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US2139373A - Electric fuel pump - Google Patents

Electric fuel pump Download PDF

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Publication number
US2139373A
US2139373A US58892A US5889236A US2139373A US 2139373 A US2139373 A US 2139373A US 58892 A US58892 A US 58892A US 5889236 A US5889236 A US 5889236A US 2139373 A US2139373 A US 2139373A
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United States
Prior art keywords
pump
fuel
motor
shaft
spacer
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Expired - Lifetime
Application number
US58892A
Inventor
Charles W Mckinley
Carleton J Lauer
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Motors Liquidation Co
Original Assignee
General Motors Corp
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Priority to US58892A priority Critical patent/US2139373A/en
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Publication of US2139373A publication Critical patent/US2139373A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/04Feeding by means of driven pumps
    • F02M37/08Feeding by means of driven pumps electrically driven
    • F02M37/10Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/04Feeding by means of driven pumps
    • F02M37/08Feeding by means of driven pumps electrically driven

Definitions

  • This invention relates to the fuel supply system for engines such as are used Ion motor vehicles, on boats, aircraft, and in stationary power plants. It is more particularly concerned with the de- ⁇ 5 livery of fuel from the reservoir or tank to the remotely located engine. It is intended to replace such older means of delivering fuel as the vacuum tank and the engine operated suction producing pump.
  • Fig. 1 is aview of the motor and pump assembly mounted on a fuel reservoir the latter being shown in transverse section.
  • Fig. 2 is a section on a vertical plane through the motor.
  • Fig. 3 is a section on a vertical plane through the pumping mechanism.- I
  • Fig. 4 is another similar section but in a different plane from that of Fig. 3.
  • Fig. 5 is a horizontal section on line 5-5 of Fig. 3.
  • Fig. 6 is a horizontal section on line 6--6 of 45 'Z is a horizontal section on line 1-1 of Referring by lreference characters to the drawings, numeral II represents a reservoir or tank carried by a motor vehicle from which fuel is to be delivered to the carburetor of the engine, the
  • An arrangement now in common use employs a pump located adjacent the engine and operated by a moving part of the latter.
  • One stroke of the pump creates suction in the pump chamber and the conduit connecting the pump chamber and reservoir resulting in the flow of fuel to the pump.
  • the other pump stroke delivers fuel from the pump chamber to the carburetor.
  • the 5 .location of the pump adjacent the engine is such that the fuel is heated and the reduced pressure of the pump action lowers the boiling point. In consequence there may develop -a quantity of fuel vapor which may merely com- 10 press and expand under the influence ,of pump operation, so that no liquid fuel is delivered to the carburetor.
  • the present invention removes the pump from the region of the engine and does not use suction as a means for causing the flow 15 through the conduit.
  • the details of the electric motor and pump assembly are productive of several advantages 2
  • the motor marked I5 has an outer shell I1 and a rotor I9, the latter provided with a rotor shaft 2
  • Shaft 2l is mounted in bearings 23 having an external spherical counter.
  • the bearings are of porous 3 metal oil absorbing material and are supplied with lubricant by oil saturated felt washers 25 mounted in suitably shaped upper and lower pockets of the shell.
  • extends below the motor housing I1 for g a purpose to be explained.
  • the brush carrying plate 21 is spaced by a paper collar 29.
  • the collar in addition to other functions, serves to prevent transmission of noises from the brushes.
  • the motor is so designed as to avoid magnetic hum;
  • the commutator is designed to be sparkless. It isintended that the motor shall last throughout the life of the car and require no lubrication.
  • a 'I'he pump is formed by uniting two parts, an upper part 3
  • a spacer 35 an elongated member, houses suitable means for transmitting the drive of the motor to the pump and has a conduit or passage for the fiow of fuel from the pump.
  • Bolts or other fastening means 31 secure the pump parts 73
  • the upper end of the spacer 35 is secured by fastening means 39 to the motor shell I1.
  • a thick rubber ring 4I is clamped between the casing I1 and the spacer '35.
  • the reduced end 53 of rotor shaft 2l is received within and keyed to a tubular driving shaft 55, the latter extending through a tubular passage in the spacer 35.
  • a tubular driving shaft 55 At the lower end of the spacer the tubular shaft 55 is similarly keyed in driving relation to the reduced upper end of the pump shaft 51, the numeral 59 indicating the coupling key.
  • the shaft 57 carries the helical pump gear 6
  • the driven gear 63 is secured to a shaft 6l journaled in a tubular bore as shown in Fig. 3.
  • a recess 69 in the top of the lower pump member houses a ball 'H which supports the shaft 5l and, with it, the shafts 55 and 2l together with the rotor element of the motor, thereby providing an antifriction thrust bearing.
  • the lower pump member 33 is formed with an inlet passage 'i3 communicating with the gear pump chamber. To the lower member 33 is also secured a suction bell l5 which is positioned just above the bottom a lter screen lll. This lower pump member also has a bypass valve leading' from the discharge side of the gear pump to the region within the screen. It employs a valve seat 79 adapted to be engaged by a disc valve 8l held by a spring 83 having an abutment t5.
  • the inlet passage 73 in the lower pump member communicates with inlet region tl in the upper pump member.
  • the outlet region of the pump chamber is marked 89. It registers with a passage 9i extending from the pump chamber to the top of the upper pump section 3i. This passage 9i is enlarged or relieved toward the junction with the pump chamber to allow fuel to be squeezed out from between the pump teeth without noise.
  • the lower end of the spacer is formed with a notch 93 and the gasket 95 has a slot @l as shown by Figi 5.
  • the tubular space @a within the spacer through which the drive shaft extends is in communication not only with the bore in the upper pump member for shaft 5l but also, by means of the notch 93 and the slot 97, with the bore carrying shaft 6l'. Lubrication of the pump shafts is thus provided.
  • An aperture lOl is formed in the spacer lead- 99, so that fuel may freelyenter this space.
  • an air seal washer BB3 is provided as shown on Fig. 2.
  • the spacer is formed with a tubular bore M35 registering with outlet passage Qi and itself communicating with passage lill in the motor casing, which latter is terminally screw-threaded for connection with any suitable conduit for supplying the carburetor of the engine. terminals for wires are of course present as shown at $59.
  • and 51 provides a sort of universal connection to accommodate any slight misalignment of the shafts.
  • the rotor element of the motor and the shafts have an anti-friction thrust bearing conveniently formed by the ball ll.
  • the pump shafts should be chrome plated because such a surface runs well in the die cast upper pump member when lubricated with
  • the pump capacity is such as to provide for maximum requirements and the spring loaded bypass is available to restore to the region within the'iilter screen the fuely in excess of that which can be delivered to the conduit and carburetor.
  • the electric motor circuit may be closed by the ignition switch with the result that the fuel is pumped to the carburetor as soon as the switch is closed, even before the starter comes into action.
  • the pump shall have a minimum capacity of twenty gallons per hour at four pounds pressure. No greater pump capacityis needed for any present day automobile and it is unnecessary for more than a single size 'of pump to be manufactured.
  • the motor is very emcient in that it supplies the twenty gallons per hour, drawing less than two amperes at six volts.
  • the self-aligning bearings have obvious utility. The seal effectively prevents any gasoline reaching and damaging-the electric motor.
  • a motor and pump assembly for delivering fuel from the fue] tank of a motor vehicle, a motor, a spacer and a pump including a pump casing connected in superposed relation, said motor and pump having aligned shafts, said spacer having an elongated liquid carrying space and a fuel discharge passage, a shaft in said liquid carrying space coupled to said motor and pump shafts, said pump having a second parallel pump shaft journalled in the casing of said pump, co-
  • a motor, a spacer and a pump including a pump housing connected in superposed relation, said motor and shafts in said pump housing, and a connecting passage between the lower end of said liquid carrying space and the upper end of said bore for the purpose of conducting liquid from said space to said bore to lubricate the second pump shaft.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

Dec. 6, 1938.
C. W MCKINLEY ET AL 2,139,373 ELECTRIC FUEL PUMP Filed Jan. 15, 1956 2 Sheets-Sheet l Patented Dec. 6, 1938 STATES UNITE l ELECTRIC FUEL PUMP Charles W. McKinley and Carleton J Lauer, Flint,
Mich., assignors to General Motors Corporation, Detroit, Mich., a corporation of Delaware Application January 13, 1936, Serial No. 58,892 3 Claims. (Cl. 103-118) This invention relates to the fuel supply system for engines such as are used Ion motor vehicles, on boats, aircraft, and in stationary power plants. It is more particularly concerned with the de- `5 livery of fuel from the reservoir or tank to the remotely located engine. It is intended to replace such older means of delivering fuel as the vacuum tank and the engine operated suction producing pump. In both these older well known forms, the fuel, flowing from the reservoir undef` the inuence of reduced pressure, has had a tendency to vaporize under excessive heat conditions and it is one of the primary objects of the present invention to devise a fuel supply system which shall avoid the disadvantage of fuel vaporization and vapor lock which, in the case of an engine operated pump, has interfered with the delivery of liquid fuel to the oat bowl of the carburetor.
Among the other objects to be attained by the specific structural arrangements, there should be included the provision for substantially noiseless operation, the promptness in supplying the fuel to the engine, the high'pumping capacity, the
long life of the mechanism and the provision whereby fuel is prevented from reaching the electric motor which is used for operating the pump.
St' l other objects and advantages will be understood from the following description.
In the drawings accompanying the description:
Fig. 1 is aview of the motor and pump assembly mounted on a fuel reservoir the latter being shown in transverse section.
Fig. 2 is a section on a vertical plane through the motor.
Fig. 3 is a section on a vertical plane through the pumping mechanism.- I
Fig. 4 is another similar section but in a different plane from that of Fig. 3.
Fig. 5 is a horizontal section on line 5-5 of Fig. 3.
Fig. 6 is a horizontal section on line 6--6 of 45 'Z is a horizontal section on line 1-1 of Referring by lreference characters to the drawings, numeral II represents a reservoir or tank carried by a motor vehicle from which fuel is to be delivered to the carburetor of the engine, the
latter usually located in a position on the vehicle remote from the tank.
An arrangement now in common use employs a pump located adjacent the engine and operated by a moving part of the latter. One stroke of the pump creates suction in the pump chamber and the conduit connecting the pump chamber and reservoir resulting in the flow of fuel to the pump. The other pump stroke delivers fuel from the pump chamber to the carburetor. The 5 .location of the pump adjacent the engine is such that the fuel is heated and the reduced pressure of the pump action lowers the boiling point. In consequence there may develop -a quantity of fuel vapor which may merely com- 10 press and expand under the influence ,of pump operation, so that no liquid fuel is delivered to the carburetor. The present invention removes the pump from the region of the engine and does not use suction as a means for causing the flow 15 through the conduit. y This is accomplished by mounting the pump I3 within the reservoir II and operating it by an electric motor I5 supported upon the reservoir or tank II. This location avoids the heating effect of the engine 2c and since the fuel is pushed under superatmospheric pressure, the liquid fuel is much less likely to boil.
The details of the electric motor and pump assembly are productive of several advantages 2| including those above set forth. The motor marked I5 has an outer shell I1 and a rotor I9, the latter provided with a rotor shaft 2|. Shaft 2l is mounted in bearings 23 having an external spherical counter. The bearings are of porous 3 metal oil absorbing material and are supplied with lubricant by oil saturated felt washers 25 mounted in suitably shaped upper and lower pockets of the shell. The extreme lower end of shaft 2| extends below the motor housing I1 for g a purpose to be explained. The brush carrying plate 21 is spaced by a paper collar 29. The collar, in addition to other functions, serves to prevent transmission of noises from the brushes. The motor is so designed as to avoid magnetic hum; The commutator is designed to be sparkless. It isintended that the motor shall last throughout the life of the car and require no lubrication.
'I'he pump is formed by uniting two parts, an upper part 3| and a lower part 33. A spacer 35, an elongated member, houses suitable means for transmitting the drive of the motor to the pump and has a conduit or passage for the fiow of fuel from the pump. Bolts or other fastening means 31 secure the pump parts 73| and 33 to the lower end of the spacer. The upper end of the spacer 35 is secured by fastening means 39 to the motor shell I1. A thick rubber ring 4I is clamped between the casing I1 and the spacer '35. The
,ing from space outer margin of the rubber ring 4l is secured to the peripheral region 43 surrounding an opening 45 in the reservoir Il by fastening means il extending through a ring 49 adjacent the motor casing l1, the rubber ring and an inner ring 5I.
The reduced end 53 of rotor shaft 2l is received within and keyed to a tubular driving shaft 55, the latter extending through a tubular passage in the spacer 35. At the lower end of the spacer the tubular shaft 55 is similarly keyed in driving relation to the reduced upper end of the pump shaft 51, the numeral 59 indicating the coupling key. The shaft 57 carries the helical pump gear 6|. 'Ihis gear 6l together with a cooperating gear 63 constitutes the gear pump, the two gears being located in a suitable chamber 65 formed in the lower part of the upper pump chamber. The driven gear 63 is secured to a shaft 6l journaled in a tubular bore as shown in Fig. 3.
A recess 69 in the top of the lower pump member houses a ball 'H which supports the shaft 5l and, with it, the shafts 55 and 2l together with the rotor element of the motor, thereby providing an antifriction thrust bearing.
The lower pump member 33 is formed with an inlet passage 'i3 communicating with the gear pump chamber. To the lower member 33 is also secured a suction bell l5 which is positioned just above the bottom a lter screen lll. This lower pump member also has a bypass valve leading' from the discharge side of the gear pump to the region within the screen. It employs a valve seat 79 adapted to be engaged by a disc valve 8l held by a spring 83 having an abutment t5.
The inlet passage 73 in the lower pump member communicates with inlet region tl in the upper pump member. The outlet region of the pump chamber is marked 89. It registers with a passage 9i extending from the pump chamber to the top of the upper pump section 3i. This passage 9i is enlarged or relieved toward the junction with the pump chamber to allow fuel to be squeezed out from between the pump teeth without noise.
The lower end of the spacer is formed with a notch 93 and the gasket 95 has a slot @l as shown by Figi 5. The tubular space @a within the spacer through which the drive shaft extends is in communication not only with the bore in the upper pump member for shaft 5l but also, by means of the notch 93 and the slot 97, with the bore carrying shaft 6l'. Lubrication of the pump shafts is thus provided.
An aperture lOl is formed in the spacer lead- 99, so that fuel may freelyenter this space. To prevent this fuel from reaching the motor an air seal washer BB3 is provided as shown on Fig. 2. When the reservoir is filled with fuel, the fuel enters the space 99 and the air at the top of this'space is compressed between the top of the column of liquid fuel and the seal whereby the fuel is prevented by the seal from reaching the motor.
The spacer is formed with a tubular bore M35 registering with outlet passage Qi and itself communicating with passage lill in the motor casing, which latter is terminally screw-threaded for connection with any suitable conduit for supplying the carburetor of the engine. terminals for wires are of course present as shown at $59.
It will be understood that such a pump and motor'assembly will largely overcome the difficulty of vapor lock since the mechanism is wholgasoline.
of the reservoir and encloses Suitable I appreciable wear when operating with gasoline.`
The drive tube 55 connecting the solid shafts 2| and 51 provides a sort of universal connection to accommodate any slight misalignment of the shafts. The rotor element of the motor and the shafts have an anti-friction thrust bearing conveniently formed by the ball ll.
The pump shafts should be chrome plated because such a surface runs well in the die cast upper pump member when lubricated with The pump capacity is such as to provide for maximum requirements and the spring loaded bypass is available to restore to the region within the'iilter screen the fuely in excess of that which can be delivered to the conduit and carburetor.
The provision for avoiding noise from the squeezing of fuel from the pump gears has been referred to above.
In case the reservoir is pumped dry the fuel remaining in the tubular space 99 is sufficient to lubricate the pump shafts for a short time.
It is to be observed also that the electric motor circuit may be closed by the ignition switch with the result that the fuel is pumped to the carburetor as soon as the switch is closed, even before the starter comes into action. v
Referring again to the power plant, it is the intent that the pump shall have a minimum capacity of twenty gallons per hour at four pounds pressure. No greater pump capacityis needed for any present day automobile and it is unnecessary for more than a single size 'of pump to be manufactured. The motor is very emcient in that it supplies the twenty gallons per hour, drawing less than two amperes at six volts. The self-aligning bearings have obvious utility. The seal effectively prevents any gasoline reaching and damaging-the electric motor.
We claim:
l. In a motor and pump assembly for delivering fuel from the fue] tank of a motor vehicle, a motor, a spacer and a pump including a pump casing connected in superposed relation, said motor and pump having aligned shafts, said spacer having an elongated liquid carrying space and a fuel discharge passage, a shaft in said liquid carrying space coupled to said motor and pump shafts, said pump having a second parallel pump shaft journalled in the casing of said pump, co-
operating pump gears on said parallelv pump= shafts, and said spacer formed with a notch at its lower end leading from the liquid carrying space and directed toward the'upper end of said second parallel shaft,A means" affording communication between said notch and the journal for said second pump shaft whereby liquid from said space may lubricate said second pump shaft.
2. The invention dened by claim' 1, said last named means being a gasket between said spacer and pump, said gasket having a slot connecting the notch and the journal bearing for the second pump shaft.
3. In a motor and pump assembly, a motor, a spacer and a pump including a pump housing connected in superposed relation, said motor and shafts in said pump housing, and a connecting passage between the lower end of said liquid carrying space and the upper end of said bore for the purpose of conducting liquid from said space to said bore to lubricate the second pump shaft. 5
CHARLES W. MCKINLEY. CARLETON J. LAUER.
US58892A 1936-01-13 1936-01-13 Electric fuel pump Expired - Lifetime US2139373A (en)

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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2515262A (en) * 1944-06-23 1950-07-18 Timken Axle Co Detroit Liquid fuel burner apparatus
US2557265A (en) * 1944-11-06 1951-06-19 Denison Eng Co Hydraulic press
US2630759A (en) * 1949-10-22 1953-03-10 Thomas E Mahlon Variable volume rotary pump
US2636667A (en) * 1942-11-18 1953-04-28 Bendix Aviat Corp Pump
US2792192A (en) * 1953-10-20 1957-05-14 North American Aviation Inc Aircraft fuel pump and tank arrangement
US2885962A (en) * 1956-03-08 1959-05-12 Borg Warner Fuel pump
US2915978A (en) * 1956-04-10 1959-12-08 Edward J Schaefer Motor pump unit
US3002794A (en) * 1957-10-14 1961-10-03 Howard Ind Inc Motor bearing organization
US3074350A (en) * 1959-01-06 1963-01-22 R C Ray Portable pump with interchangeable drive unit
US3176620A (en) * 1961-07-12 1965-04-06 Thompson Ramo Wooldridge Inc High pressure cryogenic turbine driven pump
US3232681A (en) * 1960-12-19 1966-02-01 Licentia Gmbh Bearing
US6220827B1 (en) * 1996-08-17 2001-04-24 Continental Teves Ag & Co., Ohg Electromotor/pump assembly
ES2204268A1 (en) * 2001-01-23 2004-04-16 Honda Giken Kogyo Kabushiki Kaisha Tank fitting structure for fuel pump
US20090111909A1 (en) * 2007-10-23 2009-04-30 Jig-A-World Inc. Sprayable surface repair compound
US20110311373A1 (en) * 2008-10-02 2011-12-22 Inergy Automotive Systems Research (Societe Anonyme) Rotary pump for a vehicle
US20120006943A1 (en) * 2010-07-06 2012-01-12 Airbus Operations (S.A.S.) Aircraft including a fuel pump fastened to a tank panel
US20130092267A1 (en) * 2011-10-18 2013-04-18 Airbus Operations Limited Fuel tank installation

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2636667A (en) * 1942-11-18 1953-04-28 Bendix Aviat Corp Pump
US2515262A (en) * 1944-06-23 1950-07-18 Timken Axle Co Detroit Liquid fuel burner apparatus
US2557265A (en) * 1944-11-06 1951-06-19 Denison Eng Co Hydraulic press
US2630759A (en) * 1949-10-22 1953-03-10 Thomas E Mahlon Variable volume rotary pump
US2792192A (en) * 1953-10-20 1957-05-14 North American Aviation Inc Aircraft fuel pump and tank arrangement
US2885962A (en) * 1956-03-08 1959-05-12 Borg Warner Fuel pump
US2915978A (en) * 1956-04-10 1959-12-08 Edward J Schaefer Motor pump unit
US3002794A (en) * 1957-10-14 1961-10-03 Howard Ind Inc Motor bearing organization
US3074350A (en) * 1959-01-06 1963-01-22 R C Ray Portable pump with interchangeable drive unit
US3232681A (en) * 1960-12-19 1966-02-01 Licentia Gmbh Bearing
US3176620A (en) * 1961-07-12 1965-04-06 Thompson Ramo Wooldridge Inc High pressure cryogenic turbine driven pump
US6220827B1 (en) * 1996-08-17 2001-04-24 Continental Teves Ag & Co., Ohg Electromotor/pump assembly
ES2204268A1 (en) * 2001-01-23 2004-04-16 Honda Giken Kogyo Kabushiki Kaisha Tank fitting structure for fuel pump
ES2204268B1 (en) * 2001-01-23 2005-06-01 Honda Giken Kogyo Kabushiki Kaisha DEPOSIT MOUNT STRUCTURE FOR FUEL PUMP.
US20090111909A1 (en) * 2007-10-23 2009-04-30 Jig-A-World Inc. Sprayable surface repair compound
US9255574B2 (en) * 2008-10-02 2016-02-09 Inergy Automotive Systems Research (Societe Anonyme) Rotary pump for a vehicle
US20110311373A1 (en) * 2008-10-02 2011-12-22 Inergy Automotive Systems Research (Societe Anonyme) Rotary pump for a vehicle
US20120006943A1 (en) * 2010-07-06 2012-01-12 Airbus Operations (S.A.S.) Aircraft including a fuel pump fastened to a tank panel
US8851122B2 (en) * 2010-07-06 2014-10-07 Airbus Operations (S.A.S.) Aircraft including a fuel pump fastened to a tank panel
CN103057713A (en) * 2011-10-18 2013-04-24 空中客车运营有限公司 Fuel tank installation
US8960237B2 (en) * 2011-10-18 2015-02-24 Airbus Operations Limted Fuel tank installation
US20130092267A1 (en) * 2011-10-18 2013-04-18 Airbus Operations Limited Fuel tank installation
CN103057713B (en) * 2011-10-18 2016-06-15 空中客车运营有限公司 Fuel tank apparatus

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