ATE496827T1 - Heckteil einer flugzeuggondel und mit einem solchen heckteil ausgestattete flugzeuggondel - Google Patents

Heckteil einer flugzeuggondel und mit einem solchen heckteil ausgestattete flugzeuggondel

Info

Publication number
ATE496827T1
ATE496827T1 AT08828037T AT08828037T ATE496827T1 AT E496827 T1 ATE496827 T1 AT E496827T1 AT 08828037 T AT08828037 T AT 08828037T AT 08828037 T AT08828037 T AT 08828037T AT E496827 T1 ATE496827 T1 AT E496827T1
Authority
AT
Austria
Prior art keywords
tail part
aircraft gondola
central portion
aircraft
gondola
Prior art date
Application number
AT08828037T
Other languages
English (en)
Inventor
Eric Lecossais
Thierry Ledocte
Pascal Rouyer
Felix Carimali
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
Application granted granted Critical
Publication of ATE496827T1 publication Critical patent/ATE496827T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
AT08828037T 2007-08-20 2008-06-16 Heckteil einer flugzeuggondel und mit einem solchen heckteil ausgestattete flugzeuggondel ATE496827T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705896A FR2920132B1 (fr) 2007-08-20 2007-08-20 Troncon arriere de nacelle d'aeronef et nacelle equipee d'un tel troncon arriere
PCT/FR2008/000835 WO2009024657A1 (fr) 2007-08-20 2008-06-16 Tronçon arriere de nacelle d'aeronef, et nacelle equipee d'un tel tronçon arriere

Publications (1)

Publication Number Publication Date
ATE496827T1 true ATE496827T1 (de) 2011-02-15

Family

ID=39227081

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08828037T ATE496827T1 (de) 2007-08-20 2008-06-16 Heckteil einer flugzeuggondel und mit einem solchen heckteil ausgestattete flugzeuggondel

Country Status (11)

Country Link
US (1) US8943793B2 (de)
EP (1) EP2178752B1 (de)
CN (1) CN101784443B (de)
AT (1) ATE496827T1 (de)
BR (1) BRPI0813035A2 (de)
CA (1) CA2696358C (de)
DE (1) DE602008004781D1 (de)
ES (1) ES2357874T3 (de)
FR (1) FR2920132B1 (de)
RU (1) RU2456213C2 (de)
WO (1) WO2009024657A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3081799B1 (de) * 2015-04-14 2019-08-07 Rolls-Royce Deutschland Ltd & Co KG Turbomaschine mit einem fluidleitungssystem

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
US4926633A (en) * 1989-06-27 1990-05-22 The United States Of America As Represented By The Secretary Of The Air Force Coolant pressure regulating apparatus
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
US6584763B2 (en) * 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
FR2830051B1 (fr) * 2001-09-27 2003-11-07 Hurel Hispano Le Havre Systeme de verrouillage sur un inverseur de poussee a grilles
US6848651B2 (en) * 2002-10-07 2005-02-01 Honeywell International Inc. Electro-hydraulic thrust reverser lock actuation system and method
US7216475B2 (en) * 2003-11-21 2007-05-15 General Electric Company Aft FLADE engine
US7762057B2 (en) * 2007-06-05 2010-07-27 The Boeing Company Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines

Also Published As

Publication number Publication date
CN101784443A (zh) 2010-07-21
EP2178752B1 (de) 2011-01-26
CA2696358A1 (fr) 2009-02-26
DE602008004781D1 (de) 2011-03-10
WO2009024657A1 (fr) 2009-02-26
US8943793B2 (en) 2015-02-03
BRPI0813035A2 (pt) 2014-12-23
ES2357874T3 (es) 2011-05-03
RU2456213C2 (ru) 2012-07-20
FR2920132B1 (fr) 2009-09-18
US20120000179A1 (en) 2012-01-05
EP2178752A1 (de) 2010-04-28
CA2696358C (fr) 2015-02-24
RU2010109813A (ru) 2011-09-27
CN101784443B (zh) 2013-04-24
FR2920132A1 (fr) 2009-02-27

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Legal Events

Date Code Title Description
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