FR2962978B1 - TURBOREACTOR NACELLE - Google Patents

TURBOREACTOR NACELLE

Info

Publication number
FR2962978B1
FR2962978B1 FR1056006A FR1056006A FR2962978B1 FR 2962978 B1 FR2962978 B1 FR 2962978B1 FR 1056006 A FR1056006 A FR 1056006A FR 1056006 A FR1056006 A FR 1056006A FR 2962978 B1 FR2962978 B1 FR 2962978B1
Authority
FR
France
Prior art keywords
turboreactor
nacelle
turboreactor nacelle
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.)
Active
Application number
FR1056006A
Other languages
French (fr)
Other versions
FR2962978A1 (en
Inventor
Philippe Minot
Stephane Bensilum
Herve Hurlin
Olivier Kerbler
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
Safran Nacelles SAS
Original Assignee
Aircelle SA
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 Aircelle SA, SNECMA SAS filed Critical Aircelle SA
Priority to FR1056006A priority Critical patent/FR2962978B1/en
Priority to PCT/FR2011/051649 priority patent/WO2012010774A2/en
Publication of FR2962978A1 publication Critical patent/FR2962978A1/en
Application granted granted Critical
Publication of FR2962978B1 publication Critical patent/FR2962978B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • F02K1/70Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/76Control or regulation of thrust reversers
    • F02K1/763Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/34Arrangement of components translated
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/40Movement of components
    • F05D2250/41Movement of components with one degree of freedom
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
FR1056006A 2010-07-22 2010-07-22 TURBOREACTOR NACELLE Active FR2962978B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1056006A FR2962978B1 (en) 2010-07-22 2010-07-22 TURBOREACTOR NACELLE
PCT/FR2011/051649 WO2012010774A2 (en) 2010-07-22 2011-07-12 Turbojet engine nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1056006A FR2962978B1 (en) 2010-07-22 2010-07-22 TURBOREACTOR NACELLE

Publications (2)

Publication Number Publication Date
FR2962978A1 FR2962978A1 (en) 2012-01-27
FR2962978B1 true FR2962978B1 (en) 2012-08-03

Family

ID=43706336

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1056006A Active FR2962978B1 (en) 2010-07-22 2010-07-22 TURBOREACTOR NACELLE

Country Status (2)

Country Link
FR (1) FR2962978B1 (en)
WO (1) WO2012010774A2 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2999240B1 (en) * 2012-12-11 2015-01-02 Aircelle Sa SYNCHRONIZATION SYSTEM FOR PUSH REVERSING DEVICE
FR3002785B1 (en) * 2013-03-01 2015-03-27 Aircelle Sa TRANSLATANT AND FIXED GRIDS WITH A T / R O-DUCT.
FR3007800B1 (en) * 2013-07-01 2017-10-20 Aircelle Sa THRUST INVERTER OF A TURBOJET NACELLE COMPRISING PARTIALLY INTEGRATED GRIDS IN HOODS
FR3019229B1 (en) * 2014-03-31 2016-05-06 Aircelle Sa THRUST INVERTER OF A TURBOJET NACELLE COMPRISING MOBILE HOOD CONTROL JIGS AND A VARIABLE SECONDARY TUBE
US10309343B2 (en) * 2014-11-06 2019-06-04 Rohr, Inc. Split sleeve hidden door thrust reverser
US10605197B2 (en) * 2014-12-02 2020-03-31 United Technologies Corporation Gas turbine engine and thrust reverser assembly therefore
US10208708B2 (en) * 2015-01-29 2019-02-19 Rohr, Inc. Translating cascade hidden blocker door thrust reverser
US10428764B2 (en) * 2016-02-10 2019-10-01 Rohr, Inc. Deflection limiter for a cascade assembly of a thrust reverser

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182724B (en) * 1985-10-08 1988-12-07 Rolls Royce Gas turbine engine thrust reverser
FR2622929A1 (en) * 1987-11-05 1989-05-12 Hispano Suiza Sa DRIVE INVERTER OF GRID TURBOREACTOR, WITH VARIABLE EJECTION SECTION
FR2786532B1 (en) * 1998-11-26 2001-09-07 Snecma OVERHEAD GRID TURBOREACTOR DRIVE INVERTER
GB2347126B (en) * 1999-02-23 2003-02-12 Rolls Royce Plc Thrust reverser
FR2922058B1 (en) * 2007-10-04 2009-12-04 Aircelle Sa TELESCOPIC LINEAR ACTUATOR FOR MOVING A FIRST AND A SECOND ELEMENTS RELATIVELY TO A FIXED ELEMENT

Also Published As

Publication number Publication date
FR2962978A1 (en) 2012-01-27
WO2012010774A3 (en) 2012-06-07
WO2012010774A2 (en) 2012-01-26

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Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

Owner name: AIRCELLE, FR

Effective date: 20170719

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20180125

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

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PLFP Fee payment

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