IT8423209A1 - AIR CONTROL SYSTEM ESPECIALLY FOR GAS TURBOMOTOR - Google Patents

AIR CONTROL SYSTEM ESPECIALLY FOR GAS TURBOMOTOR

Info

Publication number
IT8423209A1
IT8423209A1 IT1984A23209A IT2320984A IT8423209A1 IT 8423209 A1 IT8423209 A1 IT 8423209A1 IT 1984A23209 A IT1984A23209 A IT 1984A23209A IT 2320984 A IT2320984 A IT 2320984A IT 8423209 A1 IT8423209 A1 IT 8423209A1
Authority
IT
Italy
Prior art keywords
turbomotor
gas
control system
air control
system especially
Prior art date
Application number
IT1984A23209A
Other languages
Italian (it)
Other versions
IT8423209A0 (en
IT1178575B (en
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8423209A0 publication Critical patent/IT8423209A0/en
Publication of IT8423209A1 publication Critical patent/IT8423209A1/en
Application granted granted Critical
Publication of IT1178575B publication Critical patent/IT1178575B/en

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT23209/84A 1983-10-31 1984-10-18 AIR CONTROL SYSTEM ESPECIALLY FOR GAS TURBO ENGINE IT1178575B (en)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
IT8423209A0 IT8423209A0 (en) 1984-10-18
IT8423209A1 true IT8423209A1 (en) 1986-04-18
IT1178575B IT1178575B (en) 1987-09-09

Family

ID=24185281

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23209/84A IT1178575B (en) 1983-10-31 1984-10-18 AIR CONTROL SYSTEM ESPECIALLY FOR GAS TURBO ENGINE

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
FR2554169A1 (en) 1985-05-03
GB2149016A (en) 1985-06-05
GB8422469D0 (en) 1984-10-10
JPS60125732A (en) 1985-07-05
DE3439108A1 (en) 1985-05-09
IT1178575B (en) 1987-09-09

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