US3734638A - Flexible vane turbine pump - Google Patents

Flexible vane turbine pump Download PDF

Info

Publication number
US3734638A
US3734638A US00087456A US3734638DA US3734638A US 3734638 A US3734638 A US 3734638A US 00087456 A US00087456 A US 00087456A US 3734638D A US3734638D A US 3734638DA US 3734638 A US3734638 A US 3734638A
Authority
US
United States
Prior art keywords
impeller
pump chamber
pump
vanes
flow
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
US00087456A
Inventor
V Ebsary
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.)
Rockwell Manufacturing Co
Original Assignee
Rockwell Manufacturing Co
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 Rockwell Manufacturing Co filed Critical Rockwell Manufacturing Co
Application granted granted Critical
Publication of US3734638A publication Critical patent/US3734638A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/18Rotors
    • F04D29/188Rotors specially for regenerative pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C5/00Rotary-piston machines or pumps with the working-chamber walls at least partly resiliently deformable
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D5/00Pumps with circumferential or transverse flow
    • F04D5/002Regenerative pumps

Definitions

  • ABSTRACT A turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet in the case communicating with the pump chamber, a rotor drive shaft extending axially into the case, an impeller on the drive shaft incorporating flow vanes made of an elastomeric material.
  • the present invention has been devised to produce a flexible vane regenerative turbine pump which:
  • a. is self priming when provided with a head of liquid.
  • d. can operate at higher speeds cavitation free e. can pass solids in suspension within the impeller cell structure.
  • FIG. 1 is a longitudinal sectional elevation of a pump body incorporating impeller vanes and means to provide a head of liquid for self priming.
  • FIG. 2 is an end sectional elevation of the embodiment illustrated in FIG. 1.
  • FIG. 3 is a longitudinal sectional elevation of a pump body wherein the impeller vanes project radially from the hub and impeller vane deflecting means is mounted in the outer wall of the pump chamber and functions also as an impeller seal between the outlet and inlet.
  • FIG. 4 is an end sectional elevation of the embodiment illustrated in FIG. 3.
  • FIG. 5 is a fragmentary sectional plan wherein the impeller vanes project laterally on each side of the impeller and the deflecting means are positioned to coact therewith.
  • FIG. 6 is a view similar to FIG. 5 wherein the impeller vanes are on one side of the impeller only.
  • FIG. 7 illustrates one form of means for actuating the deflecting means of FIG. 5.
  • this turbine pump comprises an internally cylindrical case 1 having an annular pump chamber 2 with an inlet port 3 and an outlet port 4 in the outer wall of the pump chamber both having means (not shown) for connecting to supply and delivery pipes.
  • an air discharge liquid separation vessel 5 In the outlet port 4 there is an air discharge liquid separation vessel 5. It is connected by port 6 to an ancillary reservoir 7 adjoining the pump chamber dimensioned to hold sufficient liquid to create a liquid seal within the pump chamber for a priming operation. Syphonic return flow is prevented by a bleed port 8.
  • a rotor drive shaft 9 extends axially into the case 1 through a gland l0 and a hub 11 on the shaft has an impeller l2 thereon.
  • the impeller incorporates an array of vanes 13 made of an elastomeric material. There is a flow clearance between the vanes and all parts of the pump chamber except between the inlet and outlet ports where a working clearance only is provided.
  • FIGS. 3 and 4 the vanes 13 project radially and have a degree of flexibility which will permit deflection between the inlet and outlet ports in a priming operation.
  • a flexible plate 14 is secured to the peripheral wall of the pump chamber 2 between the inlet and outlet ports 3-4 as indicated at 15. It is adapted to be deflected by a spring retracted plunger 16 slidable in a hollow boss 17 on the pump case 1. There is a leak port 18 through the plate 14 and a complementary exhaust port 19 in the plunger 16 which is only open to the pump chamber and to atmosphere when the plunger is depressed as shown in FIG. 4.
  • vanes 13a and 13b project laterally on each side of the impeller 12 and the pump chamber 2 is shaped to accommodate the vanes and to provide the flow clearance.
  • Two flexible plates 14a and 14b are mounted on opposite side walls of the pump chamber 2 juxtaposed the inlet and outlet ports 3-4. They are adapted to be deflected by two spring retracted plungers 16a and 16b. Ports such as 18 and 19 are incorporated.
  • FIG. 7 One means of depressing the plungers 16a and 16b in unison is illustrated in FIG. 7.
  • the means comprise a U shaped member 20 pivotally mounted as at 21 on a bracket 22.
  • the member 20 has its limbs 23 shaped to engage and depress the plungers 16a and 16b. It is provided with an operating handle 24.
  • vanes project laterally only on one side of the impeller 12 and only one flexible plate and actuating plunger 16c is required.
  • the pump is self priming as long as the reservoir contains sufficient liquid to substantially immerse the vanes 13.
  • Pressure control is dependent on the type of elastomeric impeller vane employed. For low pressure duties where immediate cessation of flow is required without stopping the pump a more flexible impeller vane is used thereby allowing flow between the outlet and inlet ports by vane deflection due to back pressure. This means of internal by-pass of liquid dispenses with a mechanical by-pass.
  • the working clearance between the impeller vanes and the walls of the pump chamber at the position, of the inlet and outlet ports is achieved by the flexible plates 14a, b and c.
  • Other and/or supplementary means may be adopted or included.
  • the wall or walls of the pump chamber may have a projection or projections formed thereon having provision to accommodate vane deflecting means which in such a construction may be a spring retracted plunger or plungers of the type described but having a tapered nosing to contact the vanes.
  • the pump is primed in a starting operation by deflecting the impeller vanes to substantially decrease the vane cell volume when passing between the outlet and inlet ports.
  • the vane cell volume is restored to normal after passing the deflecting means thereby creating a suction efiect in juxtaposition to the inlet port.
  • fluid acceleration within the pump is created by a pressure differential generated between the walls of the pump chamber and the impeller vane cells.
  • As the liquid velocity within the pump chamber is lower than within the impeller vane cells secondary and continually increasing circulation is induced. This progressive energy cycle escalates or regenerates" until the fluid is ejected through the outlet port.
  • Regenerative pumps are advantageous for handling small fluid quantities against high operating head conditions. The shape and arrangement of the vanes and the cell capacity between them is determined according to work the pump is required to perform.
  • F168. 3 to 6 means are incorporated such as a non return valve 25 to prevent back flow through the outlet port 4.
  • the flexible vane impeller allows for priming deflection if required and normal running without continuous running deflection when compared with the conventional continuous flexing impeller pump, thereby eliminating fatigue and ultimate failure as encountered with pumps as constructed hitherto.
  • a turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet port in the case communicating with g the pump chamber, a rotor drive shaft extending axially into the case, an air discharge liquid separation vessel in the outlet port and connected by a port to an ancillary reservoir connected to the pump chamber adapted to create a liquid seal in the pump chamber for a priming operation, an impeller on the drive shaft including flow vanes made of an elastomeric material, said pump chamber being dimensioned to provide a flow clearance between the flow vanes and all parts of the chamber except between the inlet and outlet where a working clearance only is provided, retractably means in the pump chamber between the inlet and outlet to deflect the vanes during a priming operation, said means comprising at least one flexible plate having a leak port and at least one spring retracted plunger also having a leak port, each said leak ports opening to the atmosphere when the plungers are depressed, said vanes returning to a normal non-deflected position when said plungers are
  • a turbine pump as claimed in claim 1 including means to prevent back flow through the outlet port.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet in the case communicating with the pump chamber, a rotor drive shaft extending axially into the case, an impeller on the drive shaft incorporating flow vanes made of an elastomeric material.

Description

Elnite Ehsary Sttes 1 May 22, 1973 [73] Assig [21] Appl.
Inventor:
Filed:
FLEXIBLE VANE TU INE PUMP Vivan Richard Ebsary, Palm Beach,
New South Wales, Australia Rockwell Manufacturing Company,
Pittsburgh, Pa.
Nov. 6, 1970 US. Cl. ..4l5/14l, 415/148, 415/213 T Int. Cl ..F0ld 17/12, F03b 3/12, F04d 15/00 Field of Search 418/127-129, 153-156;
415/53 T, 140,141, 146,148,199 T, 213 T References Cited UNITED STATES PATENTS Baker ..4l5/213 T Worst La Bour..... Ferguson ..415/53 T Primary ExaminerWilliam L. Freeh Assistant Examiner-John J. Vrablik Attorney-Emory L. Groff and Emory L. Groff, Jr.
[57] ABSTRACT A turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet in the case communicating with the pump chamber, a rotor drive shaft extending axially into the case, an impeller on the drive shaft incorporating flow vanes made of an elastomeric material.
5 Claims, 7 Drawing Figures PATENTEDRAYZZIHYS SHEET 1 BF 3 MEL/ff V w/w X. E3 509 FLEXIBLE VANE TURBINE PUMP Flexible vane pumps as constructed hitherto are generally not as efficient as they should be theoretically, the principal reasons being:
1. High starting torque when dry.
2. Permanent deformation of the rotor impeller vane when standing idle for lengthy periods.
3. Constant rotor impeller vane flexing when pump is operating inducing premature fatigue.
4. Damage to rotor impeller vane when operated dry beyond a minimal time.
The present invention has been devised to produce a flexible vane regenerative turbine pump which:
a. is self priming when provided with a head of liquid.
b. incorporates means which can be actuated to prime in a dry start without creating a high starting torque c. when pumping does not subject the rotor impeller vane to excessive contact flexing and promotes long life without fatigue failure.
d. can operate at higher speeds cavitation free e. can pass solids in suspension within the impeller cell structure.
f. incorporate means to expel displaced air or vapors during priming and will eject entrained air or gas when pumping.
Embodiments of the invention are described with reference to the annexed schematic drawings wherein:
FIG. 1 is a longitudinal sectional elevation of a pump body incorporating impeller vanes and means to provide a head of liquid for self priming.
FIG. 2 is an end sectional elevation of the embodiment illustrated in FIG. 1.
FIG. 3 is a longitudinal sectional elevation of a pump body wherein the impeller vanes project radially from the hub and impeller vane deflecting means is mounted in the outer wall of the pump chamber and functions also as an impeller seal between the outlet and inlet.
FIG. 4 is an end sectional elevation of the embodiment illustrated in FIG. 3.
FIG. 5 is a fragmentary sectional plan wherein the impeller vanes project laterally on each side of the impeller and the deflecting means are positioned to coact therewith.
FIG. 6 is a view similar to FIG. 5 wherein the impeller vanes are on one side of the impeller only.
FIG. 7 illustrates one form of means for actuating the deflecting means of FIG. 5.
Referring to FIGS. 1 and 2 this turbine pump comprises an internally cylindrical case 1 having an annular pump chamber 2 with an inlet port 3 and an outlet port 4 in the outer wall of the pump chamber both having means (not shown) for connecting to supply and delivery pipes.
In the outlet port 4 there is an air discharge liquid separation vessel 5. It is connected by port 6 to an ancillary reservoir 7 adjoining the pump chamber dimensioned to hold sufficient liquid to create a liquid seal within the pump chamber for a priming operation. Syphonic return flow is prevented by a bleed port 8.
A rotor drive shaft 9 extends axially into the case 1 through a gland l0 and a hub 11 on the shaft has an impeller l2 thereon. The impeller incorporates an array of vanes 13 made of an elastomeric material. There is a flow clearance between the vanes and all parts of the pump chamber except between the inlet and outlet ports where a working clearance only is provided.
In FIGS. 3 and 4 the vanes 13 project radially and have a degree of flexibility which will permit deflection between the inlet and outlet ports in a priming operation. A flexible plate 14 is secured to the peripheral wall of the pump chamber 2 between the inlet and outlet ports 3-4 as indicated at 15. It is adapted to be deflected by a spring retracted plunger 16 slidable in a hollow boss 17 on the pump case 1. There is a leak port 18 through the plate 14 and a complementary exhaust port 19 in the plunger 16 which is only open to the pump chamber and to atmosphere when the plunger is depressed as shown in FIG. 4.
In FIG. 5 the vanes 13a and 13b project laterally on each side of the impeller 12 and the pump chamber 2 is shaped to accommodate the vanes and to provide the flow clearance. Two flexible plates 14a and 14b are mounted on opposite side walls of the pump chamber 2 juxtaposed the inlet and outlet ports 3-4. They are adapted to be deflected by two spring retracted plungers 16a and 16b. Ports such as 18 and 19 are incorporated.
One means of depressing the plungers 16a and 16b in unison is illustrated in FIG. 7. The means comprise a U shaped member 20 pivotally mounted as at 21 on a bracket 22. The member 20 has its limbs 23 shaped to engage and depress the plungers 16a and 16b. It is provided with an operating handle 24.
In FIG. 6 the vanes project laterally only on one side of the impeller 12 and only one flexible plate and actuating plunger 16c is required.
In the embodiment described in FIGS. 1 and 2 the pump is self priming as long as the reservoir contains sufficient liquid to substantially immerse the vanes 13.
The partial circulatory effect of this liquid seal entrains, traps and ejects air drawn from the suction line until a pressure drop sufficient to induce flow from the connected source occurs.
Once normal flow is established the reserve reservoir is automatically replenished with liquid.
Pressure control is dependent on the type of elastomeric impeller vane employed. For low pressure duties where immediate cessation of flow is required without stopping the pump a more flexible impeller vane is used thereby allowing flow between the outlet and inlet ports by vane deflection due to back pressure. This means of internal by-pass of liquid dispenses with a mechanical by-pass.
In FIGS. 3 to 6 the working clearance between the impeller vanes and the walls of the pump chamber at the position, of the inlet and outlet ports is achieved by the flexible plates 14a, b and c. Other and/or supplementary means may be adopted or included. For example, the wall or walls of the pump chamber may have a projection or projections formed thereon having provision to accommodate vane deflecting means which in such a construction may be a spring retracted plunger or plungers of the type described but having a tapered nosing to contact the vanes.
In FIGS. 3 to 6 the pump is primed in a starting operation by deflecting the impeller vanes to substantially decrease the vane cell volume when passing between the outlet and inlet ports. The vane cell volume is restored to normal after passing the deflecting means thereby creating a suction efiect in juxtaposition to the inlet port. When pumping, fluid acceleration within the pump is created by a pressure differential generated between the walls of the pump chamber and the impeller vane cells. As the liquid velocity within the pump chamber is lower than within the impeller vane cells secondary and continually increasing circulation is induced. This progressive energy cycle escalates or regenerates" until the fluid is ejected through the outlet port. Regenerative pumps are advantageous for handling small fluid quantities against high operating head conditions. The shape and arrangement of the vanes and the cell capacity between them is determined according to work the pump is required to perform.
in F168. 3 to 6 means are incorporated such as a non return valve 25 to prevent back flow through the outlet port 4.
In all forms the flexible vane impeller allows for priming deflection if required and normal running without continuous running deflection when compared with the conventional continuous flexing impeller pump, thereby eliminating fatigue and ultimate failure as encountered with pumps as constructed hitherto.
The claims defining the invention are as follows:
1. A turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet port in the case communicating with g the pump chamber, a rotor drive shaft extending axially into the case, an air discharge liquid separation vessel in the outlet port and connected by a port to an ancillary reservoir connected to the pump chamber adapted to create a liquid seal in the pump chamber for a priming operation, an impeller on the drive shaft including flow vanes made of an elastomeric material, said pump chamber being dimensioned to provide a flow clearance between the flow vanes and all parts of the chamber except between the inlet and outlet where a working clearance only is provided, retractably means in the pump chamber between the inlet and outlet to deflect the vanes during a priming operation, said means comprising at least one flexible plate having a leak port and at least one spring retracted plunger also having a leak port, each said leak ports opening to the atmosphere when the plungers are depressed, said vanes returning to a normal non-deflected position when said plungers are restored to their non-depressed position once priming has been effected.
2. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project radially from the impeller.
3. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project laterally on each side of the impeller.
4. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project laterally on one side of the impeller.
5. A turbine pump as claimed in claim 1 including means to prevent back flow through the outlet port.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION PATENT NO. 3 734, 638
DATED May 22, 1973 INVENTOR(S) Vivan Richard Ebsary It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown beiow:
(73) Assignee: None Signed and Sealed this eleventh D Of November 1 9 75 {SEAL} A nest:
RUTH-C. M AjSON C. MWRSHALL DANN .-i!!0srmg- ()[juer ('nmmissr'um'r 01' Pulenm uml Truilcmurkx

Claims (5)

1. A turbine pump comprising an internally cylindrical case having an annular pump chamber therein, an inlet and outlet port in the case communicating with the pump chamber, a rotor drive shaft extending axially into the case, an air discharge - liquid separation vessel in the outlet port and connected by a port to an ancillary reservoir connected to the pump chamber adapted to create a liquid seal in the pump chamber for a priming operation, an impeller on the drive shaft including flow vanes made of an elastomeric material, said pump chamber being dimensioned to provide a flow clearance between the flow vanes and all parts of the chamber except between the inlet and outlet where a working clearance only is provided, retractably means in the pump chamber between the inlet and outlet to deflect the vanes during a priming operation, said means comprising at least one flexible plate having a leak port and at least one spring retracted plunger also having a leak port, each said leak ports opening to the atmosphere when the plungers are depressed, said vanes returning to a normal non-deflected position when said plungers are restored to their non-depressed position once priming has been effected.
2. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project radially from the impeller.
3. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project laterally on each side of the impeller.
4. A turbine pump as claimed in claim 1 wherein the impeller is a disc and the flow vanes project laterally on one side of the impeller.
5. A turbine pump as claimed in claim 1 including means to prevent back flow through the outlet port.
US00087456A 1970-11-06 1970-11-06 Flexible vane turbine pump Expired - Lifetime US3734638A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8745670A 1970-11-06 1970-11-06

Publications (1)

Publication Number Publication Date
US3734638A true US3734638A (en) 1973-05-22

Family

ID=22205293

Family Applications (1)

Application Number Title Priority Date Filing Date
US00087456A Expired - Lifetime US3734638A (en) 1970-11-06 1970-11-06 Flexible vane turbine pump

Country Status (1)

Country Link
US (1) US3734638A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4456423A (en) * 1981-11-11 1984-06-26 Webasto-Werk W. Baier Gmbh & Co. Side channel blower
US4755105A (en) * 1986-10-27 1988-07-05 Chemcut Corporation Impeller improvement
DE4123661A1 (en) * 1991-07-17 1993-01-21 Zikeli Friedrich Dipl Ing Th Electrically driven cooling pump for vehicle IC engine - has integrated motor with two split sleeves enclosing two-part stator
US5672046A (en) * 1995-10-06 1997-09-30 Siemens Aktiengesellschaft Side-channel compressor
US6589014B1 (en) * 2002-01-15 2003-07-08 John Hawryluk Fluid-driven turbine
WO2003071137A1 (en) * 2002-02-25 2003-08-28 Rietschle Thomas Gmbh + Co. Kg Lateral channel compressor and device for machining a flange on a drive motor for a lateral channel compressor
US20030185668A1 (en) * 2002-03-26 2003-10-02 Uffelman Bradley L. Turbine fuel pump and method for calibrating
US6923618B1 (en) * 2003-09-26 2005-08-02 William Hudgens Rotary motor
WO2006029643A1 (en) * 2004-09-16 2006-03-23 Horn Gmbh & Co. Kg Hybrid pump
US20100300119A1 (en) * 2009-05-29 2010-12-02 Jung Je Heon Pump for supplying cryogenic coolant
WO2011022835A1 (en) * 2009-08-28 2011-03-03 Benn Bruce I Fluid turbine
WO2022115665A1 (en) * 2020-11-27 2022-06-02 Paul Anthony Johnson Material mover

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US763525A (en) * 1903-08-19 1904-06-28 Hugo Van Beresteyn Rotary motor.
US1489624A (en) * 1921-12-03 1924-04-08 Frank M Zottoli Turbine wheel
US1578236A (en) * 1922-03-04 1926-03-23 Bour Harry E La Centrifugal pump
US2006590A (en) * 1931-08-21 1935-07-02 Westco Pump Corp Pumping apparatus
US2217211A (en) * 1937-09-11 1940-10-08 Roots Connersville Blower Corp Rotary pump
US2604852A (en) * 1948-05-03 1952-07-29 Fairbanks Morse & Co Pump impeller
US2734457A (en) * 1956-02-14 fernstrum
US3127840A (en) * 1961-12-26 1964-04-07 Gen Electric Clothes washer with improved turbine type pump
US3191539A (en) * 1963-09-30 1965-06-29 Carter Ralph B Co Cut-water for self-priming centrifugal pumps
US3257955A (en) * 1964-02-04 1966-06-28 Gen Electric Flow control for turbine pump
US3259072A (en) * 1964-10-26 1966-07-05 Gen Motors Corp Rotary fuel pump

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2734457A (en) * 1956-02-14 fernstrum
US763525A (en) * 1903-08-19 1904-06-28 Hugo Van Beresteyn Rotary motor.
US1489624A (en) * 1921-12-03 1924-04-08 Frank M Zottoli Turbine wheel
US1578236A (en) * 1922-03-04 1926-03-23 Bour Harry E La Centrifugal pump
US2006590A (en) * 1931-08-21 1935-07-02 Westco Pump Corp Pumping apparatus
US2217211A (en) * 1937-09-11 1940-10-08 Roots Connersville Blower Corp Rotary pump
US2604852A (en) * 1948-05-03 1952-07-29 Fairbanks Morse & Co Pump impeller
US3127840A (en) * 1961-12-26 1964-04-07 Gen Electric Clothes washer with improved turbine type pump
US3191539A (en) * 1963-09-30 1965-06-29 Carter Ralph B Co Cut-water for self-priming centrifugal pumps
US3257955A (en) * 1964-02-04 1966-06-28 Gen Electric Flow control for turbine pump
US3259072A (en) * 1964-10-26 1966-07-05 Gen Motors Corp Rotary fuel pump

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4456423A (en) * 1981-11-11 1984-06-26 Webasto-Werk W. Baier Gmbh & Co. Side channel blower
US4755105A (en) * 1986-10-27 1988-07-05 Chemcut Corporation Impeller improvement
DE4123661A1 (en) * 1991-07-17 1993-01-21 Zikeli Friedrich Dipl Ing Th Electrically driven cooling pump for vehicle IC engine - has integrated motor with two split sleeves enclosing two-part stator
US5672046A (en) * 1995-10-06 1997-09-30 Siemens Aktiengesellschaft Side-channel compressor
US6589014B1 (en) * 2002-01-15 2003-07-08 John Hawryluk Fluid-driven turbine
WO2003071137A1 (en) * 2002-02-25 2003-08-28 Rietschle Thomas Gmbh + Co. Kg Lateral channel compressor and device for machining a flange on a drive motor for a lateral channel compressor
US20030185668A1 (en) * 2002-03-26 2003-10-02 Uffelman Bradley L. Turbine fuel pump and method for calibrating
US6799941B2 (en) * 2002-03-26 2004-10-05 Ti Group Automotive Systems, L.L.C. Turbine fuel pump and method for calibrating
US6923618B1 (en) * 2003-09-26 2005-08-02 William Hudgens Rotary motor
WO2006029643A1 (en) * 2004-09-16 2006-03-23 Horn Gmbh & Co. Kg Hybrid pump
US20100300119A1 (en) * 2009-05-29 2010-12-02 Jung Je Heon Pump for supplying cryogenic coolant
US9435323B2 (en) * 2009-05-29 2016-09-06 Doosan Heavy Industries & Construction Co., Ltd. Pump for supplying cryogenic coolant
WO2011022835A1 (en) * 2009-08-28 2011-03-03 Benn Bruce I Fluid turbine
WO2022115665A1 (en) * 2020-11-27 2022-06-02 Paul Anthony Johnson Material mover

Similar Documents

Publication Publication Date Title
US3734638A (en) Flexible vane turbine pump
FI101414B (en) Pump and process for separating gas from a liquid to be pumped
US4883410A (en) Fuel supply systems
US3578880A (en) Diaphragm operated priming device for centrifugal impeller pump
US3230890A (en) Centrifugal pump
US2287397A (en) Double suction liquid pump
KR930010380A (en) Pump
EP0012544B1 (en) Liquid ring pump
US3082694A (en) Self-priming centrifugal pump
US2368528A (en) Pump
CN217712948U (en) Liquid ring and fuel pump
US2224615A (en) Priming means for self-priming pumps
US3351272A (en) Vacuum pump
US3985113A (en) Primer system for rotary combustion engine
CN107762896B (en) Vacuum pump
JPS598675B2 (en) self-priming pump
GB655897A (en) Rotary tube pumps and turbines
CN219654900U (en) High suction stroke self-priming pump
JPH09100792A (en) Vertical shaft pump of suction side self-priming chamber type
US1680382A (en) Self-priming centrifugal liquid pump
US4494560A (en) Self-priming system for liquid pumps
RU2794619C1 (en) Combined monoblock pump with wet rotor
JP4663908B2 (en) Liquid ring pump
TWI698590B (en) Regenerative pump
JPS5824637B2 (en) self-priming pump