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FR1139775A - Tuyère de décharge pour un jet propulseur - Google Patents

Tuyère de décharge pour un jet propulseur

Info

Publication number
FR1139775A
FR1139775A FR1139775DA FR1139775A FR 1139775 A FR1139775 A FR 1139775A FR 1139775D A FR1139775D A FR 1139775DA FR 1139775 A FR1139775 A FR 1139775A
Authority
FR
France
Prior art keywords
discharge nozzle
propellant jet
propellant
jet
nozzle
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
English (en)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1139775A publication Critical patent/FR1139775A/fr
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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • 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
    • F02K1/15—Control or regulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
FR1139775D 1954-11-26 1955-11-25 Tuyère de décharge pour un jet propulseur Expired FR1139775A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2900789X 1954-11-26

Publications (1)

Publication Number Publication Date
FR1139775A true FR1139775A (fr) 1957-07-04

Family

ID=10917440

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1139775D Expired FR1139775A (fr) 1954-11-26 1955-11-25 Tuyère de décharge pour un jet propulseur

Country Status (2)

Country Link
US (1) US2900789A (fr)
FR (1) FR1139775A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1061569B (de) * 1957-11-14 1959-07-16 Bmw Triebwerkbau Ges M B H Konvergent-divergente Verstellschubduese fuer Strahltriebwerke

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3109284A (en) * 1956-06-14 1963-11-05 Power Jets Res & Dev Ltd Discharge nozzles for propulsive jets
US3003311A (en) * 1957-07-17 1961-10-10 Havilland Engine Co Ltd Adjustable propulsion nozzles
US3032977A (en) * 1958-06-05 1962-05-08 Gen Electric Correlated bypass inlet and outlet control for a supersonic reaction powerplant
US2984068A (en) * 1958-06-30 1961-05-16 Orenda Engines Ltd Propulsive nozzle system for reaction propulsion units
US3103102A (en) * 1958-07-18 1963-09-10 Bristol Siddeley Engines Ltd Propulsion power plants for aircraft
US3115748A (en) * 1960-05-06 1963-12-31 Rolls Royce Gas turbine engine
GB953803A (en) * 1960-10-21 1964-04-02 Bristol Siddeley Engines Ltd Improvements in or relating to jet propulsion engines
US3316716A (en) * 1964-07-01 1967-05-02 William J D Escher Composite powerplant and shroud therefor
FR2618488B1 (fr) * 1987-07-20 1989-12-15 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
JP3710099B2 (ja) * 1995-03-31 2005-10-26 株式会社アイ・エイチ・アイ・エアロスペース ジェッタベータ
US5706650A (en) * 1995-08-09 1998-01-13 United Technologies Corporation Vectoring nozzle using injected high pressure air
US6347510B1 (en) * 1998-12-18 2002-02-19 United Technologies Corporation Axi-nozzle ejector seal
US20140165575A1 (en) * 2012-12-13 2014-06-19 United Technologies Corporation Nozzle section for a gas turbine engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675670A (en) * 1954-04-20 Pulse jet engine havingf variable
US2671620A (en) * 1948-06-14 1954-03-09 Rolls Royce Control means for aircraft and aircraft power plant installations
US2697907A (en) * 1948-11-12 1954-12-28 Gen Motors Corp Multiplate variable area jet nozzle
FR998358A (fr) * 1949-10-31 1952-01-17 Cem Comp Electro Mec Tuyères d'éjection pour turbo-réacteurs
US2625008A (en) * 1951-02-28 1953-01-13 Curtiss Wright Corp Variable flow nozzle
US2770944A (en) * 1952-04-26 1956-11-20 United Aircraft Corp Variable area reaction nozzle movable from convergent to convergent-di-vergent form
US2858668A (en) * 1952-09-27 1958-11-04 Curtiss Wright Corp Control for variable area convergentdivergent exhaust nozzle
BE525114A (fr) * 1952-12-16
US2726509A (en) * 1953-04-02 1955-12-13 William B Gist Adjusting system for variable area nozzle
GB782494A (en) * 1954-03-26 1957-09-11 Rolls Royce Improvements in or relating to jet propulsion nozzle arrangements

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1061569B (de) * 1957-11-14 1959-07-16 Bmw Triebwerkbau Ges M B H Konvergent-divergente Verstellschubduese fuer Strahltriebwerke

Also Published As

Publication number Publication date
US2900789A (en) 1959-08-25

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