GB719469A - 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
GB719469A
GB719469A GB21432/51A GB2143251A GB719469A GB 719469 A GB719469 A GB 719469A GB 21432/51 A GB21432/51 A GB 21432/51A GB 2143251 A GB2143251 A GB 2143251A GB 719469 A GB719469 A GB 719469A
Authority
GB
United Kingdom
Prior art keywords
valve
centrifugal
fuel
impeller
compressor
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
GB21432/51A
Inventor
Albert Jubb
John Shaw Hollings
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 GB21432/51A priority Critical patent/GB719469A/en
Publication of GB719469A publication Critical patent/GB719469A/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
    • F02C9/16Control of working fluid flow
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

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

Abstract

719,469. Gas turbine plant; centrifugal pumps; centrifugal governors. ROLLS-ROYCE, Ltd. Sept. 11, 1952 [Sept. 11, 1951], No. 21432/51. Classes 57, 110(1) and 110(3) A fuel system for a gas turbine plant comprises a centrifugal fuel pump having flow-restricting means connected with its delivery and flow-metering means in its inlet, the flow-metering means being controlled by a speed governor sensitive to a rotational speed to be governed, the arrangement being such that in operation of the pump the radial depth of fuel in the pump impeller is less than the impeller radius. The fuel tank 14, Fig. 1. is pressurized by connecting it through a pipe 44 to an intermediate stage of the compressor 10 of the gas turbine plant or through a pipe 45 to the delivery of the compressor. Fuel passes to the eye of the fuel pump impeller 20, Fig. 5, by way of a duct 15 and a valve 39. A centrifugal governor 29 driven, together with the impeller 20, from the rotor 10 a of the compressor 10, tends to close the valve 39 against the combined effect of a spring 42 and the pressure exerted on a flexible diaphragm 50. The diaphragm 50 is subjected on one side to the pressure within a chamber 51. This pressure is a fixed proportion of the compressor delivery pressure and may be obtained by connecting the chamber 51 by way of a duct 52 to the pipe 44 or 45. The cavity 21 is vented to atmosphere through pipes 54, 43. In a modification, Figs. 2 and 4, the diaphragm 50 is omitted, and the stem 37 of the valve 39 is made hollow to provide a passage connecting the cavity 21 to the vent pipe 43. The centrifugal governor 29 comprises bob weights 30 secured to the ends of a spring steel strip 34 overlying the end of the stem 37 and to the ends of spring steel strips 31 carried by lugs 32 projecting from a boss 33 secured to the impeller 20. The bob weights 30 have inwardly extending arms 35 ending in knife edges 36 which bear upon the centre of the strip 34 to load the valve 39. The centrifugal governor 29 may be replaced by a hydraulic governor comprising a fixed capacity pump driven at the speed to be governed and delivering liquid through an orifice which may be adjustable, the pressure drop across the orifice being applied to a piston which moves the valve 39 against a resilient load which may be adjustable. Specification 709,002 is referred to.
GB21432/51A 1951-09-11 1951-09-11 Improvements in or relating to fuel systems for internal combustion engines Expired GB719469A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21432/51A GB719469A (en) 1951-09-11 1951-09-11 Improvements in or relating to fuel systems for internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21432/51A GB719469A (en) 1951-09-11 1951-09-11 Improvements in or relating to fuel systems for internal combustion engines

Publications (1)

Publication Number Publication Date
GB719469A true GB719469A (en) 1954-12-01

Family

ID=10162853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21432/51A Expired GB719469A (en) 1951-09-11 1951-09-11 Improvements in or relating to fuel systems for internal combustion engines

Country Status (1)

Country Link
GB (1) GB719469A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197911A (en) * 1986-07-28 1988-06-02 Teledyne Ind Fuel supply path in a gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197911A (en) * 1986-07-28 1988-06-02 Teledyne Ind Fuel supply path in a gas turbine engine
GB2197911B (en) * 1986-07-28 1991-03-20 Teledyne Ind Turbine shaft fuel pump

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