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GB655727A - Improvements in or relating to fuel-systems for internal-combustion engines - Google Patents

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

Info

Publication number
GB655727A
GB655727A GB1483148A GB1483148A GB655727A GB 655727 A GB655727 A GB 655727A GB 1483148 A GB1483148 A GB 1483148A GB 1483148 A GB1483148 A GB 1483148A GB 655727 A GB655727 A GB 655727A
Authority
GB
United Kingdom
Prior art keywords
fuel
orifice
chamber
capsule
pressure
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
GB1483148A
Inventor
George Howard Farmer
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB1483148A priority Critical patent/GB655727A/en
Publication of GB655727A publication Critical patent/GB655727A/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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/30Control of fuel supply characterised by variable fuel pump output
    • 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
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/16Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors
    • F02M69/18Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors the means being metering valves throttling fuel passages to injectors or by-pass valves throttling overflow passages, the metering valves being actuated by a device responsive to the engine working parameters, e.g. engine load, speed, temperature or quantity of air
    • 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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/18Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice
    • F02M7/20Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice operated automatically, e.g. dependent on altitude

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

655,727. Regulating; spray carburetters. ROLLS-ROYCE, Ltd. June 1, 1948, No. 14831. [Classes 7(iii) and 7(vi)] [Also in Groups XXVI and XXIX] The fuel flow to an engine is corrected by a device responsive to variations in fuel temperature. In Fig. 3 fuel entering at 33a is delivered by a rotary pump 35 to an orifice 40, controlled by a valve 39 moved in one direction by a diaphragm 42 subject to the pressure drop across metering orifices 45, 46, and in the opposite direction by a centrifugal governor 38 carried by the pump rotor and flows from the orifice 40 through the metering orifices 45, 46 to chamber 43 containing the outlet 33b. The orifice 46 is controlled by a needle valve 48 carried by capsule 49 in a chamber 50 connected by a pipe 51 to the engine intake pressure or supercharger delivery pressure, some of the capsules 49 being evacuated and the remainder open to atmospheric pressure. The orifice 45 is controlled by a needle valve 52 connected to a lever 53 pivoted at both ends to thermometric devices comprising liquid-filled capsules 54, 57 connected respectively to a bulb 55 in the air intake pipe 56, and to a bulb 59 in the fuel pipe 60 leading to the inlet 33a, the flow through orifice 45 being decreased as the air temperature increases, and increased as the fuel temperature increases. In a modification, Figs. 1 and 2, a pump 16 with a constant pressure byepass valve 20 delivers to a metering pump 17 connected by pipe 17a to a chamber 25, Fig. 2, the outlet 19a of which leads to an injection nozzle 14. The outlet of pump 16 is connected by a pipe 22 to a chamber 24 connected to the chamber 25 by an orifice 26a in a sliding spring-loaded plate 26 carried by an annular capsule 29 open internally to the supercharge pressure through a pipe 23. A needle valve 31 controlling the orifice 26a is carried by a capsule 32 responsive to the fuel temperature. If the boost pressure increases the plate 26 is moved to the right to increase the size of orifice 26a, the fuel supply to the engine being thereby increased by fuel flowing from chamber 24 to chamber 25, and if the fuel temperature increases the valve 31 is moved to the left to increase the fuel supply. As applied to a suction carburetter, Fig. 4, having a nozzle 62 delivering atomized fuel into the induction pipe 61, the fuel being supplied from a chamber 64 through an orifice 65 to a space 63 where it is mixed with air entering through a passage 66, the orifice 65 is controlled by a needle valve 65b, actuated by a capsule 73 subjected to intake air pressure or boost-pressure, and is formed in a plate 65a movable by a capsule 76 in accordance with variations in fuel temperature. In a modification a float chamber feeds a main nozzle through a submerged jet and an auxiliary nozzle through a second jet controlled according to fuel temperature by a valve actuated by a capsule immersed in the fuel in the float chamber. As applied to a gas-turbine engine, Fig. 6, comprising a swash-plate pump 92 delivering through a throttle valve 94 to the burners 96, the pump delivery is controlled by a servo-piston 98 moved in response to the opening and closing of an orifice 102<SP>1</SP> by a valve 104, loaded by a spring 109 and controlled by the pump outlet pressure acting on a piston 114 and atmospheric pressure acting on a capsule 110, and a capsule 115 immersed in the fuel in chamber 103 varies the force of the spring 109 in accordance with variations in fuel temperature.
GB1483148A 1948-06-01 1948-06-01 Improvements in or relating to fuel-systems for internal-combustion engines Expired GB655727A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1483148A GB655727A (en) 1948-06-01 1948-06-01 Improvements in or relating to fuel-systems for internal-combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1483148A GB655727A (en) 1948-06-01 1948-06-01 Improvements in or relating to fuel-systems for internal-combustion engines

Publications (1)

Publication Number Publication Date
GB655727A true GB655727A (en) 1951-08-01

Family

ID=10048240

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1483148A Expired GB655727A (en) 1948-06-01 1948-06-01 Improvements in or relating to fuel-systems for internal-combustion engines

Country Status (1)

Country Link
GB (1) GB655727A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197391A (en) * 1986-11-14 1988-05-18 Rolls Royce Plc Fuel system for gas turbine aero engine
WO2008006840A1 (en) * 2006-07-13 2008-01-17 Inergy Automotive Systems Research (Société Anonyme) System and process for storing an additive and injecting it into the exhaust gases of an engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197391A (en) * 1986-11-14 1988-05-18 Rolls Royce Plc Fuel system for gas turbine aero engine
WO2008006840A1 (en) * 2006-07-13 2008-01-17 Inergy Automotive Systems Research (Société Anonyme) System and process for storing an additive and injecting it into the exhaust gases of an engine

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