FR1479131A - Mécanisme d'inversion de poussée - Google Patents

Mécanisme d'inversion de poussée

Info

Publication number
FR1479131A
FR1479131A FR61010A FR61010A FR1479131A FR 1479131 A FR1479131 A FR 1479131A FR 61010 A FR61010 A FR 61010A FR 61010 A FR61010 A FR 61010A FR 1479131 A FR1479131 A FR 1479131A
Authority
FR
France
Prior art keywords
reverse thrust
thrust mechanism
reverse
thrust
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
FR61010A
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.)
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 FR61010A priority Critical patent/FR1479131A/fr
Application granted granted Critical
Publication of FR1479131A publication Critical patent/FR1479131A/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • 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)
FR61010A 1966-05-10 1966-05-10 Mécanisme d'inversion de poussée Expired FR1479131A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR61010A FR1479131A (fr) 1966-05-10 1966-05-10 Mécanisme d'inversion de poussée

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR61010A FR1479131A (fr) 1966-05-10 1966-05-10 Mécanisme d'inversion de poussée

Publications (1)

Publication Number Publication Date
FR1479131A true FR1479131A (fr) 1967-04-28

Family

ID=8608288

Family Applications (1)

Application Number Title Priority Date Filing Date
FR61010A Expired FR1479131A (fr) 1966-05-10 1966-05-10 Mécanisme d'inversion de poussée

Country Status (1)

Country Link
FR (1) FR1479131A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0515263A1 (fr) * 1991-05-23 1992-11-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Inverseur de poussée pour turbosoufflante à très grand taux de dilution
FR2759418A1 (fr) * 1997-02-13 1998-08-14 Snecma Inverseur de poussee pour turbosoufflante a tres grand taux de dilution
US6145301A (en) * 1997-07-24 2000-11-14 Societe Hispano-Suiza Aerostructures Thrust reverser for fan type turbojet engines using independently actuated pivoted thrust deflectors
FR2939477A1 (fr) * 2008-12-10 2010-06-11 Aircelle Sa Nacelle de turboreacteur a section de tuyere variable

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0515263A1 (fr) * 1991-05-23 1992-11-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Inverseur de poussée pour turbosoufflante à très grand taux de dilution
FR2676780A1 (fr) * 1991-05-23 1992-11-27 Snecma Inverseur de poussee pour turbosoufflante a tres grand taux dilution.
US5255510A (en) * 1991-05-23 1993-10-26 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Thrust reverser for a high-bypass ratio turbofan engine
FR2759418A1 (fr) * 1997-02-13 1998-08-14 Snecma Inverseur de poussee pour turbosoufflante a tres grand taux de dilution
EP0859142A1 (fr) * 1997-02-13 1998-08-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Inverseur de poussée pour turbosoufflante à trés grand taux de dilution
US6050522A (en) * 1997-02-13 2000-04-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Thrust reverser for a high bypass turbofan engine
US6145301A (en) * 1997-07-24 2000-11-14 Societe Hispano-Suiza Aerostructures Thrust reverser for fan type turbojet engines using independently actuated pivoted thrust deflectors
FR2939477A1 (fr) * 2008-12-10 2010-06-11 Aircelle Sa Nacelle de turboreacteur a section de tuyere variable
WO2010066957A1 (fr) * 2008-12-10 2010-06-17 Aircelle Nacelle de turboreacteur a section de tuyere variable

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