[go: up one dir, main page]

GB612624A - Improvements in or relating to fuel supply systems for internal combustion engines - Google Patents

Improvements in or relating to fuel supply systems for internal combustion engines

Info

Publication number
GB612624A
GB612624A GB10084/46A GB1008446A GB612624A GB 612624 A GB612624 A GB 612624A GB 10084/46 A GB10084/46 A GB 10084/46A GB 1008446 A GB1008446 A GB 1008446A GB 612624 A GB612624 A GB 612624A
Authority
GB
United Kingdom
Prior art keywords
pump
valve
delivery
pressure
fuel
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
Application number
GB10084/46A
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.)
DAVID HAVELOCH BALLANTYNE
Original Assignee
DAVID HAVELOCH BALLANTYNE
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 DAVID HAVELOCH BALLANTYNE filed Critical DAVID HAVELOCH BALLANTYNE
Publication of GB612624A publication Critical patent/GB612624A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/236Fuel delivery systems comprising two or more pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

612,624. Fluid - pressure servomotors. HOOKER, S. G., and BALLANTYNE, D. H. April 1, 1946, No. 10084. [Class 135] [Also in Group XXVII] In a fuel supply system for an internalcombustion engine comprising two or more pumps having regulating means adjusted by a common hydraulic control, means are provided for isolating one or more regulating means from the common control, whereby one or more pumps are rendered inoperative and the rate of delivery of the others is increased. As applied to a jet-propulsion engine, two swashplate pumps 16, 17 delivering through pipes 31 into a common pipe 28 leading to the engine through a throttle valve 29, are controlled by the pressure of fuel on the opposite sides of pistons 34 connected to the angularly adjustable swash-plates 21. The delivery pressure acting on a piston 39 controls a lever 40 pivoted in a diaphragm 14 and controlling a valve 41 allowing fuel to flow through orifices 36 and pipes 44, the pressure drop across the orifices controlling the pistons 34 and hence the pump deliveries. A capsule 43 adjusts the lever 40 according to altitude and the centrifugal pressure set up by the pump rotors 18 acts on diaphragms 47 which open valves 46 above a certain speed, bleeding fuel through the orifices 36 and reducing the pump deliveries. Closing of a manually-operated valve 49 causes an increase of pressure on the right-hand side of piston 34 of pump 17, increasing its delivery. Hence, if pump 16 should fail or its delivery cease due to sticking open of its valve 46 or the valve 41, the pump 17 will maintain the fuel supply on closing of the valve 49. Alternatively, if the pump 17 fails or its valve 46 sticks open, the drop in pressure in pipe 28 closes the valve 41 which causes the delivery of the pump 16 to be increased. Similarly, if the pipe 44<1> is punctured, closure of the valve 49 increases the delivery of pump 17 and the loss of pressure in the pipe 44 of pump 16 reduces its delivery to zero. Non-return valves may be provided in the pipes 44 to prevent a pump which has failed being rotated by fuel from the other pump. A governor may be fitted to each of the pumps so that when either is supplying the engine on its own, its stroke is automatically adjusted to give the maximum permissible speed of the engine.
GB10084/46A 1946-04-01 1946-04-01 Improvements in or relating to fuel supply systems for internal combustion engines Expired GB612624A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB267191X 1946-04-01
GB130347X 1947-03-13

Publications (1)

Publication Number Publication Date
GB612624A true GB612624A (en) 1948-11-16

Family

ID=26249458

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10084/46A Expired GB612624A (en) 1946-04-01 1946-04-01 Improvements in or relating to fuel supply systems for internal combustion engines

Country Status (5)

Country Link
US (1) US2517313A (en)
BE (1) BE487119A (en)
CH (1) CH267191A (en)
FR (1) FR945543A (en)
GB (1) GB612624A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2678004A (en) * 1949-09-05 1954-05-11 Lucas Ltd Joseph Control means for liquid fuel pumps
US2753803A (en) * 1950-05-16 1956-07-10 Lucas Ltd Joseph Means for controlling the supply of liquid fuel to the combustion chamber of a prime mover
US2741088A (en) * 1950-09-29 1956-04-10 Rolls Royce Flow control means for internal-combustion engine fuel systems
US2749844A (en) * 1951-11-01 1956-06-12 Bendix Aviat Corp Pump
US2988882A (en) * 1954-03-11 1961-06-20 Rolls Royce Aircraft multi-engine power plant and fuel system therefor
US2864440A (en) * 1954-03-25 1958-12-16 Rolls Royce Fuel systems for gas turbine engine installations
GB0023727D0 (en) * 2000-09-27 2000-11-08 Lucas Industries Ltd Control system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2140633A (en) * 1936-03-17 1938-12-20 Kocks Fritz Means for driving tube drawing benches
US2192539A (en) * 1937-01-15 1940-03-05 Robert S Condon Transmission or the like
US2299234A (en) * 1937-06-09 1942-10-20 Ex Cell O Corp Hydraulic pump and control means therefor
US2237430A (en) * 1939-07-07 1941-04-08 Higgins Eugene Motor and pump transmission

Also Published As

Publication number Publication date
BE487119A (en)
FR945543A (en) 1949-05-06
CH267191A (en) 1950-03-15
US2517313A (en) 1950-08-01

Similar Documents

Publication Publication Date Title
US2405888A (en) Fuel control valve
GB612624A (en) Improvements in or relating to fuel supply systems for internal combustion engines
GB585032A (en) Improvements in governors for internal combustion turbines
GB845269A (en) Improvements in fuel flow control apparatus for gas turbine engines
US2642719A (en) Engine fuel control for internal expansion engine fuel systems
GB1446631A (en) Control apparatus for fuel injection systems of internal combustion engines
US2594790A (en) Fuel system for internal-combustion engines
US2594686A (en) Supercharger for internal-combustion engines
GB681601A (en) Improvements relating to means for controlling liquid fuel pumps of internal combustion engines
GB1278253A (en) Fuel control system for gas turbine engines
GB599502A (en) Improvements in or relating to power plants
GB568054A (en) Improvements in or relating to speed governors
GB688436A (en) Improvements in or relating to fuel supply apparatus for internal-combustion engines
GB674132A (en) Improvements relating to hydraulic speed governors for prime movers
GB649287A (en) Improvements relating to fuel systems for gas-turbine engines
GB834868A (en) An emergency fuel control unit and a fuel system including such a unit
GB605458A (en) Improvements relating to fuel control systems for internal combustion prime movers
GB627419A (en) Improvements relating to fuel-systems for internal combustion engines
GB647585A (en) Improvements relating to control systems for aircraft power plant installations
GB985520A (en) Improved gas turbine engine fuel systems
GB611305A (en) Improvements in or relating to fuel injection systems for internal combustion engines
GB569837A (en) Improvements relating to supercharged internal combustion engines
GB800511A (en) Fuel supply and associated apparatus for internal combustion engines
GB663532A (en) Improvements in or relating to fuel supply systems for internal combustion engines
GB670365A (en) Improvements relating to fluid-operated servo-mechanisms