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FR2915527B1 - REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER - Google Patents

REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER

Info

Publication number
FR2915527B1
FR2915527B1 FR0703123A FR0703123A FR2915527B1 FR 2915527 B1 FR2915527 B1 FR 2915527B1 FR 0703123 A FR0703123 A FR 0703123A FR 0703123 A FR0703123 A FR 0703123A FR 2915527 B1 FR2915527 B1 FR 2915527B1
Authority
FR
France
Prior art keywords
rear caster
caster structure
push inverter
reactor engine
reactor
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
FR0703123A
Other languages
French (fr)
Other versions
FR2915527A1 (en
Inventor
Guy Vauchel
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 Nacelles SAS
Original Assignee
Aircelle SA
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 filed Critical Aircelle SA
Priority to FR0703123A priority Critical patent/FR2915527B1/en
Priority to PCT/FR2008/000266 priority patent/WO2008132297A2/en
Priority to EP08775611A priority patent/EP2139770A2/en
Publication of FR2915527A1 publication Critical patent/FR2915527A1/en
Application granted granted Critical
Publication of FR2915527B1 publication Critical patent/FR2915527B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings or cowlings
    • B64D29/08Inspection panels for power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
    • F02K1/64Reversing fan flow
    • F02K1/70Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • 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
    • F05D2230/00Manufacture
    • F05D2230/80Repairing, retrofitting or upgrading methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR0703123A 2007-04-30 2007-04-30 REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER Expired - Fee Related FR2915527B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR0703123A FR2915527B1 (en) 2007-04-30 2007-04-30 REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER
PCT/FR2008/000266 WO2008132297A2 (en) 2007-04-30 2008-02-29 Rear nacelle structure for a jet engine, such as a thrust reverser
EP08775611A EP2139770A2 (en) 2007-04-30 2008-02-29 Rear nacelle structure for a jet engine, such as a thrust reverser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0703123A FR2915527B1 (en) 2007-04-30 2007-04-30 REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER

Publications (2)

Publication Number Publication Date
FR2915527A1 FR2915527A1 (en) 2008-10-31
FR2915527B1 true FR2915527B1 (en) 2009-06-12

Family

ID=38800740

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0703123A Expired - Fee Related FR2915527B1 (en) 2007-04-30 2007-04-30 REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER

Country Status (3)

Country Link
EP (1) EP2139770A2 (en)
FR (1) FR2915527B1 (en)
WO (1) WO2008132297A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2967398B1 (en) 2010-11-16 2012-11-02 Aircelle Sa STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY
FR3033545B1 (en) 2015-03-12 2018-08-10 Airbus Operations NACELLE FOR AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST ONE ARTICULATED NACELLE COVER AT ITS FRONT END
DE102015206093A1 (en) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of an aircraft gas turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2661213B1 (en) * 1990-04-19 1992-07-03 Snecma AVIATION ENGINE WITH VERY HIGH DILUTION RATES AND OF THE SAID TYPE FRONT CONTRAFAN.
GB9120658D0 (en) * 1991-09-27 1991-11-06 Short Brothers Plc Ducted fan turbine engine
US5350136A (en) * 1993-05-14 1994-09-27 United Technologies Corporation Nacelle arrangement
FR2757823B1 (en) * 1996-12-26 1999-03-12 Aerospatiale LAMINARY FLOW TURBOREACTOR BASKET
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
FR2897339B1 (en) * 2006-02-16 2008-04-11 Aircelle Sa NACELLE DE TURBOREACTEUR WITH LATERAL OPENING OF HOODS

Also Published As

Publication number Publication date
EP2139770A2 (en) 2010-01-06
WO2008132297A2 (en) 2008-11-06
WO2008132297A3 (en) 2008-12-31
FR2915527A1 (en) 2008-10-31

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20101230