[go: up one dir, main page]

US2779513A - Submerged rotary type fuel pump - Google Patents

Submerged rotary type fuel pump Download PDF

Info

Publication number
US2779513A
US2779513A US583185A US58318556A US2779513A US 2779513 A US2779513 A US 2779513A US 583185 A US583185 A US 583185A US 58318556 A US58318556 A US 58318556A US 2779513 A US2779513 A US 2779513A
Authority
US
United States
Prior art keywords
pump
shaft
diaphragm
fuel pump
rotary type
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
US583185A
Inventor
John W Dickey
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Priority to US583185A priority Critical patent/US2779513A/en
Application granted granted Critical
Publication of US2779513A publication Critical patent/US2779513A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • 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

Definitions

  • the present invention relates to a submerged rotary type fuel pump, and more particularly to an externally driven tank mounted pump.
  • Fig. 1 is a vertical substantially mid-sectional view of a preferred embodiment of the invention
  • Fig. 2 is a section taken on the line 2-2 of Fig. 1;
  • Fig. 3 is a section taken substantially on the line 3-3 of Fig. 1;
  • Fig. 4 is a vertical section of the pump structure taken substantially on the line 4-4 of Fig. 3;
  • Fig. 5 is a further detail section of the pump structure taken on the line 5-5 of Fig. 3;
  • Fig. 6 is a detail of one of the magnetic coupling discs, the magnetic poles being indicated pictorially.
  • a cup shaped casing 1 of cylindrical form having an intermediate shoulder 2 on which an impervious non-magnetic diaphragm 3 is mounted and hermetically sealed as by means of a soldering operation.
  • a rotary vane type of pump indicated generally at 1% 18 mounted in any suitable manner on the bottom of the casing 1 with its shaft 4 protruding concentrically into The shaft 4 carries a disc-shaped rotor 5 (Fig. 3) having radial slots 6 in which rectangular vanes 7 are slidably mounted for cooperation with the interior of an eccentric pump chamber 8 formed in the pump casing 9.
  • the pump 10 is provided with an inlet 11 (Fig. 5), an outlet 12 (Fig. 2) and a spring loaded by-pass valve connection 13, together with suitable ports and passages as indicated more particularly in Figs. 1, 3 and 5, whereby rotation of the pump shaft 4 causes liquid in which the pump is immersed to enter the inlet 11, and be forced out of the outlet 12.
  • the upper end of the casing 1 is closed by a mounting plate 14- arranged to be bolted to the top of a fuel tank 15 as indicated at 16, a gasket 17 being interposed to prevent leakage from the tank.
  • a driving motor 18 is carried by the mounting plate 14 and attached thereto by bolts and nuts as indicated at 19.
  • the motor shaft 2,779,513 C Fatented Jan. 29, 1957 21 extends into the upper chamber of the cup-shaped housing 1 in alignment with the pump shaft 4.
  • Magnetic means for coupling the motor shaft 21 to the pump shaft 4 comprising a hollow stub shaft 22 slidably journalled on the motor shaft 21 and connected for rotation therewith by a cross pin 23 engaging in slots 24 in the stub shaft 22.
  • a mounting cup 25 is fixedly mounted on the stub shaft 22 and has seated therein a flat ring magnet member 26 having a series of alternating magnetic poles formed on its surface as best shown in Fig. 6. It is preferred that this magnet be formed of a material having very high permanent coercive force such as the materials now available formed of sintered ceramic material, one form of which is known to the trade by the name of Indox.
  • the ring magnet 26 is held in the cup 25 by any suitable means as by an outer cup member Zil of non-magnetic material having its rim bent inwardly against a beveled surface of the magnet as shown in Fig. l.
  • the magnet is maintained in closely spaced relation to the diaphragm 3 by means of a thrust bearing 27 for the stub shaft 22, the stationary cup 36 of which thrust bearing rests directly on said diaphragm.
  • a similar permanent magnet 28 is mounted on a hollow stub shaft 29 by means of a mounting cup 31.
  • the stub shaft 29 is slidably journalled on the end of the pump shaft 4 and is connected to rotate with the pump shaft by a cross pin 32.
  • Magnet 28 is spaced from the diaphragm 3 by means of a thrust bearing 33 the stationary cup of which rests against the under side of the diaphragm 3.
  • Both the stub shafts 22 and 29 are drawn toward the diaphragm 3 by the mutual attraction of the two face-polarized ring magnets 26 and 23.
  • An outlet fitting comprising a nipple 35 is located in the mounting plate 14 and extends downward through the rim of the casing 1, the joint being sealed by the gasket 17.
  • a similar nipple 34 extends upwardly from the pump outlet 12 in alignment with the nipple 35 and a hose 36 is arranged to be clamped on the nipples as 3 is then inserted in the casing and soldered to the shoulder 2 of the casing to form a permanent fluid-tight partition between the upper and lower chambers of the casing.
  • the motor 18 is then attached to the mounting plate 14, the driving coupling member including the magnet 26 and shaft 22 is slid on the motor shaft 21, the outlet hose 36 is attached to the nipples 34 and 35 of the pump and outlet fitting, and the assembly is then inserted in the tank and attached thereto by means of the bolts 16.
  • Energization of the motor is transmitted through the magnetic coupling to the pump which operates in conventional manner to draw liquid in the inlet 11 of the pump and develop pressure in the outlet 12.
  • the output of the pump which is in excess of the fuel consumed by the device, such as an internal combustion engine, to be supplied thereby is permitted to escape back into the fuel tank through the spring pressed relief valve 13.
  • the upper chamber is also'preferably vented to the atmosphere bymeans of slots for the bolts 19 in the mounting plate 14.
  • a cup-shaped casing having a shaft extending into the lower chamber toward said diaphragm normal thereto, a stub shaft mounted on'the pump shaft and slidably but'non-rotatably connected thereto, 'a facepolarized disc magnet rigidly mounted on the stub shaft in parallel relation and in proximity to the diaphragm, and a thrust bearing for the stub shaft resting on said diaphragm and controlling the spacing of'the disc magnet from the diaphragm; a mounting plate fixed to and closing the upper chamber of the casing, ;a motor mounted thereon having a shaft extending into said upper chamber in alinernent with "the pump shaft, and a face-polarized disc magnet mounted on the motor shaft to rotate therewith parallel to and in close proximity to the diaphragm.
  • a tank-mounted fuel pump as set forth in claim 1 including further a hollow stubshaft telescopically splined on the motor shaft, the latter-mentioned disc magnet being mounted :rigidly on said hollow stub shaft; and a thrust bearing for said stub shaft resting on the diaphragm and controlling the spacing of the .latter-mentioneddisc magnet therefrom.
  • Atank mountedfuel pump as set forth in claim 1 in which the motorrmounting plateserves-also as a closure for the tank in which the pump is mounted, and said diaphragm is tightly sealed in the casing to prevent passage of liquid from one chamber to the other.
  • a tank-mounted pump as ,set forth in claim v3 in which the lower chamber is vented into the tank, while the upper chamber is vented to the. outside of the tank.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)

Description

Jan, 29, 19
5 J. w. DICKEY SUBMERGED ROTARY TYPE FUEL PUMP Filed May 7, 1956 4 (3 ilm Tmulm'.
ATTORNE 2 United States Patent SUBMERGED ROTARY TYPE FUEL PUMP John W. Dickey, Newfield, N. Y., assignor to Bendix Aviation Corporation, a corporation of Delaware Application May 7, 1956, Serial No. 583,185 4 Claims. (Cl. 222-333) The present invention relates to a submerged rotary type fuel pump, and more particularly to an externally driven tank mounted pump.
It is an object of the present invention to provide a novel pump of this type which is a rigid unitary structure, eiiicient in operation and not requiring fine adjustment.
It is another object to provide such a device which is adapted for continuous reliable operation over long periods of time without requiring service or adjustment.
It is another object to provide such a device in which a permanent impervious closure seals the pump from the motor.
It is another object to provide such a device in which the motor is connected to the pump by a magnetic coupling in which the spacing and aligning of the magnets is maintained in a simple and effective manner.
Further objects and advantages will be apparent from the following description taken in connection with the accompanying drawing in which:
Fig. 1 is a vertical substantially mid-sectional view of a preferred embodiment of the invention;
Fig. 2 is a section taken on the line 2-2 of Fig. 1;
Fig. 3 is a section taken substantially on the line 3-3 of Fig. 1;
Fig. 4 is a vertical section of the pump structure taken substantially on the line 4-4 of Fig. 3;
Fig. 5 is a further detail section of the pump structure taken on the line 5-5 of Fig. 3; and
Fig. 6 is a detail of one of the magnetic coupling discs, the magnetic poles being indicated pictorially.
In Fig. 1 of the drawing there is illustrated a cup shaped casing 1 of cylindrical form having an intermediate shoulder 2 on which an impervious non-magnetic diaphragm 3 is mounted and hermetically sealed as by means of a soldering operation. A rotary vane type of pump indicated generally at 1% 18 mounted in any suitable manner on the bottom of the casing 1 with its shaft 4 protruding concentrically into The shaft 4 carries a disc-shaped rotor 5 (Fig. 3) having radial slots 6 in which rectangular vanes 7 are slidably mounted for cooperation with the interior of an eccentric pump chamber 8 formed in the pump casing 9. The pump 10 is provided with an inlet 11 (Fig. 5), an outlet 12 (Fig. 2) and a spring loaded by-pass valve connection 13, together with suitable ports and passages as indicated more particularly in Figs. 1, 3 and 5, whereby rotation of the pump shaft 4 causes liquid in which the pump is immersed to enter the inlet 11, and be forced out of the outlet 12.
The upper end of the casing 1 is closed by a mounting plate 14- arranged to be bolted to the top of a fuel tank 15 as indicated at 16, a gasket 17 being interposed to prevent leakage from the tank. A driving motor 18 is carried by the mounting plate 14 and attached thereto by bolts and nuts as indicated at 19. The motor shaft 2,779,513 C Fatented Jan. 29, 1957 21 extends into the upper chamber of the cup-shaped housing 1 in alignment with the pump shaft 4.
Magnetic means for coupling the motor shaft 21 to the pump shaft 4 is provided comprising a hollow stub shaft 22 slidably journalled on the motor shaft 21 and connected for rotation therewith by a cross pin 23 engaging in slots 24 in the stub shaft 22. A mounting cup 25 is fixedly mounted on the stub shaft 22 and has seated therein a flat ring magnet member 26 having a series of alternating magnetic poles formed on its surface as best shown in Fig. 6. It is preferred that this magnet be formed of a material having very high permanent coercive force such as the materials now available formed of sintered ceramic material, one form of which is known to the trade by the name of Indox.
The ring magnet 26 is held in the cup 25 by any suitable means as by an outer cup member Zil of non-magnetic material having its rim bent inwardly against a beveled surface of the magnet as shown in Fig. l. The magnet is maintained in closely spaced relation to the diaphragm 3 by means of a thrust bearing 27 for the stub shaft 22, the stationary cup 36 of which thrust bearing rests directly on said diaphragm.
A similar permanent magnet 28 is mounted on a hollow stub shaft 29 by means of a mounting cup 31. The stub shaft 29 is slidably journalled on the end of the pump shaft 4 and is connected to rotate with the pump shaft by a cross pin 32. Magnet 28 is spaced from the diaphragm 3 by means of a thrust bearing 33 the stationary cup of which rests against the under side of the diaphragm 3. Both the stub shafts 22 and 29 are drawn toward the diaphragm 3 by the mutual attraction of the two face-polarized ring magnets 26 and 23.
An outlet fitting comprising a nipple 35 is located in the mounting plate 14 and extends downward through the rim of the casing 1, the joint being sealed by the gasket 17. A similar nipple 34 extends upwardly from the pump outlet 12 in alignment with the nipple 35 and a hose 36 is arranged to be clamped on the nipples as 3 is then inserted in the casing and soldered to the shoulder 2 of the casing to form a permanent fluid-tight partition between the upper and lower chambers of the casing.
The motor 18 is then attached to the mounting plate 14, the driving coupling member including the magnet 26 and shaft 22 is slid on the motor shaft 21, the outlet hose 36 is attached to the nipples 34 and 35 of the pump and outlet fitting, and the assembly is then inserted in the tank and attached thereto by means of the bolts 16.
Energization of the motor is transmitted through the magnetic coupling to the pump which operates in conventional manner to draw liquid in the inlet 11 of the pump and develop pressure in the outlet 12. The output of the pump which is in excess of the fuel consumed by the device, such as an internal combustion engine, to be supplied thereby is permitted to escape back into the fuel tank through the spring pressed relief valve 13.
It will be appreciated that since the ring magnets 26 and 28 are merely maintained in alignment by the motor shaft 21 and pump shaft 4 respectively, while their spacing from the diaphragm 3 is maintained by the thrust bearings 27 and 33 resting directly thereon, the magnets will be kept in the desired close proximity to each other without the necessity for close adjustment of either the motor or the pump.
In order to permit circulation of liquid through the lower chamber it is preferably vented to the fuel tank as 7 indicated at '40. The upper chamber is also'preferably vented to the atmosphere bymeans of slots for the bolts 19 in the mounting plate 14.
Although but one embodiment of the invention has been shown and described in detail it will be understood that other forms are possible and changes maybe made in the design and arrangement of the parts without departing from the spiritof the invention.
1 claim:
1. In a tank-mounted rotary fuel pump, a cup-shaped casing, an impervious non-magnetic diaphragm dividing the casing into upper and lower chambers, a "pump mounted on the bottom 'of the casing having a shaft extending into the lower chamber toward said diaphragm normal thereto, a stub shaft mounted on'the pump shaft and slidably but'non-rotatably connected thereto, 'a facepolarized disc magnet rigidly mounted on the stub shaft in parallel relation and in proximity to the diaphragm, and a thrust bearing for the stub shaft resting on said diaphragm and controlling the spacing of'the disc magnet from the diaphragm; a mounting plate fixed to and closing the upper chamber of the casing, ;a motor mounted thereon having a shaft extending into said upper chamber in alinernent with "the pump shaft, and a face-polarized disc magnet mounted on the motor shaft to rotate therewith parallel to and in close proximity to the diaphragm.
2. A tank-mounted fuel pump as set forth in claim 1 including further a hollow stubshaft telescopically splined on the motor shaft, the latter-mentioned disc magnet being mounted :rigidly on said hollow stub shaft; and a thrust bearing for said stub shaft resting on the diaphragm and controlling the spacing of the .latter-mentioneddisc magnet therefrom.
3. Atank=mountedfuel pump as set forth in claim 1 in which the motorrmounting plateserves-also as a closure for the tank in which the pump is mounted, and said diaphragm is tightly sealed in the casing to prevent passage of liquid from one chamber to the other.
4. A tank-mounted pump as ,set forth in claim v3 in which the lower chamber is vented into the tank, while the upper chamber is vented to the. outside of the tank.
No references cited.
an, an...
US583185A 1956-05-07 1956-05-07 Submerged rotary type fuel pump Expired - Lifetime US2779513A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US583185A US2779513A (en) 1956-05-07 1956-05-07 Submerged rotary type fuel pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US583185A US2779513A (en) 1956-05-07 1956-05-07 Submerged rotary type fuel pump

Publications (1)

Publication Number Publication Date
US2779513A true US2779513A (en) 1957-01-29

Family

ID=24332029

Family Applications (1)

Application Number Title Priority Date Filing Date
US583185A Expired - Lifetime US2779513A (en) 1956-05-07 1956-05-07 Submerged rotary type fuel pump

Country Status (1)

Country Link
US (1) US2779513A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2947259A (en) * 1957-12-06 1960-08-02 Tokheim Corp Motor-pump unit for automotive fuel
US2951447A (en) * 1958-07-31 1960-09-06 Gen Motors Corp Impeller pumps with magnentic drives
US2968248A (en) * 1957-12-16 1961-01-17 Gen Motors Corp Magnetic drive impeller pump
US3035442A (en) * 1957-09-16 1962-05-22 Badger Meter Mfg Co Coupling means for fluid meters
US3158295A (en) * 1962-03-14 1964-11-24 F E Myers & Bro Co Submersible pump
US3158025A (en) * 1962-04-13 1964-11-24 Worthington Corp Magnetic driver for flowmeter
US3256736A (en) * 1962-11-07 1966-06-21 Rockwell Mfg Co Fluid meters
US3310693A (en) * 1964-02-04 1967-03-21 Gray & Huleguard Inc Magnetic coupling
US3415195A (en) * 1967-06-05 1968-12-10 Walbro Corp Magnetic drive pump
US3470824A (en) * 1968-09-12 1969-10-07 Walbro Corp Magnetic drive pump
US4767378A (en) * 1985-08-01 1988-08-30 Siemens Aktiengesellschaft Frontal magnet coupling with integrated magnetic bearing load relief
WO2000029741A1 (en) * 1998-11-12 2000-05-25 Volvo Lastvagnar Ab Fuel delivery system
US6543217B2 (en) 2000-05-10 2003-04-08 Volvo Car Corporation System for determining the effectiveness of a catalytic coating on a catalytic converter in a motor vehicle
US6974052B1 (en) * 1999-06-21 2005-12-13 Sara Lee/De N.V. Dosing device adapted for dispensing a concentrate from a holder in a metered manner

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3035442A (en) * 1957-09-16 1962-05-22 Badger Meter Mfg Co Coupling means for fluid meters
US2947259A (en) * 1957-12-06 1960-08-02 Tokheim Corp Motor-pump unit for automotive fuel
US2968248A (en) * 1957-12-16 1961-01-17 Gen Motors Corp Magnetic drive impeller pump
US2951447A (en) * 1958-07-31 1960-09-06 Gen Motors Corp Impeller pumps with magnentic drives
US3158295A (en) * 1962-03-14 1964-11-24 F E Myers & Bro Co Submersible pump
US3158025A (en) * 1962-04-13 1964-11-24 Worthington Corp Magnetic driver for flowmeter
US3256736A (en) * 1962-11-07 1966-06-21 Rockwell Mfg Co Fluid meters
US3310693A (en) * 1964-02-04 1967-03-21 Gray & Huleguard Inc Magnetic coupling
US3415195A (en) * 1967-06-05 1968-12-10 Walbro Corp Magnetic drive pump
US3470824A (en) * 1968-09-12 1969-10-07 Walbro Corp Magnetic drive pump
US4767378A (en) * 1985-08-01 1988-08-30 Siemens Aktiengesellschaft Frontal magnet coupling with integrated magnetic bearing load relief
WO2000029741A1 (en) * 1998-11-12 2000-05-25 Volvo Lastvagnar Ab Fuel delivery system
US6539926B2 (en) 1998-11-12 2003-04-01 Volvo Lastvagner Ab Fuel delivery system
US6974052B1 (en) * 1999-06-21 2005-12-13 Sara Lee/De N.V. Dosing device adapted for dispensing a concentrate from a holder in a metered manner
US6543217B2 (en) 2000-05-10 2003-04-08 Volvo Car Corporation System for determining the effectiveness of a catalytic coating on a catalytic converter in a motor vehicle

Similar Documents

Publication Publication Date Title
US2779513A (en) Submerged rotary type fuel pump
US3911300A (en) Encapsulated wet dynamoelectric machine rotor
US4065234A (en) Magnetically driven rotary pumps
US3802804A (en) Magnetically coupled pump structure
US2370590A (en) Motor pump unit
US4212601A (en) Motor pump
US2807395A (en) Electric fuel pump mounting
US2752857A (en) Motor pump unit with axial gap motor
US1694805A (en) Fuel-supply system for internal-combustion engines
US2709965A (en) Motor driven pump
US2951447A (en) Impeller pumps with magnentic drives
US3014623A (en) Motor and pump mounting means
US2430509A (en) Shaft seal for submersible pumps
US2239228A (en) Pump mechanism
US3525578A (en) Vacuum pump
GB1462937A (en) Pump for liquids
US4218196A (en) Motor fuel pump
US2968248A (en) Magnetic drive impeller pump
US2423825A (en) Motor pump unit
US2624286A (en) Submerged pump and motor assembly
US3322071A (en) Pump
US2312525A (en) Pump construction
US2263091A (en) Fuel pump
US2343752A (en) Pump pressure limiting device
GB1039165A (en) Improvements in or relating to reciprocating fluid pumps