 23 has just left the sealing zone and is entering the inlet neutral zone AB, while vane 24 has just passed the mid point E of of the pumping zone.
  • the sealing zone D-A is placed in communication with the inlet zone A-B, so that the interior of the rotor is now under condition of suction due to communication established with said inlet zone by way of the groove 37.
  • a casing having inlet and outlet ports, parallel end surfaces, and a peripheral bore whereof the surface is normal to said end surfaces; a cylindrical rotor of smaller cross section than the casing bore rotatively supported in the casing and positioned relatively close to a portion of the casing bore lying between inlet and outlet ports and at a substantially greater distance from another portion of the bore also lying between inlet and outlet ports; a plurality of symmetrically spaced radial slots extending inwardly from the periphery of the rotor; slide vanes within the rotor slots having a working fit between the end surfaces of the casing; yielding means for urging the vanes outward of the rotor slots against the bore of the casing during rotor rotation; and means for alternately communicating fluid pressure existing in the outlet port and fluid pressure existing in the inlet port simultaneously to the inner ends of all the rotor slots, the last mentioned means including a small annular recess at one end of the rotor in communication with the bottoms of the van
  • a casing having inlet and outlet ports, parallel end surfaces, and a peripheral bore whereof the surface is normal to said end surfaces; a cylindrical rotor of smaller cross section than the casing bore rotatively supported in the casing and positioned relatively close to a portion of the casing bore lying between inlet and outlet ports and at a substantially greater distance from another portion of the bore also lying between inlet and outlet ports; a plurality of symmetrically spaced radial slots extending inwardly from the periphery of the rotor; slide vanes in the rotor slots having a working fit between the end surfaces of the casing; spring means for urging the vanes outwardly of the rotor slots against the bore of the casing during rotor rotation; and means for alternately communicating fluid pressure existing in the outlet port and fluid pressure existing in the inlet port simultaneously to the inner ends of all the rotor slots, the last mentioned means including a small annular recess at one end of the rotor in communication with the bottoms of the van
  • a casing having an inlet and an outlet port, parallel end walls, and a peripheral bore the surface of which is normal to said end walls; a rotor of smaller diameter than that of the casing bore having a small circular recess at one end thereof and a plurality of equally spaced slots in communication with said recess extending inwardly from its periphery and containing slide vanes, said rotor being offset so that it is relatively close to a portion of the bore lying between the inlet and outlet ports to establish, with the vanes, a sealing zone, and at a substantially greater distance from another portion of the bore to establish, with the vanes, a pumping zone also between the inlet and outlet ports; and a channel connecting the aforesaid recess in the rotor with the sealing zone at a point substantially midway between the inlet and outlet ports, whereby passage 'of the vanes during rotor rotation, causes the vanes in the rotor slots to be alternately subjected to the inlet and outlet

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

W 5, 1955 1.. DUNNlNG 2,705,459
PUMP
Filed Nov. 9, 1950 2 s s 1 I 1716i z WITNESSES 4 INVENTOR Zezgfifmflamzmy,
Q 1 ca I BY (,i m
ATTORNEYS.
\ PUMP Filed Nov. 9, 1950 2 Sheets-Sheet 2 April 5, 1955 L. DUNNING Lu 2 o N WITNESSES 4 United States Patent PUMP Leighton Dunning, Philadelphia, Pa., assiguor to William M. Wilsons Sons, Inc., Lansdale, Pa., a corporation of Pennsylvania Application November 9, 1950, Serial No. 194,891
3 Claims. (Cl. 103-136) This invention relates to pumps. More specifically, it is concerned with rotary pumps of the type wherein fluid displacement is accomplished by vanes constrained to sliding movement in radial grooves of a rotor eccentrically disposed within a cylindric casing, and wherein the vanes are yieldingly urged outward of the rotor slots by spring pressure for maintenance of their distal edges in contact with the inner circumferential surface of said casing.
Often due to inaccuracies in machining and consequent failure of the component parts of such pumps to properly fit one into another, rapid wear takes place with consequent development of leakages between the parts and reduction in the operating efficiency of the pumps. Moreover, considerable power is required to overcome the friction between the mutually contacting surfaces of the relatively moving parts, particularly between the distal edges of the constantly spring pressed vanes and the internal circumferential surface of the casings during the operation of such pumps, which tends to reduce their efficiency.
My invention is directed more especially toward overcoming the above mentioned drawbacks. This desideratum is attained, as hereinafter more fully disclosed, through provision of means whereby the rotor and the vanes are interconnected in such a manner as to be free to adapt themselves to each other and to the casing, with their contiguous contacting surfaces in true meeting relation; and through the further provision of channelling by which some of the fluid being pumped is diverted to act with the springs as the vanes successively traverse the first half of the pumping zone within the casing, and to partially counteract the effect of the springs as the vanes are forced inward of their guide slots in the rotor by camming action with the casing in traversing the remaining half of the pumping zone, for
easement of the friction during the latter phase.
Other objects and attendant advantages will appear from the following detailed description of the attached drawings, wherein Fig. 1 is a view in longitudinal axial section of a rotary pump conveniently embodying my invention.
Fig. 2 is a view in cross section taken as indicated by the angled arrows II-II in Fig. 1.
Fig. 3 is a view corresponding to Fig. 2 with the moving parts of the pump differently positioned.
Fig. 4 is a perspective view of the pump rotor.
Fig. 5 is a broken out perspective view of one of the rotor vanes.
Fig. 6 shows the drive shaft of the pump in perspective; and
Figs. 7 and 8 are fragmentary views in section corresponding to Fig. 1 and showing two modifications.
As herein exemplified, my improved rotary pump has a cylindric casing 10 with one of its side walls 11 integrally formed, and the other side wall 12 removably secured by screw bolts 13. The side wall 12 has recesses 14 and 15 or ports in its inner face respectively in communication with diametrically-opposite inlets and outlets 16 and 17 into which flow pipes 18 and 19 are respectively screwed, each of said recesses or ports being, in this instance, approximately equal to a sextant in circumferential extent. Eccentrically disposed within the casing is a hollow spoked rotor 20 of smaller diameter with its opposite ends contacting the inner faces of the side walls 11 and 12; and slidable in full length radial slots 21 of the rotor are blades, whereof there are three in this instance, respectively designated 22, 23 and 24 and having a working fit between the side walls of the casing. Individual helical springs 25 yieldingly urge the blades 2224 outwardly of the rotor slots 21 for maintenance of their distal ends in pressure engagement with the inner circumferential surface of the casing 10. As shown, each blade 22-24 has a centrally-located socket hole 26 to receive one end of the corresponding spring 25 with liberal circumferential clearance, the other end of the spring bearing against the head of an inserted pin 27 which latter bears in turn upon the bottom of the corresponding slot 21 of the rotor. It is to be noted that the shanks of pins 27 extend outward through the unsupported portions of the springs 25 beyond the inner ends of the blades. These pins thus serve as guides to prevent lateral flexure of the springs 25 as the blades move inwardly of the rotor slots. By reason of the construction just described, it will be seen that the blades 22-24 are free to adapt themselves to the interior surfaces of the casing 10 without imposition of any restraint to their movement, whereby rapid wear of the mutually contacting surfaces is effectively prevented.
Extending inwardly through a stuffed bearing 28 in the removable side wall 12 of the casing 10 is a drive shaft 29, whereof the inner end is rotatively supported in a bearing boss 30 on the opposite wall 11 of said casing. The shaft receiving bore of the rotor is enlarged at the ends as at 31 and has contact at the center only with the shaft 29 as at 32, said shaft being provided with diametral stud projections 33 which engage correspondingly located groove indentations 34 in the face of a small concentric recess 35 in one end of the rotor as shown in Figs. 1, 2 and 4. The rotor is thus positively connected to the shaft 29 with freedom to adapt itself positionally within the casing 10 so that friction of its ends with the inner faces of said casing is reduced to a minimum and rapid wear here also effectively counteracted. As shown, a spacing washer 36 surrounds the shaft 29 between the inner face of the wall 12 and the face of the recess 35 in the contiguous end of the rotor 20. By means of a substantially radial channel groove 37 in the inner face of the side wall 12 of casing 10, flow communication is maintained between the neutral and pumping zone of the pump as and. for a purpose presently explained.
As alternatives, the bore of the rotor may be enlarged throughout as shown in Fig. 7, and the shaft 29 provided with a narrow circumferential enlargement 32a to fit within said bore and engage it only at the center; or, as shown in Fig. 8, a semi-circular lIWoodrutl) key 38 may be used to drive connect the rotor to the shaft the the region 32 and to hold it against shifting axially. In Fig. 8, the recess 35 in the end of the rotor is cut somewhat deeper and radial grooves such. as shown at 34 in Fig. 4, are here omitted, the pin 33 thereby serving now only as a means to prevent the shaft 29 from being withdrawn. The effect of either of these alternative constructions will obviously be the same as that described in connection with Fig. 1.
Operation As the rotor 20 is driven counterclockwise or in the direction of the arrows in Figs. 2, 3, fluid is constantly drawn in through the inlet 16 and discharged through the outlet 17 by passage of the vanes 2224 through the pumping zone BC between the recesses 14 and 15 to one side of the rotor in a manner characteristic of pumps of this type, said vanes being biased outward of the slots 21 by the springs 25 during their travel from the mid point of the sealing zone AD to the mid point of said pumping Zone, and being thereafter depressed until returned to the mid point of said sealing zone. Due to circumferential contact of the shaft 29 at 32 with the bore of the rotor at the center only, and to application of the spring pressure medially of the vanes 2224 in accordance with my invention, said rotor and vanes are free to position and adapt themselves to the casing. As a consequence, the end faces of the rotor 20 and the side edges of the vanes will contact evenly over their entire areas with the inner circumferential surface and side walls of the casing 10, to the advantage that the pump will operate smoothly, with avoidance of unequal wear between the mutually contacting surfaces, and with consequent assurance against the development of leakages.
In Fig. 3, the vane 22 has finished pumping, and passed through the outlet neutral zone -D, and is just entering the sealing zone DA between the recesses 14 and 15 and opposite the pumping zone B-C, and vane 23 has just left the sealing zone and is entering the inlet neutral zone AB, while vane 24 has just passed the mid point E of of the pumping zone. At the stage just described, the sealing zone D-A is placed in communication with the inlet zone A-B, so that the interior of the rotor is now under condition of suction due to communication established with said inlet zone by way of the groove 37. The suction thus set up, will tend to draw the vane 24 inward of the groove and thereby partially counteract the effect of the corresponding spring 25 as said vane is forced back by camming action with the internal circumferential wall of the casing in traversing the upper or second half of the pumping zone B-C. In Fig. 2, vane 24 has just moved into the outlet neutral zone C--D, and vane 22 passed the groove 37 with the result that the upper portion of the sealing zone AD and the interior of the rotor 20 are now under condition of pressure, whereby vane 23, which has just entered the pumping zone, will be helped out against the circumferential wall of casing 10, and thus be maintained in more effective sealing contact with said wall until it again reaches the mid point of the pumping zone B-C.
From the foregoing it will thus be seen that I have provided a rotary pump which is simple in construction; which can be relied upon to operate smoothly and efiiciently at all times, and which requires but a minimum of power to drive it.
Having thus described my invention, I claim:
1. In a rotary pump, a casing having inlet and outlet ports, parallel end surfaces, and a peripheral bore whereof the surface is normal to said end surfaces; a cylindrical rotor of smaller cross section than the casing bore rotatively supported in the casing and positioned relatively close to a portion of the casing bore lying between inlet and outlet ports and at a substantially greater distance from another portion of the bore also lying between inlet and outlet ports; a plurality of symmetrically spaced radial slots extending inwardly from the periphery of the rotor; slide vanes within the rotor slots having a working fit between the end surfaces of the casing; yielding means for urging the vanes outward of the rotor slots against the bore of the casing during rotor rotation; and means for alternately communicating fluid pressure existing in the outlet port and fluid pressure existing in the inlet port simultaneously to the inner ends of all the rotor slots, the last mentioned means including a small annular recess at one end of the rotor in communication with the bottoms of the vane slots, and a duct in one of the end walls of the casing extending from said recess to the narrow interval between the casing bore and the rotor substantially midway between the inlet and outle ports.
2. In a rotary pump, a casing having inlet and outlet ports, parallel end surfaces, and a peripheral bore whereof the surface is normal to said end surfaces; a cylindrical rotor of smaller cross section than the casing bore rotatively supported in the casing and positioned relatively close to a portion of the casing bore lying between inlet and outlet ports and at a substantially greater distance from another portion of the bore also lying between inlet and outlet ports; a plurality of symmetrically spaced radial slots extending inwardly from the periphery of the rotor; slide vanes in the rotor slots having a working fit between the end surfaces of the casing; spring means for urging the vanes outwardly of the rotor slots against the bore of the casing during rotor rotation; and means for alternately communicating fluid pressure existing in the outlet port and fluid pressure existing in the inlet port simultaneously to the inner ends of all the rotor slots, the last mentioned means including a small annular recess at one end of the rotor in communication with the bottoms of the vane slots, and a duct in one of the end walls of the casing extending from said recess to the narrow interval between the casing bore and the rotor substantially midway between the inlet and the outlet ports.
3. In a rotary pump, a casing having an inlet and an outlet port, parallel end walls, and a peripheral bore the surface of which is normal to said end walls; a rotor of smaller diameter than that of the casing bore having a small circular recess at one end thereof and a plurality of equally spaced slots in communication with said recess extending inwardly from its periphery and containing slide vanes, said rotor being offset so that it is relatively close to a portion of the bore lying between the inlet and outlet ports to establish, with the vanes, a sealing zone, and at a substantially greater distance from another portion of the bore to establish, with the vanes, a pumping zone also between the inlet and outlet ports; and a channel connecting the aforesaid recess in the rotor with the sealing zone at a point substantially midway between the inlet and outlet ports, whereby passage 'of the vanes during rotor rotation, causes the vanes in the rotor slots to be alternately subjected to the inlet and outlet pressures.
References Cited in the file of this patent UNITED STATES PATENTS 226,773 Newcomb Apr. 20, 1880 596,928 Wiedenbauer Jan. 4, 1898 999,753 Curtis Aug. 8, 1911 1,539,728 Ensign May 26, 1925 1,737,942 Pagel Dec. 3, 1929 2,255,785 Kendrick Sept. 16, 1941 2,256,459 Kendrick Sept. 16, 1941 2,412,949 Brown et a1 Dec. 24, 1946 2,498,972 Whiteley Feb. 28, 1950 2,499,763 Livermore Mar. 7, 1950 2,521,595 Miller Sept. 5, 1950 2,541,405 Chapman Feb. 13, 1951 2,588,342 Bidwell Mar. 11, 1952 2,599,927 Livermore June 10, 1952 FOREIGN PATENTS 102,792 Australia Dec. 17, 1937
US194891A 1950-11-09 1950-11-09 Pump Expired - Lifetime US2705459A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US194891A US2705459A (en) 1950-11-09 1950-11-09 Pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US194891A US2705459A (en) 1950-11-09 1950-11-09 Pump

Publications (1)

Publication Number Publication Date
US2705459A true US2705459A (en) 1955-04-05

Family

ID=22719278

Family Applications (1)

Application Number Title Priority Date Filing Date
US194891A Expired - Lifetime US2705459A (en) 1950-11-09 1950-11-09 Pump

Country Status (1)

Country Link
US (1) US2705459A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842006A (en) * 1954-06-01 1958-07-08 Deere Mfg Co Drive mechanism
US2967489A (en) * 1957-02-07 1961-01-10 Vickers Inc Power transmission
US2967488A (en) * 1957-02-07 1961-01-10 Vickers Inc Power transmission
US3037455A (en) * 1957-09-04 1962-06-05 Ford Motor Co Pumps
US3059421A (en) * 1960-05-05 1962-10-23 Thompson Ramo Wooldridge Inc Apparatus for minimizing the combustible content of exhaust gases
US3059584A (en) * 1960-01-13 1962-10-23 Sonic Eng Corp Rotary pumps and compressors
US4601647A (en) * 1983-01-18 1986-07-22 Nippon Piston Ring Co., Ltd. Hollow rotor for movable vane pumps and the like and method of making the same
US5056993A (en) * 1987-03-17 1991-10-15 Smith Roger R Liquid intake mechanism for rotary vane hydraulic motors
WO1999006710A1 (en) * 1997-07-30 1999-02-11 Delaware Capital Formation Inc. Rotary pump with hydraulic vane actuation

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US226773A (en) * 1880-04-20 Rotary pump
US596928A (en) * 1898-01-04 Alois wiedenbauer
US999753A (en) * 1909-04-10 1911-08-08 Frank J Curtis Rotary pump.
US1539728A (en) * 1924-02-23 1925-05-26 Lloyd V Reynolds Rotary pump
US1737942A (en) * 1926-11-18 1929-12-03 Pagel Rotarypump Mfg Company Rotary fluid pump or motor
US2256459A (en) * 1941-02-12 1941-09-16 Manly Corp Fluid pressure device
US2255785A (en) * 1940-09-06 1941-09-16 Manly Corp Fluid pressure device
US2412949A (en) * 1942-09-14 1946-12-24 Kyle And Company Inc Rotary engine
US2498972A (en) * 1944-12-04 1950-02-28 Frank A Whiteley Rotary pump
US2499763A (en) * 1945-07-27 1950-03-07 William T Livermore Loose slipper rotary pump
US2521595A (en) * 1947-09-03 1950-09-05 Buffalo Machinery Company Inc Split blade for air and steam turbines
US2541405A (en) * 1946-12-18 1951-02-13 Bowser Inc Rotary hand pump
US2588342A (en) * 1943-01-02 1952-03-11 Walter P Innes Jr Fluid engine
US2599927A (en) * 1944-10-06 1952-06-10 William T Livermore Slipper pump

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US226773A (en) * 1880-04-20 Rotary pump
US596928A (en) * 1898-01-04 Alois wiedenbauer
US999753A (en) * 1909-04-10 1911-08-08 Frank J Curtis Rotary pump.
US1539728A (en) * 1924-02-23 1925-05-26 Lloyd V Reynolds Rotary pump
US1737942A (en) * 1926-11-18 1929-12-03 Pagel Rotarypump Mfg Company Rotary fluid pump or motor
US2255785A (en) * 1940-09-06 1941-09-16 Manly Corp Fluid pressure device
US2256459A (en) * 1941-02-12 1941-09-16 Manly Corp Fluid pressure device
US2412949A (en) * 1942-09-14 1946-12-24 Kyle And Company Inc Rotary engine
US2588342A (en) * 1943-01-02 1952-03-11 Walter P Innes Jr Fluid engine
US2599927A (en) * 1944-10-06 1952-06-10 William T Livermore Slipper pump
US2498972A (en) * 1944-12-04 1950-02-28 Frank A Whiteley Rotary pump
US2499763A (en) * 1945-07-27 1950-03-07 William T Livermore Loose slipper rotary pump
US2541405A (en) * 1946-12-18 1951-02-13 Bowser Inc Rotary hand pump
US2521595A (en) * 1947-09-03 1950-09-05 Buffalo Machinery Company Inc Split blade for air and steam turbines

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842006A (en) * 1954-06-01 1958-07-08 Deere Mfg Co Drive mechanism
US2967489A (en) * 1957-02-07 1961-01-10 Vickers Inc Power transmission
US2967488A (en) * 1957-02-07 1961-01-10 Vickers Inc Power transmission
US3037455A (en) * 1957-09-04 1962-06-05 Ford Motor Co Pumps
US3059584A (en) * 1960-01-13 1962-10-23 Sonic Eng Corp Rotary pumps and compressors
US3059421A (en) * 1960-05-05 1962-10-23 Thompson Ramo Wooldridge Inc Apparatus for minimizing the combustible content of exhaust gases
US4601647A (en) * 1983-01-18 1986-07-22 Nippon Piston Ring Co., Ltd. Hollow rotor for movable vane pumps and the like and method of making the same
US5056993A (en) * 1987-03-17 1991-10-15 Smith Roger R Liquid intake mechanism for rotary vane hydraulic motors
WO1999006710A1 (en) * 1997-07-30 1999-02-11 Delaware Capital Formation Inc. Rotary pump with hydraulic vane actuation
AU732941B2 (en) * 1997-07-30 2001-05-03 Delaware Capital Formation, Inc. Rotary pump with hydraulic vane actuation
CN1120935C (en) * 1997-07-30 2003-09-10 特拉华资本组成公司 Rotary pump with hydraulic vane actuation

Similar Documents

Publication Publication Date Title
US2335284A (en) Rotary fluid pressure device
US3223044A (en) Three-area vane type fluid pressure energy translating devices
CA1279622C (en) Liquid ring vacuum pump
US2020611A (en) Rotary machine
US2967488A (en) Power transmission
US2725013A (en) Rotary engine
US2832293A (en) Vane pump
US2705459A (en) Pump
US3216362A (en) Flexible ring pump drive device
US2731919A (en) Prendergast
US1743977A (en) Rotary engine
US2278131A (en) Pump
US3221665A (en) Hydraulic pump or motor with hydraulic pressure-responsive vane
US2969743A (en) Rotary slidable-vane machines
US2414187A (en) Rotary compressor or supercharger
US2985110A (en) Pump construction
US4011033A (en) Positive displacement vane type rotary pump
US2373656A (en) Rotary operating machine
US3762843A (en) Van type rotary hydraulic transducer
US2487685A (en) Rotary oscillating vane pump
US3567350A (en) Power transmission
US2872873A (en) Power transmission
US2068570A (en) Rotary pump
US2410596A (en) Sliding vane engine or pump
US2225803A (en) Rotary pump or motor