FR1124348A - Gas turbine engine improvements - Google Patents

Gas turbine engine improvements

Info

Publication number
FR1124348A
FR1124348A FR1124348DA FR1124348A FR 1124348 A FR1124348 A FR 1124348A FR 1124348D A FR1124348D A FR 1124348DA FR 1124348 A FR1124348 A FR 1124348A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
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
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1124348A publication Critical patent/FR1124348A/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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
FR1124348D 1954-06-10 1955-05-16 Gas turbine engine improvements Expired FR1124348A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1715254A GB795652A (en) 1954-06-10 1954-06-10 Improvements in or relating to gas-turbine jet propulsion engines

Publications (1)

Publication Number Publication Date
FR1124348A true FR1124348A (en) 1956-10-09

Family

ID=10090200

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1124348D Expired FR1124348A (en) 1954-06-10 1955-05-16 Gas turbine engine improvements

Country Status (2)

Country Link
FR (1) FR1124348A (en)
GB (1) GB795652A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2971327A (en) * 1957-11-26 1961-02-14 Westinghouse Electric Corp Discharge control of an overexpanding propulsion nozzle
US3010280A (en) * 1958-03-25 1961-11-28 United Aircraft Corp Variable-expansion nozzle
US3066485A (en) * 1957-12-11 1962-12-04 Bertin & Cie Steering device for rocket-propelled vehicles

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049875A (en) * 1952-08-15 1962-08-21 United Aircraft Corp Variable flap plug type nozzle
FR1211773A (en) * 1958-10-08 1960-03-18 Snecma Device for adapting a convergent-divergent nozzle to variable speeds
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
US3463404A (en) * 1966-12-21 1969-08-26 United Aircraft Corp Gas boundary layer variable area orifice
US4007586A (en) * 1975-11-10 1977-02-15 The United States Of America As Represented By The Secretary Of The Army Spin nozzle and thrust augmentor mechanism
EP2074323B1 (en) 2006-10-12 2012-11-21 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation
DE102014208883A1 (en) * 2014-05-12 2015-12-03 MTU Aero Engines AG Method for designing a turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2971327A (en) * 1957-11-26 1961-02-14 Westinghouse Electric Corp Discharge control of an overexpanding propulsion nozzle
US3066485A (en) * 1957-12-11 1962-12-04 Bertin & Cie Steering device for rocket-propelled vehicles
US3010280A (en) * 1958-03-25 1961-11-28 United Aircraft Corp Variable-expansion nozzle

Also Published As

Publication number Publication date
GB795652A (en) 1958-05-28

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