US2521420A - Pump - Google Patents

Pump Download PDF

Info

Publication number
US2521420A
US2521420A US553814A US55381444A US2521420A US 2521420 A US2521420 A US 2521420A US 553814 A US553814 A US 553814A US 55381444 A US55381444 A US 55381444A US 2521420 A US2521420 A US 2521420A
Authority
US
United States
Prior art keywords
casing
pump
rotor
seal ring
washer
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
US553814A
Inventor
Donald R Spotz
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.)
Northrop Grumman Space and Mission Systems Corp
Original Assignee
Thompson Products Inc
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 Thompson Products Inc filed Critical Thompson Products Inc
Priority to US553814A priority Critical patent/US2521420A/en
Application granted granted Critical
Publication of US2521420A publication Critical patent/US2521420A/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
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C15/00Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
    • F04C15/0057Driving elements, brakes, couplings, transmission specially adapted for machines or pumps
    • F04C15/0076Fixing rotors on shafts, e.g. by clamping together hub and shaft
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/911Seal combined with nominal motion transmitting device
    • Y10S277/912Spline connection

Definitions

  • Figure 3 isl an exploded view illustrating the manner in which the pumpparts are readily removed from the pump casing without removal of the casing from the engine.
  • 9 composed of an oil-impregnated sinteredv bronze or other oil-retaining bearing material is seated in the casing
  • 9 has a chamfered central aperture

Landscapes

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

Description

Patented Sept. 5, 1950 l PUMP Donald R.V Spotz, Lakewood, Ohio, assignor to Thompson Products, Inc., Cleveland, Ohio, a
corporation of Ohio Application september 1s, 1944, serial No. 553,811
This invention relates. to a simplified positive displacement vane type pump that is inexpensive and easy to manufacture.
Specifically, the invention relates to a vane type pump for mounting on a prime mover such as an aircraft engine to be driven thereby and having a casing equipped with a readily removable end cap on-the end thereof remote from the prime mover mounted end together with pump parts inside of the casing adapted to be readily removed through said remote end upon removal of the end cap.
The invention will be hereinafter specifically described as embodied in an aircraft engine fuel pump of the type disclosedI in the Russell R.'
Curtis yPatent No. 2,268,805, dated January 6. 1942, but it should be understood that the principles of this invention are generally applicable to other types of pumps. It should also be understood that the pumps of this invention are useful for pumping many different types of fluids including water, solvents such as alcohol, gasoline, oil and the like. l
In general the pumps of this invention include a casing having an end wall portion adapted Ato t into the aperture of a prime mover. This end wall has a small central aperture for receiving a shaft therethrough to be coupled with the prime mover. The casing has an open end remote froml the end wall.' A readily removable cap is provided for closing this open end. All of the pump parts are held in the casing between the end wall and the removable end cap, and are so designed that they can be retracted from the casing by removal of the end cap. The pumps of this inventionjtherefore, can beserviced without separating them from the prime mover on which they may be mounted.
It is, then, an object of this invention to provide a pump and casing assembly arranged for mounting on a prime mover and having a readily removable end cap closing an opening through which all of the pump parts can be retracted without disconnecting the assembly from the prime mover.
A further object of the invention is to provide a simplified positive displacement type pump and casing assembly arranged so that all of the pump parts in the casing assembly are held in position by a removable end cap and are removed from the casing through the end closed by the removable end cap.
A still further object of theinvcntion is to pro` vide a simplified positive displacement pump that is easily assembled and disassembled, and is inexpensive to manufacture.
A still further object of the invention is to provide a universal type pump adapted to handle fluids of all natures and-adapted to be quickly repaired.
4 claims. (cl. 10s-137) A further object of this invention is to provide a pump and seal assembly for quick installation in a. casing arranged to be readily removed from the casing upon removal of a single end cap on the casing.
Other and further objects of the invention will be apparent to those skilled in the art from the following detailed description of the annexed sheet of drawings which, by way of preferred example only, illustrates one embodiment of the invention. f
On the drawings:
Figure 1 is a top plan view of a pump according to this invention mounted on an engine part shown in horizontal cross section.
Figure 2 is avertical cross-sectional view, with parts in side elevation, of the assembly shown in Figure 1 taken along the line II-JI of Figure 1.
Figure 3 isl an exploded view illustrating the manner in which the pumpparts are readily removed from the pump casing without removal of the casing from the engine.
As shown on the drawings:
The pump assembly I0 of this invention is mounted on an engine part II and includes a main pump casing or housing I2. a by-.pass and relief valve casing I3 mounted on top of the v casing I2, and a spring casing I4 mounted on top of the valve casing I3. The casings I3 and Ill and the parts therein are described in the hereinbefore referred to Curtis Patent 2,268,805.
The pump casing I2 has an inlet port I2a and an outlet port I2b on opposite sides thereof together with an 'end wall I2c at one end thereof projecting forwardly from a surrounding mounting flange I2d. The casing I2 has an open end I2e remote from the wall I2C but in axial alignment therewith. The casing I2 thus denes a cylindrical chamber open at one end I 2e thereof and closed at the other end I2C thereof. The end I2c has a central aperture I2f therethrough.
The engine part II includes a .pad I5 with an aperture I5a therethrough receiving the end wall I2c in snug engagement therewith. This end wall I2c thus acts as a pilot portion for aligning the pump on the engine part. A gasket or sealing washer I6 overlies the pad I5 and is positioned between the pad and the mounting face of the mounting `flange I2d.
Studs I'I project from the pad I5 at spaced intervals and extend through the mounting flange I2d. Nuts I8 threaded on the studs I'I clamp the flange in fixed relation on the pad,
thereby securing the pump assembly I0 to the A thrust washer |9 composed of an oil-impregnated sinteredv bronze or other oil-retaining bearing material is seated in the casing |2 against; the end wall |2c thereof. This washer |9 has a chamfered central aperture |9a therethrough.
A splined driver or pump shaft has a first splined end 20a adapted to project into the engine part to be coupled with the engine drive. The driver 20 has a shaft portion 20h which fits freely in the aperture Isa of the washer I9 and |2f of the end wall |2e. A rounded collar portion 20c is formed on the driver adjacent the cylindrical shaft portion 2Gb thereof and this collar rides on the chamfered aperture |9a of the washer I9, in rockable relation.
The driver has a smaller splined end 20d remote from the end 20a thereof which is splined into the hollow hub .2| a of the pump rotor 2|. The rotor 2| has a second hub 2| b at the opposite end thereof.
The hub 2 la is hollow and has a plug 22 pressed therein inwardly from its end. A coil spring 23 is compressed between the plug 22 and the splined end 20d of the driver 20 to urge the driver outwardly from the rotor hub so that its collar 20c will continually seat on the chamfered aperture |9a of the thrust washer |9. A ball and socket joint relationship between the driver and the thrust washer is obtained.
The rotor 2| ts freely into the casing l2 and is rotatably supported therein on bearing rings 24 and 25 which can be formed of graphitic carbon or the like plain bearing material. The bearing 24 rotatably supports the rotor hub 2|a while the bearing 25 rotatably supports the rotor hub 2lb..
A pump liner 26 is snugly tted in the casing I2 between the bearings 24 and 25 and around a central enlarged portion 2|c of the rotor 2|. The liner 26 has an eccentric inner bore 26a cooperating with the exterior surface of the central hub portion 2 Ic to define therebetween the pumping chamber for the pump. The liner has apertures aligned With the casing ports |2a and |2b so that the pumping chamber is in communication with these ports.
I he central portion of the rotor 2| has a pair of slots such as the slot 21 therethrough in right angular relationship. These slots ,slidably support the pumping vanes such as 28. The pumping vanes have intermediate tongues but their peripheral portions provide continuous surfaces in the pumping chamber.
The liner 26 Ais held against rotation in the casing |2 by means of a lock clip 29 which ts in a recess such as recess 2Gb in the liner which can be conveniently formed by a milling cutter. The clip 29 is inserted through an aperture |21' in the casing l2.
A stationary seal ring 30 composed of graphitic carbon or similar material has a grooved end face seated on the thrust washer I9 and cooperating therewith to dene grooves 3| which will drain any liquid which may leak past the end seal face of ring 30, to passageways 32 connecting the interior of the casing with the inner ends of the threaded plugs |2g.
An O ring 33, composed of resilient rubber-like material capable of resisting aromatic solvents is urged against the peripheral portion of the stationary seal ring 30 by a washer 34 acted on by a spring 35 which is compressed between the washer and the bearing 24. This O ring will seal the peripheral portion of the stationary seal ring 30 in the casing.
' A rotating seal ring 36 composed of Monel 4: y metal or the like material is disposed around the hub 2|a and has an end face riding on the stationary seal ring 30. A Phosphor gbronze or stainless steel wire clip 31 is'snapped into. the hub 2 la of the rotor and fits in an internal groove in' the rotating seal ring 36 to form akey `connection todrive the rotating seal ring with the rotor.
A synthetic rubber rsleeve 38 embraces the rotating seal ring 36 and has a beaded end seated in a peripheral groove on the rotating seal ring 36. The sleeve 38 snugly engages the hub 2|a and is tightly secured thereon by means of a lock wire39. A metal cup 40 embraces the portion of the sleeve disposed around the seal ring 36 and is urged by a spring 4| to move the seal ring against the stationary ring 30. The spring 4| is bottomed on a washer 42 which is held against axial movement on the hub 2 la by a lock wire 43.
The plug 22 prevents leakage through the rotor hub 2|a. The seal assembly including vthe stationary seal ring 30, the rotating seal 36, and the rubber sleeve 39 prevents leakage of material around the rotor hub 2 la, However, if the seal between the rotating and stationary seal rings should leak, the leaked material will be drained through the grooves 3| into a passageway 32.
The driver 20 is free to wobble, since it is rockably splined in the hub 2|a, but wobbling movements of the driver will not unevenly load the bearings for the rotor. The driver at all times has sealing engagement with the thrust washer 9 although it is free to rock and tilt on this washer. This sealing engagement prevents leakage of lubricating oil from the engine driver into and through the pump drain grooves 3| and passageways 32. Likewise, this seal prevents any liquid leakage on the interior of the pump past the driver 20 to the exterior of the pump through the central aperture |2f.
The open end |2e of the casing |2 is closed by an end cap 44 which is in the nature of a stamped metal plate preferably composed of stainless steel. A gasket or sealing washer 45 is interposed between the end of the casing and the plate 44. Cap screws 46 are passed through the end cap 44 and are threaded into the casing to secure the end cap to the casing. The end cap abuts the bearing 25 and cooperates with the end wall |2e of the casing to clamp all of the pump parts therebetween.
When the end cap 44 is removed from the casing I2, as illustrated in Figure 3, all of the pump parts are readily retracted through the open end |2e of the casing and can be replaced or repaired without disconnecting the casing from the engine part The spring 35 acts as a resilient take-up means for the O ring seal 33 should this part take a compression set. When the end cap 44 is removed, the spring 35 aids in the removal of the pump parts, since it tends to force the bearingy `or replaced without difficulty.
ment with the end wall in spaced relation therep from, a mounting flange on said casing sur- 'rounding said end wall, a pump shaft extending freely through the aperture in said end wall, said pump shaft having a shoulder disposed in the casing, a thrust washer bottomed on said apertured end wall, said thrust washer having a beveled aperture receiving said shoulder of the drive shaft in tiltable relation thereon, a stationary seal ring having one face thereof bottomed on said thrust washer, an O ring in said casing bottomed on the peripheral portion of the other face of said stationary seal ring, a washer overlying said 0 ring, a rotating seal ring having an end face riding `on said other face of the stationary seal ring, a pump rotor in said casing having hubs at the ends thereof with one of the hubs extending through and keyed to the rotating seal ring, bearing rings seated in said casing rotatably supporting'said rotor hubs, a pump liner between said bearing rings cooperating with said rotor to dene therebetween a pumping chamber, pumping vanes carried by said rotor, a spring compressed between said washer overlying the 0 ring and the bearing ring adjacent said washer, a removable end cap secured to the open end of said casing thrusting against the other of said bearings cooperating with said apertured end wall to clamp the pump parts inthe casing, and all of said parts in said casing being arranged for removal through the open end of the casing.
2. A pump comprising Va casing having a peripheral wall, a flanged end with an apertured end wall and an open end opposite the apertured end wall, said flanged-end being arranged for attachment to an engine pad, a liner in said casing, bearing rings in said casing bottomed'on opposite ends of said liner, a pump rotor in saidl casing rotatable in said bearing rings, pumping vanes carried by said rotor, a hub on said rotor projecting through one of said bearing rings, a driver for said rotor projecting through the apertured end wall of the casing, said driver having a shoulder portion in the casing of larger diameter than the aperture in said end wall, means in said casing receiving said shoulder in tiltable relation, a stationary seal ring bottomed on said means, a rotating seal ring riding on said stationary seal ring, a washer on said hub of the rotor, a nrst spring bottomed on said rotating seal ring and on said washer to maintain the rotating seal ring in sliding sealing engagement with the stationary seal ring, a second spring compressed between said stationary seal ring and the adjacent bearing ring. and an end 'cap removably secured to the open end of the casing in thrusting relation tothe other bear- .ing ring whereby .removal of said end cap alon opposite sides of said liner, a pump rotor in said casing rotatable in said bearing rings, pumping vanes carried by said rotor, a hubon said rotor projecting through one of said bearing rings, a driver forA said rotor projecting through the apertured end wall of said casing, said driver having a shoulder portion in the casing of larger diameter than the diameter of the aperture in said end Wall. means in said casing receiving said shoulder in tiltable relation, a stationary seal ring bottomed on said means, an 0 ring having one face bottomed on said stationary seal ring, a washer in surface engagement with the other face of said 0 ring, a rotating seal ring riding on said stationary seal ring, a second washer on said hub of the rotor, a spring bottomed on said rotating real ring and on said second washer to maintain the rotating seal ring in sliding sealing engagement with the stationary seal ring, a second spring compressed between said first washer and the adjacent bearing ring to maintain said O ring in sealing engagement with said stationary seal ring, and an end cap removably secured to the open end of the casing in thrusting relation to other bearing ring whereby removal of said end cap allows said second spring to urge pump parts out of the open end of the casing.
4. A pump comprising .a casing having an apertured end wall with a mounting flange therearound for attachment to an engine, said casing having an open end remote from said apertured end wall, a lubricated thrust washer seated against said end wall and having a chamfered aperture opening toward said open end and registering with the aperture of said end wall. a pump rotor rotatably disposed in said casing, pumping vanes carried by said rotor, a. drive shaft for said rotor extending through said aD- ertured end wall and said thrust washer, said shaft having a peripherally rounded circumferopen end of the casing for clamping said ro tor and said seal parts between the end wall of ythe cap against the action of said spring, said chamfered washer aperture facilitating removal of said drive shaft and insuring sealing of said shaft upon assembly. v
DONALD R, SPO'IZ.
anrEaENcEs cri-En The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,497,050 Wardell June 10, 1924 1,877,688 Petersen 1---- Sept. 13, 1932 2,112,522 Czarnecki. et al. Mar.` 29, 1938 2,131,968 Petersen Oct. 4, 1938 2,268,805 Curtis Jan. 6, 1942 ,2,302,907 Eilers NOV. 24, 1942 2,348,679 Groves May 9, 1944 2,372,816 Deschamps et al. Apr. 3. 1945 3,380,783 Painter` July 31, 1945
US553814A 1944-09-13 1944-09-13 Pump Expired - Lifetime US2521420A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US553814A US2521420A (en) 1944-09-13 1944-09-13 Pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US553814A US2521420A (en) 1944-09-13 1944-09-13 Pump

Publications (1)

Publication Number Publication Date
US2521420A true US2521420A (en) 1950-09-05

Family

ID=24210863

Family Applications (1)

Application Number Title Priority Date Filing Date
US553814A Expired - Lifetime US2521420A (en) 1944-09-13 1944-09-13 Pump

Country Status (1)

Country Link
US (1) US2521420A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782725A (en) * 1954-05-18 1957-02-26 Hojberg Laurencio Brochner Rotary pump
US2856860A (en) * 1955-08-03 1958-10-21 Mechanisms Company Fluid pressure transducer with end clearance control
US2971469A (en) * 1959-09-14 1961-02-14 Jabsco Pump Co Pump with floating end plates
US20160252136A1 (en) * 2014-02-14 2016-09-01 Bayerische Motoren Werke Aktiengesellschaft Device for Transmitting a Torque in a Range Extender

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1497050A (en) * 1923-10-25 1924-06-10 Hill Compressor & Pump Company Rotary pump
US1877688A (en) * 1931-04-16 1932-09-13 Viking Pump Company Rotary pump
US2112522A (en) * 1936-06-13 1938-03-29 Eddington Metal Specialty Co Pump
US2131968A (en) * 1935-10-24 1938-10-04 Viking Pump Company Reversibly associated rotary pump and valve device
US2268805A (en) * 1939-07-13 1942-01-06 Curtis Pump Co Aircraft fuel pump
US2302907A (en) * 1939-04-24 1942-11-24 Tokheim Oil Tank & Pump Co Lubricating and sealing drain device
US2348679A (en) * 1941-03-14 1944-05-09 Yale & Towne Mfg Co Pump
US2372816A (en) * 1942-09-16 1945-04-03 Bendix Aviat Corp Engine accessory
US2380783A (en) * 1941-04-07 1945-07-31 Gerotor May Company Pump structure

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1497050A (en) * 1923-10-25 1924-06-10 Hill Compressor & Pump Company Rotary pump
US1877688A (en) * 1931-04-16 1932-09-13 Viking Pump Company Rotary pump
US2131968A (en) * 1935-10-24 1938-10-04 Viking Pump Company Reversibly associated rotary pump and valve device
US2112522A (en) * 1936-06-13 1938-03-29 Eddington Metal Specialty Co Pump
US2302907A (en) * 1939-04-24 1942-11-24 Tokheim Oil Tank & Pump Co Lubricating and sealing drain device
US2268805A (en) * 1939-07-13 1942-01-06 Curtis Pump Co Aircraft fuel pump
US2348679A (en) * 1941-03-14 1944-05-09 Yale & Towne Mfg Co Pump
US2380783A (en) * 1941-04-07 1945-07-31 Gerotor May Company Pump structure
US2372816A (en) * 1942-09-16 1945-04-03 Bendix Aviat Corp Engine accessory

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782725A (en) * 1954-05-18 1957-02-26 Hojberg Laurencio Brochner Rotary pump
US2856860A (en) * 1955-08-03 1958-10-21 Mechanisms Company Fluid pressure transducer with end clearance control
US2971469A (en) * 1959-09-14 1961-02-14 Jabsco Pump Co Pump with floating end plates
US20160252136A1 (en) * 2014-02-14 2016-09-01 Bayerische Motoren Werke Aktiengesellschaft Device for Transmitting a Torque in a Range Extender
US10495154B2 (en) * 2014-02-14 2019-12-03 Bayerische Motoren Werke Aktiengesellschaft Device for transmitting a torque in a range extender

Similar Documents

Publication Publication Date Title
US4538820A (en) Shaft seal
US3675933A (en) Seal with installed space parts
US2027505A (en) Bearing seal for rotary shafts
GB499775A (en) Improvements in or relating to shaft bearing and sealing assemblies for pumps
US3053189A (en) Motor driven pumps
US2279136A (en) Rotary pump
US2625883A (en) Centrifugal pump drive and seal means
US2429953A (en) Shaft seal assembly
US2521420A (en) Pump
US2393260A (en) Shaft seal
US2226001A (en) Gland
US2407218A (en) Fluid sealing device
US3526469A (en) Pump motor seal system
US2666394A (en) Pump construction
US2432684A (en) Liquid cooled seal
US2749156A (en) Seal
US3097610A (en) Pump and motor construction
US2756080A (en) Rotary seal and clutch assembly
US1978689A (en) Sealing means
US2438457A (en) Shaft seal
US2489212A (en) Fluid seal
US4242062A (en) Dual piston pump with pressure seal lubrication feature
US2104355A (en) Shaft sealing means
US2355390A (en) Bearing
US11073212B1 (en) Packing cartridge and method of installation