FR2323883A1 - Manchon d'ejection pour turboreacteur d'aeronef - Google Patents

Manchon d'ejection pour turboreacteur d'aeronef

Info

Publication number
FR2323883A1
FR2323883A1 FR7627343A FR7627343A FR2323883A1 FR 2323883 A1 FR2323883 A1 FR 2323883A1 FR 7627343 A FR7627343 A FR 7627343A FR 7627343 A FR7627343 A FR 7627343A FR 2323883 A1 FR2323883 A1 FR 2323883A1
Authority
FR
France
Prior art keywords
ejection sleeve
turboreactor
aircraft
aircraft turboreactor
ejection
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.)
Granted
Application number
FR7627343A
Other languages
English (en)
Other versions
FR2323883B1 (fr
Inventor
Leonard John Rodgers
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
Publication of FR2323883A1 publication Critical patent/FR2323883A1/fr
Application granted granted Critical
Publication of FR2323883B1 publication Critical patent/FR2323883B1/fr
Granted 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
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
FR7627343A 1975-09-12 1976-09-10 Manchon d'ejection pour turboreacteur d'aeronef Granted FR2323883A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB37534/75A GB1514305A (en) 1975-09-12 1975-09-12 Ejector sleeves for aircraft mounted gas turbine engines

Publications (2)

Publication Number Publication Date
FR2323883A1 true FR2323883A1 (fr) 1977-04-08
FR2323883B1 FR2323883B1 (fr) 1982-09-17

Family

ID=10397205

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7627343A Granted FR2323883A1 (fr) 1975-09-12 1976-09-10 Manchon d'ejection pour turboreacteur d'aeronef

Country Status (5)

Country Link
US (1) US4049220A (fr)
JP (1) JPS5252016A (fr)
DE (1) DE2640648C2 (fr)
FR (1) FR2323883A1 (fr)
GB (1) GB1514305A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2936492A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Nacelle pour turboreacteur.
FR3015434A1 (fr) * 2013-12-23 2015-06-26 Snecma Suspension de turbomachine

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4369937A (en) * 1981-05-18 1983-01-25 The United States Of America As Represented By The Secretary Of The Army Hinging and latching apparatus
US4466587A (en) * 1981-12-21 1984-08-21 General Electric Company Nacelle installation
US5727755A (en) * 1994-01-21 1998-03-17 Craig; Alfred C. Aircraft engines with a controllable outer casing
US5730392A (en) * 1995-09-22 1998-03-24 Aeronautical Concept Of Exhaust, Ltd. Adjustable fairing for thrust reversers
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
ES2316257B1 (es) * 2006-10-31 2010-01-12 Airbus España, S.L. Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos.

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067968A (en) * 1958-12-29 1962-12-11 Heppenstall Charles William Retractable jet engine noise suppressor
US3516511A (en) * 1969-05-22 1970-06-23 Rohr Corp Method and apparatus for augmenting the thrust and suppressing the noise of an aircraft jet engine
US3581841A (en) * 1970-07-27 1971-06-01 Rohr Corp Thrust reversing and noise suppressing apparatus for a jet engine
US3583640A (en) * 1969-11-03 1971-06-08 Rohr Corp Jet propulsion apparatus and method of operating the same
US3637042A (en) * 1970-07-27 1972-01-25 Rohr Corp Method and apparatus for suppressing the noise of jet-propelled aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US560141A (en) * 1896-05-12 Bicycle-supporting apparatus
US1703496A (en) * 1927-06-01 1929-02-26 Naud Jack Dog race track
US2972860A (en) * 1958-01-30 1961-02-28 Westinghouse Electric Corp Combined variable ejector and thrust reverser
US3084507A (en) * 1958-06-17 1963-04-09 Douglas Aircraft Co Inc Jet engine sound suppressor and reverser
US3591087A (en) * 1969-05-08 1971-07-06 Rohr Corp Apparatus for augmenting the thrust of an aircraft jet engine
DE2031170A1 (de) * 1970-06-24 1971-12-30 Bosch Gmbh Robert Transporteinrichtung für Lasten

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067968A (en) * 1958-12-29 1962-12-11 Heppenstall Charles William Retractable jet engine noise suppressor
US3516511A (en) * 1969-05-22 1970-06-23 Rohr Corp Method and apparatus for augmenting the thrust and suppressing the noise of an aircraft jet engine
US3583640A (en) * 1969-11-03 1971-06-08 Rohr Corp Jet propulsion apparatus and method of operating the same
US3581841A (en) * 1970-07-27 1971-06-01 Rohr Corp Thrust reversing and noise suppressing apparatus for a jet engine
US3637042A (en) * 1970-07-27 1972-01-25 Rohr Corp Method and apparatus for suppressing the noise of jet-propelled aircraft

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2936492A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Nacelle pour turboreacteur.
WO2010037923A1 (fr) * 2008-10-01 2010-04-08 Aircelle Nacelle pour turboreacteur
RU2509688C2 (ru) * 2008-10-01 2014-03-20 Эрсель Гондола турбореактивного двигателя
US8753072B2 (en) 2008-10-01 2014-06-17 Aircelle Turbojet engine nacelle
FR3015434A1 (fr) * 2013-12-23 2015-06-26 Snecma Suspension de turbomachine
US9394057B2 (en) 2013-12-23 2016-07-19 Snecma Suspension for a turbine engine

Also Published As

Publication number Publication date
FR2323883B1 (fr) 1982-09-17
JPS5252016A (en) 1977-04-26
US4049220A (en) 1977-09-20
DE2640648C2 (de) 1982-04-22
GB1514305A (en) 1978-06-14
DE2640648A1 (de) 1977-04-07

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse