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AU5010069A - Gas turbine engines - Google Patents

Gas turbine engines

Info

Publication number
AU5010069A
AU5010069A AU50100/69A AU5010069A AU5010069A AU 5010069 A AU5010069 A AU 5010069A AU 50100/69 A AU50100/69 A AU 50100/69A AU 5010069 A AU5010069 A AU 5010069A AU 5010069 A AU5010069 A AU 5010069A
Authority
AU
Australia
Prior art keywords
gas turbine
turbine engines
engines
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.)
Expired
Application number
AU50100/69A
Inventor
Clayton Berkey Donald
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
Priority to AU50100/69A priority Critical patent/AU5010069A/en
Priority to GB01822/69A priority patent/GB1211064A/en
Publication of AU5010069A publication Critical patent/AU5010069A/en
Expired 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
    • F02K3/06—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 with front fan
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
AU50100/69A 1969-02-06 1969-02-06 Gas turbine engines Expired AU5010069A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
AU50100/69A AU5010069A (en) 1969-02-06 1969-02-06 Gas turbine engines
GB01822/69A GB1211064A (en) 1969-02-06 1969-03-05 Improvements in gas turbine engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU50100/69A AU5010069A (en) 1969-02-06 1969-02-06 Gas turbine engines
GB01822/69A GB1211064A (en) 1969-02-06 1969-03-05 Improvements in gas turbine engines

Publications (1)

Publication Number Publication Date
AU5010069A true AU5010069A (en) 1972-03-02

Family

ID=25628750

Family Applications (1)

Application Number Title Priority Date Filing Date
AU50100/69A Expired AU5010069A (en) 1969-02-06 1969-02-06 Gas turbine engines

Country Status (2)

Country Link
AU (1) AU5010069A (en)
GB (1) GB1211064A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
US10724479B2 (en) 2013-03-15 2020-07-28 United Technologies Corporation Thrust efficient turbofan engine
US9624827B2 (en) 2013-03-15 2017-04-18 United Technologies Corporation Thrust efficient turbofan engine
EP3855010A1 (en) * 2013-09-30 2021-07-28 Raytheon Technologies Corporation Thrust efficient turbofan engine
GB201712993D0 (en) * 2017-08-14 2017-09-27 Rolls Royce Plc Gas turbine engine
CN108412636A (en) * 2018-03-07 2018-08-17 杨京生 Fanjet core engine for aviation power field
GB201810885D0 (en) * 2018-07-03 2018-08-15 Rolls Royce Plc High efficiency gas turbine engine

Also Published As

Publication number Publication date
GB1211064A (en) 1970-11-04

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