GB892692A - Gas turbine engine with fuel filter systems - Google Patents

Gas turbine engine with fuel filter systems

Info

Publication number
GB892692A
GB892692A GB40519/60A GB4051960A GB892692A GB 892692 A GB892692 A GB 892692A GB 40519/60 A GB40519/60 A GB 40519/60A GB 4051960 A GB4051960 A GB 4051960A GB 892692 A GB892692 A GB 892692A
Authority
GB
United Kingdom
Prior art keywords
valve
fuel
directed
filter
passes
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
GB40519/60A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB892692A publication Critical patent/GB892692A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • F02M37/22Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines, e.g. arrangements in the feeding system
    • F02M37/32Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines, e.g. arrangements in the feeding system characterised by filters or filter arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Mechanically-Actuated Valves (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

892,692. Filters in parallel; backflushing. GENERAL MOTORS CORPORATION. Nov. 25, 1960 [Nov. 27, 1959], No. 40519/60. Class 46. In the position shown, gas-turbine fuel is boosted at 16 and passing along conduit 20 is directed by valve 28 through a filter 34, and the filtered fuel is directed by valve 30 to main pump 14, whence it passes into a control unit 12. Most of the fuel passes at 10 to the engine but the excess passes along conduit 52 and is directed by valve 30 backwards through a filter 32, the resulting suspension of fuel and residue being directed by valve 28 along conduit 64 to be separated in a density centrifuge 66 and the thus-cleaned fuel being added to conduit 20 at 82. A drum cam 96 driven by the centrifuge impeller 68 through reduction gearing (ratio e.g. 1 : 10,000) periodically changes-over the valves 28, 30 simultaneously through linkage 86 to 94 so as to transpose the functions of the filters 32, 34. Alternatively the valve movement may take place in response to a predetermined pressure drop across the filter in use.
GB40519/60A 1959-11-27 1960-11-25 Gas turbine engine with fuel filter systems Expired GB892692A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US892692XA 1959-11-27 1959-11-27

Publications (1)

Publication Number Publication Date
GB892692A true GB892692A (en) 1962-03-28

Family

ID=22216662

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40519/60A Expired GB892692A (en) 1959-11-27 1960-11-25 Gas turbine engine with fuel filter systems

Country Status (1)

Country Link
GB (1) GB892692A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2210305A1 (en) * 1969-11-04 1973-09-13 Trw Inc FLOW SYSTEM, IN PARTICULAR FUEL SYSTEM FOR POWER PLANTS
FR2173829A1 (en) * 1972-03-03 1973-10-12 Trw Inc
DE2640362A1 (en) * 1975-09-12 1977-03-24 Rolls Royce 1971 Ltd FUEL SYSTEM FOR GAS TURBINE ENGINES
GB2227953A (en) * 1989-01-13 1990-08-15 Gen Electric Fluid transfer device
GB2348830A (en) * 1999-04-12 2000-10-18 Federal Mogul Eng Ltd Liquid cleaning arrangement including duplex filter and centrifugal separator therefor
DE10013905A1 (en) * 2000-03-21 2001-09-27 Mannesmann Vdo Ag Conveying device for conveying fuel
RU2446858C2 (en) * 2010-05-18 2012-04-10 Анатолий Васильевич Смульский Separation filter unit
ITTO20120268A1 (en) * 2012-03-26 2013-09-27 Assytech S R L PURIFICATION SYSTEM FOR FUELS
FR2999652A1 (en) * 2012-12-18 2014-06-20 Snecma FUEL CIRCUIT OF A TURBOMACHINE

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2210305A1 (en) * 1969-11-04 1973-09-13 Trw Inc FLOW SYSTEM, IN PARTICULAR FUEL SYSTEM FOR POWER PLANTS
FR2173829A1 (en) * 1972-03-03 1973-10-12 Trw Inc
DE2640362A1 (en) * 1975-09-12 1977-03-24 Rolls Royce 1971 Ltd FUEL SYSTEM FOR GAS TURBINE ENGINES
GB2227953A (en) * 1989-01-13 1990-08-15 Gen Electric Fluid transfer device
GB2348830A (en) * 1999-04-12 2000-10-18 Federal Mogul Eng Ltd Liquid cleaning arrangement including duplex filter and centrifugal separator therefor
DE10013905A1 (en) * 2000-03-21 2001-09-27 Mannesmann Vdo Ag Conveying device for conveying fuel
US6422213B2 (en) 2000-03-21 2002-07-23 Mannesmann Vdo Ag Delivery device for delivering fuel
RU2446858C2 (en) * 2010-05-18 2012-04-10 Анатолий Васильевич Смульский Separation filter unit
ITTO20120268A1 (en) * 2012-03-26 2013-09-27 Assytech S R L PURIFICATION SYSTEM FOR FUELS
FR2999652A1 (en) * 2012-12-18 2014-06-20 Snecma FUEL CIRCUIT OF A TURBOMACHINE
US9650960B2 (en) 2012-12-18 2017-05-16 Snecma Fuel circuit of a turbine engine

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