FR2711187B1 - Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers. - Google Patents

Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers.

Info

Publication number
FR2711187B1
FR2711187B1 FR9312291A FR9312291A FR2711187B1 FR 2711187 B1 FR2711187 B1 FR 2711187B1 FR 9312291 A FR9312291 A FR 9312291A FR 9312291 A FR9312291 A FR 9312291A FR 2711187 B1 FR2711187 B1 FR 2711187B1
Authority
FR
France
Prior art keywords
double
turbojet engine
pivoting door
thrust reversers
force recovery
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 - Fee Related
Application number
FR9312291A
Other languages
French (fr)
Other versions
FR2711187A1 (en
Inventor
Porte Alain
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.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9312291A priority Critical patent/FR2711187B1/en
Publication of FR2711187A1 publication Critical patent/FR2711187A1/en
Application granted granted Critical
Publication of FR2711187B1 publication Critical patent/FR2711187B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
FR9312291A 1993-10-15 1993-10-15 Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers. Expired - Fee Related FR2711187B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9312291A FR2711187B1 (en) 1993-10-15 1993-10-15 Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9312291A FR2711187B1 (en) 1993-10-15 1993-10-15 Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers.

Publications (2)

Publication Number Publication Date
FR2711187A1 FR2711187A1 (en) 1995-04-21
FR2711187B1 true FR2711187B1 (en) 1996-02-02

Family

ID=9451874

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9312291A Expired - Fee Related FR2711187B1 (en) 1993-10-15 1993-10-15 Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers.

Country Status (1)

Country Link
FR (1) FR2711187B1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2765917B1 (en) * 1997-07-10 1999-08-20 Hispano Suiza Sa PUSH INVERTER WITH LOCKING DISPLAY
FR2765916B1 (en) * 1997-07-10 1999-08-20 Hispano Suiza Sa PUSH INVERTER WITH IMPROVED IMPACT RESISTANCE
FR2769953B1 (en) * 1997-10-16 1999-12-10 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A SIDE RETAINING BALANCE PANEL
FR2823259B1 (en) * 2001-04-05 2003-06-27 Hispano Suiza Sa SYNCHRONIZED LOCKING SYSTEM FOR THE DOORS OF A PUSH INVERTER
US6695574B1 (en) * 2002-08-21 2004-02-24 Pratt & Whitney Canada Corp. Energy absorber and deflection device
US7146796B2 (en) * 2003-09-05 2006-12-12 The Nordam Group, Inc. Nested latch thrust reverser
US7275362B2 (en) * 2004-09-08 2007-10-02 The Boeing Company Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers
US7571527B2 (en) 2005-03-29 2009-08-11 The Boeing Company Mandrel for fabrication of a monolithic composite nacelle panel
US7690190B2 (en) 2005-05-11 2010-04-06 The Boeing Company Aircraft systems including cascade thrust reversers
US7559507B2 (en) 2005-06-27 2009-07-14 The Boeing Company Thrust reversers including locking assemblies for inhibiting deflection
US7600371B2 (en) 2005-10-18 2009-10-13 The Boeing Company Thrust reversers including support members for inhibiting deflection
US10458280B2 (en) 2013-03-13 2019-10-29 United Technologies Corporation Gas turbine engine hydraulically operated nacelle latch

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3576337A (en) * 1969-03-21 1971-04-27 Rohr Corp Locking system
US3600023A (en) * 1970-02-09 1971-08-17 Rohr Corp Locking system
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
FR2683860B1 (en) * 1991-11-14 1995-04-28 Hurel Dubois Avions SAFETY INSTALLATION FOR A PUSH-INVERTER WITH DOORS EQUIPPED WITH AN AIRCRAFT AND ASSEMBLY INCORPORATING SUCH AN INSTALLATION.

Also Published As

Publication number Publication date
FR2711187A1 (en) 1995-04-21

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Legal Events

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

Effective date: 20110630