GB881002A - Improvements in or relating to liquid fuel supply systems - Google Patents

Improvements in or relating to liquid fuel supply systems

Info

Publication number
GB881002A
GB881002A GB1093458A GB1093458A GB881002A GB 881002 A GB881002 A GB 881002A GB 1093458 A GB1093458 A GB 1093458A GB 1093458 A GB1093458 A GB 1093458A GB 881002 A GB881002 A GB 881002A
Authority
GB
United Kingdom
Prior art keywords
filter
fuel
control unit
heater
ice
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
GB1093458A
Inventor
Frederick William Walto Morley
David Morris Brown
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 GB1093458A priority Critical patent/GB881002A/en
Publication of GB881002A publication Critical patent/GB881002A/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
    • F02C7/224Heating fuel before feeding to the burner
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D35/00Filtering devices having features not specifically covered by groups B01D24/00 - B01D33/00, or for applications not specifically covered by groups B01D24/00 - B01D33/00; Auxiliary devices for filtration; Filter housing constructions
    • B01D35/12Devices for taking out of action one or more units of multi- unit filters, e.g. for regeneration

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

881,002. Filters. ROLLS-ROYCE Ltd. March 12, 1959 [April 3, 1958], No. 10934/58. Class 46. [Also in Group XXVI] A liquid fuel supply system for a gas turbine comprising a fuel filter and downstream of it a unit, e.g. a fuel supply control unit, in which ice formation is liable to cause malfunctioning, has means arranged on sensing of ice formation in the filter, to heat the unit prior to the heating of the filter for de-icing purposes whereby water formed by melting of ice in the filter flows through the unit without freezing therein. Fuel from a tank 16 is delivered by a booster pump 17 into a fuel pipe 18 containing a fuel heater 19 heated by air tapped from the engine compressor 10 by a conduit 20. The air flow is controlled by a valve 21 operated by a solenoid 21a. The fuel leaving the heater 19 normally passes through a valve 29, a main filter 24 high pressure fuel pump 22, control mechanism 25 and shut off cock 26 to the engine. The system also comprises an auxiliary fuel filter 27. When ice clogs the filter 24, the pressure drop across it increases and causes the collapse of the bellows 34 so that switch 35 is closed. This energises the solenoid 21a which opens valve 21 and allows hot air to be supplied to the heater 19. At the same time the motor 31 is operated to rotate cam 30. This allows spring 29b to urge valve member 29a to the left so that fuel is supplied to the control unit 25 through the auxiliary filter 27. After a period of ninety seconds the cam 30 starts to move the valve member 29a to the right so that for about fifteen seconds both filters are fed with heated fuel. Thereafter, fuel is fed to the filter 24 only. During the periods when hot fuel is fed to the filter 24, the ice in the filter is melted and due to the previous heating of the control unit, the resulting water flows through the control mechanism without freezing. The motor 31 also rotates a cam 30a which closes a holding switch 35a for one revolution of the motor. In a modification, Figs. 2 and 3 (not shown), the control unit and filter have control valves and connecting ducting arranged so that in one setting of the valves the heater is arranged between the filter and the control unit and in the second setting, the filter is arranged between the heater and the control unit.
GB1093458A 1958-04-03 1958-04-03 Improvements in or relating to liquid fuel supply systems Expired GB881002A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1093458A GB881002A (en) 1958-04-03 1958-04-03 Improvements in or relating to liquid fuel supply systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1093458A GB881002A (en) 1958-04-03 1958-04-03 Improvements in or relating to liquid fuel supply systems

Publications (1)

Publication Number Publication Date
GB881002A true GB881002A (en) 1961-11-01

Family

ID=9977001

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1093458A Expired GB881002A (en) 1958-04-03 1958-04-03 Improvements in or relating to liquid fuel supply systems

Country Status (1)

Country Link
GB (1) GB881002A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1061243A3 (en) * 1999-06-16 2004-02-11 ROLLS-ROYCE plc An apparatus for and a method of filtering a fluid
FR2944216A1 (en) * 2009-04-14 2010-10-15 Snecma METHOD FOR DETECTING A CRISPING STATUS OR MAINTENANCE NEED FOR A TURBOMACHINE FUEL CIRCUIT
WO2012069745A1 (en) * 2010-11-26 2012-05-31 Snecma Monitoring of a filter of the fuel-supply system of an aircraft engine
CN108310854A (en) * 2018-01-23 2018-07-24 北京东方通捷燃气有限责任公司 A kind of gas filter and its combustion gas Gao Peizhan of application

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1061243A3 (en) * 1999-06-16 2004-02-11 ROLLS-ROYCE plc An apparatus for and a method of filtering a fluid
FR2944216A1 (en) * 2009-04-14 2010-10-15 Snecma METHOD FOR DETECTING A CRISPING STATUS OR MAINTENANCE NEED FOR A TURBOMACHINE FUEL CIRCUIT
WO2010119215A1 (en) * 2009-04-14 2010-10-21 Snecma Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
WO2012069745A1 (en) * 2010-11-26 2012-05-31 Snecma Monitoring of a filter of the fuel-supply system of an aircraft engine
FR2968040A1 (en) * 2010-11-26 2012-06-01 Snecma MONITORING A FILTER FOR THE FUEL SUPPLY CIRCUIT OF AN AIRCRAFT ENGINE
CN103249930A (en) * 2010-11-26 2013-08-14 斯奈克玛 Monitoring of a filter of the fuel-supply system of an aircraft engine
US8781709B2 (en) 2010-11-26 2014-07-15 Snecma Monitoring of a filter of the fuel-supply system of an aircraft engine
CN103249930B (en) * 2010-11-26 2016-01-13 斯奈克玛 The monitoring of airplane engine fuel oil supply system filter
RU2599084C2 (en) * 2010-11-26 2016-10-10 Снекма Monitoring filter of fuel-supply system of aircraft engine
CN108310854A (en) * 2018-01-23 2018-07-24 北京东方通捷燃气有限责任公司 A kind of gas filter and its combustion gas Gao Peizhan of application

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