FR2650861B1 - - Google Patents

Info

Publication number
FR2650861B1
FR2650861B1 FR8910640A FR8910640A FR2650861B1 FR 2650861 B1 FR2650861 B1 FR 2650861B1 FR 8910640 A FR8910640 A FR 8910640A FR 8910640 A FR8910640 A FR 8910640A FR 2650861 B1 FR2650861 B1 FR 2650861B1
Authority
FR
France
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 - Fee Related
Application number
FR8910640A
Other languages
French (fr)
Other versions
FR2650861A1 (en
Inventor
Jean Marey Daniel
Nicolas Szybiak Guy
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR8910640A priority Critical patent/FR2650861A1/en
Publication of FR2650861A1 publication Critical patent/FR2650861A1/en
Application granted granted Critical
Publication of FR2650861B1 publication Critical patent/FR2650861B1/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
    • 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
FR8910640A 1989-08-08 1989-08-08 Bypass turbo jet thrust reverser with obstacles connected to the primary cowling Granted FR2650861A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8910640A FR2650861A1 (en) 1989-08-08 1989-08-08 Bypass turbo jet thrust reverser with obstacles connected to the primary cowling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8910640A FR2650861A1 (en) 1989-08-08 1989-08-08 Bypass turbo jet thrust reverser with obstacles connected to the primary cowling

Publications (2)

Publication Number Publication Date
FR2650861A1 FR2650861A1 (en) 1991-02-15
FR2650861B1 true FR2650861B1 (en) 1994-04-22

Family

ID=9384556

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8910640A Granted FR2650861A1 (en) 1989-08-08 1989-08-08 Bypass turbo jet thrust reverser with obstacles connected to the primary cowling

Country Status (1)

Country Link
FR (1) FR2650861A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2676780B1 (en) * 1991-05-23 1993-08-13 Snecma PUSH INVERTER FOR VERY HIGH DILUTION TURBOSOUFFLANTE.
FR2721977B1 (en) * 1994-06-30 1996-08-02 Hispano Suiza Sa DOUBLE-FLOW TURBOREACTOR DRIVE INVERTER WITH PRIMARY HOOD-RELATED OBSTACLES
FR2738597B1 (en) * 1995-09-13 1997-10-03 Hispano Suiza Sa TURBOJET DRIVE INVERTER WITH DOORS ASSOCIATED WITH A PRIMARY PANEL
FR2749041B1 (en) * 1996-05-23 1998-06-26 Hispano Suiza Sa DOUBLE FLOW TURBOREACTOR DRIVE INVERTER WITH PRIMARY HOOD OBSTACLES
FR2757901B1 (en) * 1996-12-26 1999-01-29 Hispano Suiza Sa DOWNSTREAM DOUBLE FLOW TURBOREACTOR DRIVE INVERTER
FR2759418B1 (en) * 1997-02-13 1999-03-19 Snecma PUSH INVERTER FOR VERY HIGH DILUTION TURBOSOFFICE
FR2766522B1 (en) * 1997-07-24 1999-09-03 Hispano Suiza Sa TURBO BLOWER THRUST INVERTER WITH OBSTACLE WITH AXIAL GUIDANCE LINKED TO THE PRIMARY COVER
WO2008045089A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Core cowl airfoil for a gas turbine engine
EP3702603B1 (en) 2019-02-28 2023-12-13 Airbus Operations GmbH Thrust reverser assembly for an engine nacelle of an aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2839891A (en) * 1953-11-27 1958-06-24 Boeing Co Thrust reversers for jet engines
US3280561A (en) * 1965-06-07 1966-10-25 Gen Electric Thrust reverser mechanism
US3917198A (en) * 1974-06-21 1975-11-04 Rohr Industries Inc Overwing post exit blocker/deflector door thrust reverser

Also Published As

Publication number Publication date
FR2650861A1 (en) 1991-02-15

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Legal Events

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

Effective date: 20090430