US2843049A - Resilient rotor pump or motor - Google Patents
Resilient rotor pump or motor Download PDFInfo
- Publication number
- US2843049A US2843049A US406960A US40696054A US2843049A US 2843049 A US2843049 A US 2843049A US 406960 A US406960 A US 406960A US 40696054 A US40696054 A US 40696054A US 2843049 A US2843049 A US 2843049A
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- Prior art keywords
- rotor
- shaft
- vanes
- pump
- chamber
- 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
Links
- 230000004888 barrier function Effects 0.000 description 11
- 239000007788 liquid Substances 0.000 description 8
- 238000007789 sealing Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 3
- 229910000906 Bronze Inorganic materials 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920003051 synthetic elastomer Polymers 0.000 description 1
- 239000005061 synthetic rubber Substances 0.000 description 1
Images
Classifications
-
- 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
- F04C5/00—Rotary-piston machines or pumps with the working-chamber walls at least partly resiliently deformable
Definitions
- This invention relates to hydraulic pumps and, in particular, to hydraulic pumps or motors with resilient rotors.
- One object of this invention is to provide a hydraulic pump or motor having a rotor with renewable vanes or blades, whereby any vanes or blades which show wear or breakage can be quickly and easily removed and replaced without the necessity of replacing the entire rotor.
- Another object is to provide a hydraulic pump or motor as set forth in the preceding object, wherein the rotor vanes or blades are double-ended and preferably bulbous at the opposite ends, so that one end is inserted in a correspondingly-slotted rotor hub and the other end engages the inner wall of the pump casing or the barrier between the suction and discharge ports of the pump, as the rotor rotates.
- Another object is to provide a hydraulic pump or motor having a rotor with resilient vanes or blades rotatable within a rotor chamber having suction and discharge ports separated from one another by a rotarybarrier in the form of a roller which rotates as it flexes the vanes or blades passing by it, whereby the suction and pressure sides of the pump are effectively separated from one another while at the same time the blades exert the minimum of friction, noise and wear upon the roller barrier and are flexed with the maximum ease and efficiency.
- Figure 1 is a central vertical section through a resilient rotor hydraulic pump, according to one form of the invention, taken along the line 1--1 in Figure 2, with the shaft seal in side elevation;
- Figure 2 is a vertical cross-section taken along the line 2-2 of Figure l;
- Figure 3 is a perspective view of one of the replaceable double-ended rotor vanes or blades of the pump shown in Figures 1 and 2.
- Figures 1 and 2 show a rotary hydraulic pump or motor, generally designated 10, accordingto one form of the invention, as consisting generally of a casing 12 within which a shaft 14 carrying a rotor 16 which resilient blades 18 is rotatably mounted and engageable with a rotary barrier 20 which separates the suction and pressure sides of the pump, as discussed more fully below,
- the casing 12 is in three parts, namely a hollow central or chamber part 22 and opposite end members 24 and 26 respectively.
- the central portion 22 has parallel opposite faces 28 and 30 against which the inner faces 29 and 31 respectively of the end members 24 and 26 abut, and the central part 22 is provided with bores 32 spaced at intervals around its suitably-bossed periphery for receiving bolts 34 passing through aligned holes 36 in the end member 24 and threaded into aligned threaded holes 38 in the opposite end member 26.
- the casing central, part 22 is provided,with.oppositely-projecting port bosses 40 and 42 containing threaded inlet or suction and outlet or discharge pipe connections 44 and 46 respec tively leading by way of inlet or suction and outlet or discharge passageways 48 and 50 respectively to a cylindrical rotor chamber 52, the opposite ends of which are closed by the end members 24 and 26.
- the central part 22 of the casing 12 is provided with a transverse cylindrical bore 58 within which the cylindrical barrier 20 is snugly but rotatably mounted.
- the roller thus constituting the barrier 20 may be made of any suitable material, such as steel or bronze,
- the bore 58 is so located that the cylindrical surface 59 of the roller or barrier 20 projects into the rotor chamber 52 between the inlet and outlet ports 54 and 56 ( Figure 2).
- the end member 24 is provided with a hollow extension 60 containing a cup-shaped bore or socket 62 Within which a shaft bearing 64 is mounted.
- the shaft bearing 64 is provided with a bore 66 coaxial with the center of the rotor chamber 52 and rotatably receiving the inner or dead end of the shaft 14.
- a threaded drain port 68 closed by a threaded plug 70 is provided in the lower part of the end member 24, communicating with the lower end of the rotor chamber 52 ( Figure l).
- the opposite end member 26 is provided with a tubular extension 72 terminating in a mounting flange 74 containing an annular recess 76 in which the outer race of an anti-friction bearing unit 78 is mounted, the inner race of which is mounted on the opposite or outer end of the shaft 14.
- annular boss or seat 98 Surrounding the bore 88 in the partition wall 86 is an annular boss or seat 98 engaged by an annular sealing member 100 with a wiping action, the sealing member 100 being bored as at 102 to be snugly but slidably mounted on the shaft 14 and urged against the seat 98 by a compression spring 104 engaging a flanged collar 106 surrounding and containing the sealing member 100. At its opposite end the spring 104 engages an abutment collar or disc 106a snugly and fixedly secured to the shaft 14. In this manner, even though liquid may escape from the rotor cham ber 52, it is prevented from passing outward through the bore 88 by reason of the sealing engagement of the yieldingly-urged sealing member 100 with its seat 98, as the shaft 14 rotates.
- the inner face 31 of the end member 26 of the casing 12 is provided with an annular recess 110 coaxial with the axis of the shaft 14 and receiving a pressure disc 112 flush with the inner face 31 and held in position by a locating pin 114 seated in the pressure disc 112 and end member 26 respectively ( Figure l),
- the shaft 14 passes through a central aperture 116 frorri the ante-chamber 94 to the rotor chamber 52.
- the hub 120 is in the form of a cylindrical barrel of bronze or other suitable material having a bore 122 snugly receiving the shaft 14 and having circumferentially-spaced parallel-walled slots or grooves 124 disposed around the periphery of the hub 120 and extending from end to end thereof in directions parallel to the axis of rotation of the shaft 14, which is of course the axis of the rotor shaft bore 122.
- the slots 124 at their inner ends nearest the shaft bore 122 terminate in enlargements 126' of approximately circular cross-section extending the entire lengths of the grooves.
- the grooves or slots 124 serve to snugly receive either of the correspondingly bulbous or enlarged ends 128 or 130 of the vanes 18 in such a manner as to securely but removably hold the vanes 18 therein, with the narrower neck portion 132, preferably parallel-surfaced, of each vane 18 passing snugly through the outer portion 134 of each slot or groove 124, which for convenience is made parallel-walled to fit the neck portion 132.
- the vanes or blades 18 are made from resilient or elastic deformable material, such as natural or synthetic rubber or compounds thereof, or of resilient synthetic plastic, and have opposite end surfaces 136 of dumbbell-shaped outline engageable with the inner surfaces 28 and 31 of the casing end members 24 and 26, or, more specifically, with the inner surface 138 of the pressure disc 112.
- the pump of the present invention has been found by experience to be quiet in operation, and very efficient in its action, delivering a substantially uniform flow of liquid to the point of utilization at adequate pressures, and at the same time pumping any quantities of air which may enter with the liquid, so as to prevent the pump from becoming air-locked or air-bound.
- the concentrically-mounted rotor 16 has also been found by experience to produce a higher efiiciency than an eccentn'cally-mounted rotor without the barrier 20.
- any of the rotor vanes 18 becomes cracked, broken, damaged or excessively worn, it is easily removed and replaced by unbolting the end member 24 from the central casing part 22 and pulling axially upon the vane to be removed, as with a pair of pliers or similar implement. A new vane may then be inserted in the groove or slot 124 from which the defective vane was removed, by pushing it into that groove or slot. The end member 24 is then bolted back in place, and operation of the pump resumed. If all of the vanes 18 are to be replaced, the central part 22 of the pump casing 12 may also be removed for greater accessibility of the rotor 16. Due
- the exposed enlarged edge 128 or 130 provides a wear-resisting edge which also more effectively engages the rotary barrier 59 as the pump operates. While each vane 18 may be provided with the enlargement 128 or 130 along one edge only thereof, the provision of similar enlargements 128 and 130 along both edges makes either edge of the vane insertable in the anchorage slot 124 without the necessity of previously inspecting the vanes to ascertain the proper edge to insert.
- the edge 130 may be made of a different size or cross-sectional shape from the edge 128, with a corresponding loss of the advantage of interchangeability.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Description
July 15, 1958 D. SHERWOOD ,0
RESILIENT ROTOR PUMP OR MOTOR Filed Jan. 29, 1954 1N VEN TOR.
34 Dav/M5 erwood fimthh M fys United StatcsPatent RESILIENT ROTOR PUMP OR MOTOR David Sherwood, Detroit, Mich., assignor to Sherwood Brass Works, Detroit, Mich., a corporation of Michigan This invention relates to hydraulic pumps and, in particular, to hydraulic pumps or motors with resilient rotors.
One object of this invention is to provide a hydraulic pump or motor having a rotor with renewable vanes or blades, whereby any vanes or blades which show wear or breakage can be quickly and easily removed and replaced without the necessity of replacing the entire rotor.
Another object is to provide a hydraulic pump or motor as set forth in the preceding object, wherein the rotor vanes or blades are double-ended and preferably bulbous at the opposite ends, so that one end is inserted in a correspondingly-slotted rotor hub and the other end engages the inner wall of the pump casing or the barrier between the suction and discharge ports of the pump, as the rotor rotates.
Another object is to provide a hydraulic pump or motor having a rotor with resilient vanes or blades rotatable within a rotor chamber having suction and discharge ports separated from one another by a rotarybarrier in the form of a roller which rotates as it flexes the vanes or blades passing by it, whereby the suction and pressure sides of the pump are effectively separated from one another while at the same time the blades exert the minimum of friction, noise and wear upon the roller barrier and are flexed with the maximum ease and efficiency.
Other objects and advantages of the invention will become apparent during the course of the following description of the accompanying drawing, wherein:
Figure 1 is a central vertical section through a resilient rotor hydraulic pump, according to one form of the invention, taken along the line 1--1 in Figure 2, with the shaft seal in side elevation;
Figure 2 is a vertical cross-section taken along the line 2-2 of Figure l; and
Figure 3 is a perspective view of one of the replaceable double-ended rotor vanes or blades of the pump shown in Figures 1 and 2.
Referring to the drawings in detail, Figures 1 and 2 show a rotary hydraulic pump or motor, generally designated 10, accordingto one form of the invention, as consisting generally of a casing 12 within which a shaft 14 carrying a rotor 16 which resilient blades 18 is rotatably mounted and engageable with a rotary barrier 20 which separates the suction and pressure sides of the pump, as discussed more fully below,
The casing 12 is in three parts, namely a hollow central or chamber part 22 and opposite end members 24 and 26 respectively. The central portion 22 has parallel opposite faces 28 and 30 against which the inner faces 29 and 31 respectively of the end members 24 and 26 abut, and the central part 22 is provided with bores 32 spaced at intervals around its suitably-bossed periphery for receiving bolts 34 passing through aligned holes 36 in the end member 24 and threaded into aligned threaded holes 38 in the opposite end member 26. The casing central, part 22 is provided,with.oppositely-projecting port bosses 40 and 42 containing threaded inlet or suction and outlet or discharge pipe connections 44 and 46 respec tively leading by way of inlet or suction and outlet or discharge passageways 48 and 50 respectively to a cylindrical rotor chamber 52, the opposite ends of which are closed by the end members 24 and 26.
At'a position located between the intake or suction port 54 at the junction of the inlet or suction passageway 48 with the rotor chamber 52 and the outlet or discharge port 56 similarly located at the junction of the outlet or discharge passageway 50 with the rotor chamber 52 (Figure 2), the central part 22 of the casing 12 is provided with a transverse cylindrical bore 58 within which the cylindrical barrier 20 is snugly but rotatably mounted. The roller thus constituting the barrier 20 may be made of any suitable material, such as steel or bronze,
but a non-metallic material such as that known in industry as nylon is preferred for its noise-reducing and wearresistant qualities. The bore 58 is so located that the cylindrical surface 59 of the roller or barrier 20 projects into the rotor chamber 52 between the inlet and outlet ports 54 and 56 (Figure 2).
The end member 24 is provided with a hollow extension 60 containing a cup-shaped bore or socket 62 Within which a shaft bearing 64 is mounted. The shaft bearing 64 is provided with a bore 66 coaxial with the center of the rotor chamber 52 and rotatably receiving the inner or dead end of the shaft 14. A threaded drain port 68 closed by a threaded plug 70 is provided in the lower part of the end member 24, communicating with the lower end of the rotor chamber 52 (Figure l). The opposite end member 26 is provided with a tubular extension 72 terminating in a mounting flange 74 containing an annular recess 76 in which the outer race of an anti-friction bearing unit 78 is mounted, the inner race of which is mounted on the opposite or outer end of the shaft 14. The outer end of the shaft 14 is bored as at 80 to receive a pin 82 by which a coupling 84 is drivingly connected to the shaft 14, for engagement with a source of power, such as, for example, a rotary part of an internal combustion engine. In place of the flange mounting 74, a base mounting may optionally be used, if preferred.
The tubular extension 72 between the flange 74 and the central casing part 22 is provided with a partition wall 86 containing a central bore 88 communicating at its outer end with an annular chamber 90 adjacent the anti-friction bearing 78 (Figure 1), access to which is gained through the ports or passageways 92, and a shaft seal chamber or ante-chamber 94 containing a conventional shaft seal, generally designated 96. Surrounding the bore 88 in the partition wall 86 is an annular boss or seat 98 engaged by an annular sealing member 100 with a wiping action, the sealing member 100 being bored as at 102 to be snugly but slidably mounted on the shaft 14 and urged against the seat 98 by a compression spring 104 engaging a flanged collar 106 surrounding and containing the sealing member 100. At its opposite end the spring 104 engages an abutment collar or disc 106a snugly and fixedly secured to the shaft 14. In this manner, even though liquid may escape from the rotor cham ber 52, it is prevented from passing outward through the bore 88 by reason of the sealing engagement of the yieldingly-urged sealing member 100 with its seat 98, as the shaft 14 rotates.
The inner face 31 of the end member 26 of the casing 12 is provided with an annular recess 110 coaxial with the axis of the shaft 14 and receiving a pressure disc 112 flush with the inner face 31 and held in position by a locating pin 114 seated in the pressure disc 112 and end member 26 respectively (Figure l), The shaft 14 passes through a central aperture 116 frorri the ante-chamber 94 to the rotor chamber 52.
Keyed as at 118 to the shaft 14 within the rotor chamber 52 is the hub 120 of the rotor 16. The hub 120 is in the form of a cylindrical barrel of bronze or other suitable material having a bore 122 snugly receiving the shaft 14 and having circumferentially-spaced parallel-walled slots or grooves 124 disposed around the periphery of the hub 120 and extending from end to end thereof in directions parallel to the axis of rotation of the shaft 14, which is of course the axis of the rotor shaft bore 122. The slots 124 at their inner ends nearest the shaft bore 122 terminate in enlargements 126' of approximately circular cross-section extending the entire lengths of the grooves.
The grooves or slots 124 serve to snugly receive either of the correspondingly bulbous or enlarged ends 128 or 130 of the vanes 18 in such a manner as to securely but removably hold the vanes 18 therein, with the narrower neck portion 132, preferably parallel-surfaced, of each vane 18 passing snugly through the outer portion 134 of each slot or groove 124, which for convenience is made parallel-walled to fit the neck portion 132. The vanes or blades 18 are made from resilient or elastic deformable material, such as natural or synthetic rubber or compounds thereof, or of resilient synthetic plastic, and have opposite end surfaces 136 of dumbbell-shaped outline engageable with the inner surfaces 28 and 31 of the casing end members 24 and 26, or, more specifically, with the inner surface 138 of the pressure disc 112.
In the operation of the invention, as the shaft 14 and rotor 16 are rotated clockwise in the direction of the large arrow (Figure 2), the vanes 18 are flexed successively as they arrive at the roller or barrier 59, forcing the liquid from the chamber 52 outward through the outlet,
port 56 and outlet passageway 50 into the outlet or discharge pipe (not shown) connected to the outlet pipe conection 46. The roller or barrier 20 rotates within its bore 58 as it is engaged by the ends 128 or 130 of the vanes 18, reducing friction and consequently reducing wear and noise. As the vanes continue to move in the direction of the large arrow past the inlet or suction port 54, they draw in liquid through the inlet port 54, inlet passageway 48 and inlet pipe connection 44 from the inlet pipe (not shown). This liquid travels in an arcuate path around the periphery of the rotor chamber 52, as shown by the small arrows (Figure 2). The protrusion of the roller or barrier 20 into the rotor chamber 52 and the consequent flexing of the vanes 18, effectively prevents leakage of liquid between the inlet and pressure sides of the pump 10, as represented by the inlet or suction and outlet or discharge passageways 48 and 50, and the corresponding ports 54 and 56 thereof.
The pump of the present invention has been found by experience to be quiet in operation, and very efficient in its action, delivering a substantially uniform flow of liquid to the point of utilization at adequate pressures, and at the same time pumping any quantities of air which may enter with the liquid, so as to prevent the pump from becoming air-locked or air-bound. The concentrically-mounted rotor 16 has also been found by experience to produce a higher efiiciency than an eccentn'cally-mounted rotor without the barrier 20.
If any of the rotor vanes 18 becomes cracked, broken, damaged or excessively worn, it is easily removed and replaced by unbolting the end member 24 from the central casing part 22 and pulling axially upon the vane to be removed, as with a pair of pliers or similar implement. A new vane may then be inserted in the groove or slot 124 from which the defective vane was removed, by pushing it into that groove or slot. The end member 24 is then bolted back in place, and operation of the pump resumed. If all of the vanes 18 are to be replaced, the central part 22 of the pump casing 12 may also be removed for greater accessibility of the rotor 16. Due
to the bulbous or enlarged edges 128, of the vanes 18, operation of the pump will not pull the vanes out of their grooves or slots 124. At the same time, the exposed enlarged edge 128 or 130, as the case may be, provides a wear-resisting edge which also more effectively engages the rotary barrier 59 as the pump operates. While each vane 18 may be provided with the enlargement 128 or 130 along one edge only thereof, the provision of similar enlargements 128 and 130 along both edges makes either edge of the vane insertable in the anchorage slot 124 without the necessity of previously inspecting the vanes to ascertain the proper edge to insert. Optionally, of course, the edge 130 may be made of a different size or cross-sectional shape from the edge 128, with a corresponding loss of the advantage of interchangeability.
It will be evident that the pump 10 may be used as a rotary hydraulic motor by supplying pressure fluid to the inlet passageway 48 thereof.
What I claim is:
A rotary pump or motor comprising a pump casing containing a rotor chamber having axially-spaced opposite end Walls and a peripheral Wall with a generally cylindrical internal surface thereon, said casing having spaced liquid inlet and outlet ports communicating with said chamber, a shaft rotatably mounted in said casing and extending into said chamber, said peripheral wall having a vanedeflecting member thereon projecting inwardly therefrom toward said shaft, a rotor rotatably mounted on said shaft within said chamber, said rotor having flexible vanes of elastic deformable material projecting approximately radially therefrom into engagement at their side edges with said opposite end walls and at their outer ends with said peripheral wall and vane-deflecting member, said rotor having a hub with substantially radial circumferentially-spaced recesses extending inwardly from the periphery thereof and having enlargements at their inner ends, and said vanes having their inner end portions snugly and fixedly but removably seated in said recesses and having enlarged opposite outer and inner ends of similar cross-sectional dimensions interchangeably fitting said enlargements of said recesses, the inner ends thereof being secured in said hub recess enlargements.
References Cited in the file of this patent UNITED STATES PATENTS 592,237 Closs Oct. 26, 1897 787,988 Moore Apr. 25, 1905 1,053,321 Schrock Feb. 18, 1913 1,086,488 Wachter Feb. 10, 1914 1,140,983 Campbell et al May 25, 1915 1,818,430 Ricardo Aug. 11, 1931 2,189,356 Briggs Feb. 6, 1940 2,237,451 Samuels Apr. 8, 1941 2,258,371 Wernert Oct. 7, 1941 2,293,268 Quiroz Aug. 18, 1942 2,332,411 Swanson et al. Oct. 19, 1943 2,382,839 Wuensch Aug. 14, 1945 2,404,678 Wuensch July 23, 1946 2,455,194 Rumsey Nov. 30, 1948 2,460,952 Simer et a1. Feb. 8, 1949 2,466,440 Kiekhaefer Apr. 5, 1949 2,469,510 Martinmaas, Jr. May 10, 1949 2,493,478 Dinesen et al Jan. 3, 1950 2,605,714 Hoenecke Aug. 5, 1952 2,629,331 Kerr Feb. 24, 1953 2,631,546 Dawson Mar. 17, 1953 2,636,478 Smyser Apr. 28, 1953 2,649,706 Kemp Aug. 25, 1953 2,719,001 Knuth Sept. 27, 1955 2,753,809 Garrison July 10, 1956 FOREIGN PATENTS 1,701 Great Britain "I of 1882 147,150
Germany Jan. 8, 1904
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US406960A US2843049A (en) | 1954-01-29 | 1954-01-29 | Resilient rotor pump or motor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US406960A US2843049A (en) | 1954-01-29 | 1954-01-29 | Resilient rotor pump or motor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2843049A true US2843049A (en) | 1958-07-15 |
Family
ID=23610055
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US406960A Expired - Lifetime US2843049A (en) | 1954-01-29 | 1954-01-29 | Resilient rotor pump or motor |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2843049A (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2976811A (en) * | 1958-07-28 | 1961-03-28 | Jabsco Pump Co | Impeller with independent elastomeric blades and sealing means |
| US3065705A (en) * | 1961-01-16 | 1962-11-27 | Hypro Engineering Inc | Pump with flexible bladed rotor |
| US3185239A (en) * | 1960-04-08 | 1965-05-25 | Hovercraft Dev Ltd | Vehicles for travelling over land and/or water |
| US3211103A (en) * | 1962-02-07 | 1965-10-12 | Kiekhaefer Corp | Rotary vane-type pump structure |
| US3277833A (en) * | 1964-03-16 | 1966-10-11 | Trw Inc | Hydraulic device |
| US3442221A (en) * | 1966-01-14 | 1969-05-06 | Soilserv Inc | Apparatus for precision planting of seeds |
| US3895893A (en) * | 1971-12-03 | 1975-07-22 | Manfred Sommer | Rotary piston pump |
| US4047857A (en) * | 1974-11-04 | 1977-09-13 | Arno Fischer | Rotary piston engine |
| US4060987A (en) * | 1975-05-29 | 1977-12-06 | Shlomo Chaim Fisch | Turbine drive system |
| US5584656A (en) * | 1995-06-28 | 1996-12-17 | The Scott Fetzer Company | Flexible impeller for a vacuum cleaner |
| US5642986A (en) * | 1995-06-28 | 1997-07-01 | The Scott Fetzer Company | Flexible impeller with one-piece hub |
| US6923618B1 (en) * | 2003-09-26 | 2005-08-02 | William Hudgens | Rotary motor |
| US20090200340A1 (en) * | 2008-02-08 | 2009-08-13 | Heiner Ophardt | Rotary foam pump |
| US11339782B2 (en) | 2020-06-26 | 2022-05-24 | LeimbachCausey, LLC | Multi-chamber impeller pump |
| IT202100000860A1 (en) * | 2021-01-19 | 2022-07-19 | Bruno Wolhfarth Srl | FLEXIBLE IMPELLER PUMP |
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| US2605714A (en) * | 1948-07-24 | 1952-08-05 | Clyde E Van Duser | Rotary oscillating piston pump |
| US2629331A (en) * | 1948-03-16 | 1953-02-24 | Fmc Corp | Brine pump |
| US2631546A (en) * | 1948-10-19 | 1953-03-17 | Edward A Dawson | Rotary sliding vane pump |
| US2636478A (en) * | 1948-06-21 | 1953-04-28 | F C Ripley Sr | Fluid flow measuring device |
| US2649706A (en) * | 1947-10-02 | 1953-08-25 | Philip G Kemp | Washing machine |
| US2719001A (en) * | 1952-12-20 | 1955-09-27 | Kiekhaefer Corp | Positive displacement pump with dual coacting flexible vane-type impellers |
| US2753809A (en) * | 1953-01-12 | 1956-07-10 | Jabsco Pump Co | Rotary motor or pump |
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- 1954-01-29 US US406960A patent/US2843049A/en not_active Expired - Lifetime
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| US1818430A (en) * | 1929-02-18 | 1931-08-11 | Ricardo Harry Ralph | Rotary blower, pump, or fluid pressure engine |
| US2237451A (en) * | 1937-11-09 | 1941-04-08 | Seaboard Commercial Corp | Fan construction |
| US2258371A (en) * | 1938-05-30 | 1941-10-07 | Wernert Karl | Rotary piston machine with rotor of yieldable material |
| US2189356A (en) * | 1938-08-02 | 1940-02-06 | Arthur M Briggs | Rotary pump |
| US2332411A (en) * | 1939-12-27 | 1943-10-19 | Swanson Robert Allen | Pump |
| US2293268A (en) * | 1941-04-21 | 1942-08-18 | Quiroz Francisco Angel | Rotary pump |
| US2455194A (en) * | 1943-11-10 | 1948-11-30 | Rumsey Lillian Gray | Rotary flexible vane pump |
| US2382839A (en) * | 1944-06-05 | 1945-08-14 | Wuensch Charles Erb | Centrifugal pump |
| US2404678A (en) * | 1944-06-05 | 1946-07-23 | Wuensch Charles Erb | Impeller |
| US2460952A (en) * | 1945-07-28 | 1949-02-08 | Paddle Pumps Inc | Rotary pump with elastic rotor sealing rib |
| US2469510A (en) * | 1946-10-07 | 1949-05-10 | Jr Werner W Martinmaas | Rotary vane engine |
| US2649706A (en) * | 1947-10-02 | 1953-08-25 | Philip G Kemp | Washing machine |
| US2493478A (en) * | 1948-02-24 | 1950-01-03 | Perfection Mfg Corp | Rotary pump |
| US2629331A (en) * | 1948-03-16 | 1953-02-24 | Fmc Corp | Brine pump |
| US2636478A (en) * | 1948-06-21 | 1953-04-28 | F C Ripley Sr | Fluid flow measuring device |
| US2605714A (en) * | 1948-07-24 | 1952-08-05 | Clyde E Van Duser | Rotary oscillating piston pump |
| US2466440A (en) * | 1948-07-29 | 1949-04-05 | Kiekhaefer Elmer Carl | Impeller for rotary pumps |
| US2631546A (en) * | 1948-10-19 | 1953-03-17 | Edward A Dawson | Rotary sliding vane pump |
| US2719001A (en) * | 1952-12-20 | 1955-09-27 | Kiekhaefer Corp | Positive displacement pump with dual coacting flexible vane-type impellers |
| US2753809A (en) * | 1953-01-12 | 1956-07-10 | Jabsco Pump Co | Rotary motor or pump |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2976811A (en) * | 1958-07-28 | 1961-03-28 | Jabsco Pump Co | Impeller with independent elastomeric blades and sealing means |
| US3185239A (en) * | 1960-04-08 | 1965-05-25 | Hovercraft Dev Ltd | Vehicles for travelling over land and/or water |
| US3065705A (en) * | 1961-01-16 | 1962-11-27 | Hypro Engineering Inc | Pump with flexible bladed rotor |
| US3211103A (en) * | 1962-02-07 | 1965-10-12 | Kiekhaefer Corp | Rotary vane-type pump structure |
| US3277833A (en) * | 1964-03-16 | 1966-10-11 | Trw Inc | Hydraulic device |
| US3442221A (en) * | 1966-01-14 | 1969-05-06 | Soilserv Inc | Apparatus for precision planting of seeds |
| US3895893A (en) * | 1971-12-03 | 1975-07-22 | Manfred Sommer | Rotary piston pump |
| US4047857A (en) * | 1974-11-04 | 1977-09-13 | Arno Fischer | Rotary piston engine |
| US4060987A (en) * | 1975-05-29 | 1977-12-06 | Shlomo Chaim Fisch | Turbine drive system |
| US5584656A (en) * | 1995-06-28 | 1996-12-17 | The Scott Fetzer Company | Flexible impeller for a vacuum cleaner |
| US5626461A (en) * | 1995-06-28 | 1997-05-06 | The Scott Fetzer Company | Stranded impeller |
| US5642986A (en) * | 1995-06-28 | 1997-07-01 | The Scott Fetzer Company | Flexible impeller with one-piece hub |
| US5655884A (en) * | 1995-06-28 | 1997-08-12 | The Scott Fetzer Company | Flexible impeller with overmolded hub |
| US6923618B1 (en) * | 2003-09-26 | 2005-08-02 | William Hudgens | Rotary motor |
| US20090200340A1 (en) * | 2008-02-08 | 2009-08-13 | Heiner Ophardt | Rotary foam pump |
| US8196780B2 (en) * | 2008-02-08 | 2012-06-12 | Gotohti.Com Inc | Rotary foam pump |
| US11339782B2 (en) | 2020-06-26 | 2022-05-24 | LeimbachCausey, LLC | Multi-chamber impeller pump |
| IT202100000860A1 (en) * | 2021-01-19 | 2022-07-19 | Bruno Wolhfarth Srl | FLEXIBLE IMPELLER PUMP |
| EP4030058A1 (en) | 2021-01-19 | 2022-07-20 | Bruno Wolhfarth SRL | Flexible impeller pump |
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