JPS5331011A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
JPS5331011A
JPS5331011A JP9149077A JP9149077A JPS5331011A JP S5331011 A JPS5331011 A JP S5331011A JP 9149077 A JP9149077 A JP 9149077A JP 9149077 A JP9149077 A JP 9149077A JP S5331011 A JPS5331011 A JP S5331011A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
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
JP9149077A
Other languages
Japanese (ja)
Inventor
Pooru Adamuson Aasaa
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 JPS5331011A publication Critical patent/JPS5331011A/en
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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
JP9149077A 1976-08-02 1977-08-01 Gas turbine engine Pending JPS5331011A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US71042376A 1976-08-02 1976-08-02

Publications (1)

Publication Number Publication Date
JPS5331011A true JPS5331011A (en) 1978-03-23

Family

ID=24853961

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9149077A Pending JPS5331011A (en) 1976-08-02 1977-08-01 Gas turbine engine

Country Status (3)

Country Link
JP (1) JPS5331011A (en)
DE (1) DE2733986A1 (en)
FR (1) FR2360758A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4969325A (en) * 1989-01-03 1990-11-13 General Electric Company Turbofan engine having a counterrotating partially geared fan drive turbine
US9885291B2 (en) 2012-08-09 2018-02-06 Snecma Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan
US9879561B2 (en) 2012-08-09 2018-01-30 Snecma Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan
FR2994452B1 (en) 2012-08-09 2016-12-23 Snecma TURBOMACHINE COMPRISING A PLURALITY OF FIXED RADIAL BLADES MOUNTED BEFORE THE BLOWER
EP3853466A1 (en) 2018-09-21 2021-07-28 Safran Aircraft Engines Turbo-reactor comprising a power supply device
FR3086342B1 (en) * 2018-09-21 2020-12-11 Safran Aircraft Engines REDUCER TURBOREACTOR
FR3086348B1 (en) 2018-09-21 2020-12-04 Safran Aircraft Engines REDUCER TURBOREACTOR

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1055328A (en) * 1964-07-20 1967-01-18 Rolls Royce Gas turbine engine

Also Published As

Publication number Publication date
DE2733986A1 (en) 1978-02-09
FR2360758A1 (en) 1978-03-03

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