GB8422469D0 - Air control system - Google Patents

Air control system

Info

Publication number
GB8422469D0
GB8422469D0 GB848422469A GB8422469A GB8422469D0 GB 8422469 D0 GB8422469 D0 GB 8422469D0 GB 848422469 A GB848422469 A GB 848422469A GB 8422469 A GB8422469 A GB 8422469A GB 8422469 D0 GB8422469 D0 GB 8422469D0
Authority
GB
United Kingdom
Prior art keywords
control system
air control
air
control
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.)
Withdrawn
Application number
GB848422469A
Other versions
GB2149016A (en
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 GB8422469D0 publication Critical patent/GB8422469D0/en
Publication of GB2149016A publication Critical patent/GB2149016A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
GB08422469A 1983-10-31 1984-09-05 Air control system Withdrawn GB2149016A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US54759283A 1983-10-31 1983-10-31

Publications (2)

Publication Number Publication Date
GB8422469D0 true GB8422469D0 (en) 1984-10-10
GB2149016A GB2149016A (en) 1985-06-05

Family

ID=24185281

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08422469A Withdrawn GB2149016A (en) 1983-10-31 1984-09-05 Air control system

Country Status (5)

Country Link
JP (1) JPS60125732A (en)
DE (1) DE3439108A1 (en)
FR (1) FR2554169A1 (en)
GB (1) GB2149016A (en)
IT (1) IT1178575B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2192229B (en) * 1986-07-04 1990-05-02 Rolls Royce Plc A compressor and air bleed system
CA2013933A1 (en) * 1989-06-05 1990-12-05 General Electric Company Gas turbine powerplant
DE102012003902A1 (en) * 2011-12-14 2013-06-20 Istvan Bolgar Inlet for gas turbine, has inlet wall, bypass-channel formed at inner side of inlet wall, and bypass flow-stator arranged at end of bypass-channel, where inner side of bypass-channel is limited by bypass-channel wall that has drain holes

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB609322A (en) * 1945-11-07 1948-09-29 Power Jets Res & Dev Ltd Improvements relating to axial-flow compressors and like machines, and blading thereof
US2999631A (en) * 1958-09-05 1961-09-12 Gen Electric Dual airfoil
GB1291943A (en) * 1970-02-11 1972-10-04 Secr Defence Improvements in or relating to ducted fans
DE2149619A1 (en) * 1971-10-05 1973-04-19 Motoren Turbinen Union TURBINE JET FOR VERTICAL OR SHORT-STARTING OR LANDING AIRPLANES
US3777489A (en) * 1972-06-01 1973-12-11 Gen Electric Combustor casing and concentric air bleed structure
US4791783A (en) * 1981-11-27 1988-12-20 General Electric Company Convertible aircraft engine

Also Published As

Publication number Publication date
IT8423209A0 (en) 1984-10-18
GB2149016A (en) 1985-06-05
FR2554169A1 (en) 1985-05-03
IT8423209A1 (en) 1986-04-18
IT1178575B (en) 1987-09-09
JPS60125732A (en) 1985-07-05
DE3439108A1 (en) 1985-05-09

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)