FR1437136A - Development of gas turbine engines - Google Patents

Development of gas turbine engines

Info

Publication number
FR1437136A
FR1437136A FR20831A FR20831A FR1437136A FR 1437136 A FR1437136 A FR 1437136A FR 20831 A FR20831 A FR 20831A FR 20831 A FR20831 A FR 20831A FR 1437136 A FR1437136 A FR 1437136A
Authority
FR
France
Prior art keywords
development
gas turbine
turbine engines
engines
gas
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
FR20831A
Other languages
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines Ltd
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 Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Application granted granted Critical
Publication of FR1437136A publication Critical patent/FR1437136A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/10—Varying effective area of jet pipe or nozzle by distorting the jet pipe or nozzle

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR20831A 1964-06-15 1965-06-15 Development of gas turbine engines Expired FR1437136A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2475464A GB1106077A (en) 1964-06-15 1964-06-15 Gas turbine jet power plant

Publications (1)

Publication Number Publication Date
FR1437136A true FR1437136A (en) 1966-04-29

Family

ID=10216724

Family Applications (1)

Application Number Title Priority Date Filing Date
FR20831A Expired FR1437136A (en) 1964-06-15 1965-06-15 Development of gas turbine engines

Country Status (2)

Country Link
FR (1) FR1437136A (en)
GB (1) GB1106077A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2064433B1 (en) 2006-10-12 2013-11-20 United Technologies Corporation Gas turbine engine system and corresponding method for controlling a bypass airflow
US9010126B2 (en) * 2008-02-20 2015-04-21 United Technologies Corporation Gas turbine engine with variable area fan nozzle bladder system
US10961950B2 (en) * 2016-11-03 2021-03-30 The Boeing Company Fan nacelle trailing edge

Also Published As

Publication number Publication date
GB1106077A (en) 1968-03-13

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