BE712412A - - Google Patents

Info

Publication number
BE712412A
BE712412A BE712412DA BE712412A BE 712412 A BE712412 A BE 712412A BE 712412D A BE712412D A BE 712412DA BE 712412 A BE712412 A BE 712412A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE712412A publication Critical patent/BE712412A/xx

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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE712412D 1967-04-03 1968-03-19 BE712412A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US62800567A 1967-04-03 1967-04-03

Publications (1)

Publication Number Publication Date
BE712412A true BE712412A (en) 1968-07-31

Family

ID=24517022

Family Applications (1)

Application Number Title Priority Date Filing Date
BE712412D BE712412A (en) 1967-04-03 1968-03-19

Country Status (5)

Country Link
US (1) US3451215A (en)
BE (1) BE712412A (en)
DE (1) DE1626036A1 (en)
FR (1) FR1563248A (en)
GB (1) GB1187171A (en)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3742705A (en) * 1970-12-28 1973-07-03 United Aircraft Corp Thermal response shroud for rotating body
US3748056A (en) * 1971-02-09 1973-07-24 Nissan Motor Turbine blade cooling
US3730640A (en) * 1971-06-28 1973-05-01 United Aircraft Corp Seal ring for gas turbine
FR2185753B1 (en) * 1972-05-26 1976-06-11 Szydlowski Joseph
US3901622A (en) * 1973-05-31 1975-08-26 Gen Motors Corp Yieldable shroud support
US3864056A (en) * 1973-07-27 1975-02-04 Westinghouse Electric Corp Cooled turbine blade ring assembly
US4092824A (en) * 1974-05-28 1978-06-06 Vereinigte Flugtechnische Werke-Fokker Gmbh Method of operating a turbine
US3924581A (en) * 1974-12-06 1975-12-09 Curtiss Wright Corp Doweling construction for rotary engine housing
US4161102A (en) * 1977-10-05 1979-07-17 Teledyne Industries, Inc. Turbine engine starting system
US4268221A (en) * 1979-03-28 1981-05-19 United Technologies Corporation Compressor structure adapted for active clearance control
US5463864A (en) * 1993-12-27 1995-11-07 United Technologies Corporation Fuel nozzle guide for a gas turbine engine combustor
DE19520100A1 (en) * 1995-06-01 1996-12-05 Jean Kuhn Rotational explosion engine
US6032457A (en) * 1996-06-27 2000-03-07 United Technologies Corporation Fuel nozzle guide
US5916142A (en) * 1996-10-21 1999-06-29 General Electric Company Self-aligning swirler with ball joint
US6644033B2 (en) * 2002-01-17 2003-11-11 The Boeing Company Tip impingement turbine air starter for turbine engine
WO2006112807A2 (en) * 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
US7871248B2 (en) * 2007-02-20 2011-01-18 Honeywell International Inc. Airframe mounted electric motor driven lubrication pump control deoil system
US8490408B2 (en) * 2009-07-24 2013-07-23 Pratt & Whitney Canada Copr. Continuous slot in shroud
EP2733314B1 (en) * 2012-11-15 2017-04-05 Safran Aero Boosters SA Radial attachment and positioning flanges for axial turbomachine casing sections
US11073044B2 (en) * 2013-01-21 2021-07-27 Raytheon Technologies Corporation Adjustable floating oil channel for gas turbine engine gear drive
FR3063313B1 (en) * 2017-02-28 2022-10-28 Safran Aircraft Engines AIRCRAFT ENGINE INPUT ARRANGEMENT INCLUDING A MECHANICAL DECOUPLER
US11085309B2 (en) 2017-09-22 2021-08-10 General Electric Company Outer drum rotor assembly
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
CN114151228B (en) * 2022-02-09 2022-04-22 中国航发四川燃气涡轮研究院 Method for dividing binary vector spray pipe regulating sheet into discrete cold air areas

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457833A (en) * 1943-02-03 1949-01-04 Westinghouse Electric Corp Cartridge starter for combustion gas turbines
US2959919A (en) * 1958-01-02 1960-11-15 Gen Electric Gas impingement starter nozzle for turbines
US2971333A (en) * 1958-05-14 1961-02-14 Gen Electric Adjustable gas impingement turbine nozzles
US3009320A (en) * 1959-06-15 1961-11-21 Gen Electric Fluid impingement starter for turbine engines
US3085396A (en) * 1959-07-03 1963-04-16 Rolls Royce Gas turbine engine with gas starter
GB1069199A (en) * 1965-02-20 1967-05-17 Bristol Siddeley Engines Ltd Improvements in means for starting gas turbine engines

Also Published As

Publication number Publication date
GB1187171A (en) 1970-04-08
FR1563248A (en) 1969-04-11
DE1626036A1 (en) 1971-03-04
US3451215A (en) 1969-06-24

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