JPS5664122A - Foreign matter particle separator for gas turbine engine - Google Patents

Foreign matter particle separator for gas turbine engine

Info

Publication number
JPS5664122A
JPS5664122A JP13591980A JP13591980A JPS5664122A JP S5664122 A JPS5664122 A JP S5664122A JP 13591980 A JP13591980 A JP 13591980A JP 13591980 A JP13591980 A JP 13591980A JP S5664122 A JPS5664122 A JP S5664122A
Authority
JP
Japan
Prior art keywords
gas turbine
foreign matter
turbine engine
particle separator
matter particle
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.)
Pending
Application number
JP13591980A
Other languages
English (en)
Inventor
Ueinsutein Bariii
Suteyaa Uiriamu
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.)
General Electric Co
Original Assignee
General Electric 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 General Electric Co filed Critical General Electric Co
Publication of JPS5664122A publication Critical patent/JPS5664122A/ja
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Cyclones (AREA)
  • Separating Particles In Gases By Inertia (AREA)
JP13591980A 1979-10-01 1980-10-01 Foreign matter particle separator for gas turbine engine Pending JPS5664122A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/080,854 US4265646A (en) 1979-10-01 1979-10-01 Foreign particle separator system

Publications (1)

Publication Number Publication Date
JPS5664122A true JPS5664122A (en) 1981-06-01

Family

ID=22160062

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13591980A Pending JPS5664122A (en) 1979-10-01 1980-10-01 Foreign matter particle separator for gas turbine engine

Country Status (8)

Country Link
US (1) US4265646A (ja)
JP (1) JPS5664122A (ja)
CA (1) CA1136866A (ja)
DE (1) DE3036525A1 (ja)
FR (1) FR2466617A1 (ja)
GB (1) GB2058929A (ja)
IL (1) IL61028A0 (ja)
IT (1) IT1133141B (ja)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012117534A (ja) * 2010-11-30 2012-06-21 General Electric Co <Ge> 入口粒子分離システム

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US8087885B2 (en) * 2004-12-01 2012-01-03 United Technologies Corporation Stacked annular components for turbine engines
US7874163B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Starter generator system for a tip turbine engine
WO2006059971A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
US8104257B2 (en) * 2004-12-01 2012-01-31 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
EP1828545A2 (en) 2004-12-01 2007-09-05 United Technologies Corporation Annular turbine ring rotor
EP1828591B1 (en) * 2004-12-01 2010-07-21 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006059978A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Cantilevered tip turbine engine
US7887296B2 (en) 2004-12-01 2011-02-15 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
WO2006059973A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with a heat exchanger
EP1834067B1 (en) 2004-12-01 2008-11-26 United Technologies Corporation Fan blade assembly for a tip turbine engine and method of assembly
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
WO2006110124A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006059990A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
US8757959B2 (en) 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
EP1828547B1 (en) 2004-12-01 2011-11-30 United Technologies Corporation Turbofan comprising a plurality of individually controlled inlet guide vanes and corresponding controlling method
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
WO2006060009A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
US7921636B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
DE602004016065D1 (de) 2004-12-01 2008-10-02 United Technologies Corp Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
DE602004020125D1 (de) 2004-12-01 2009-04-30 United Technologies Corp Schmiermittel-versorgungssystem für das getriebe eines tip-turbinen-triebwerks
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
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US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
RU2293195C2 (ru) * 2005-01-17 2007-02-10 Ирина Федоровна Алавердова Газотурбинная энергоустановка
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012117534A (ja) * 2010-11-30 2012-06-21 General Electric Co <Ge> 入口粒子分離システム

Also Published As

Publication number Publication date
FR2466617A1 (fr) 1981-04-10
US4265646A (en) 1981-05-05
DE3036525A1 (de) 1981-04-16
IT8024868A0 (it) 1980-09-24
IT1133141B (it) 1986-07-09
CA1136866A (en) 1982-12-07
IL61028A0 (en) 1980-11-30
GB2058929A (en) 1981-04-15

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