ATE535443T1 - Triebwerksgondel zum einbau in ein flugzeug - Google Patents

Triebwerksgondel zum einbau in ein flugzeug

Info

Publication number
ATE535443T1
ATE535443T1 AT08828514T AT08828514T ATE535443T1 AT E535443 T1 ATE535443 T1 AT E535443T1 AT 08828514 T AT08828514 T AT 08828514T AT 08828514 T AT08828514 T AT 08828514T AT E535443 T1 ATE535443 T1 AT E535443T1
Authority
AT
Austria
Prior art keywords
shells
jet engine
aircraft
mid
shell
Prior art date
Application number
AT08828514T
Other languages
English (en)
Inventor
Gilles Bourdon
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 ATE535443T1 publication Critical patent/ATE535443T1/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
    • B64D29/08—Inspection panels for power plants
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Harvester Elements (AREA)
  • Breeding Of Plants And Reproduction By Means Of Culturing (AREA)
  • Transplanting Machines (AREA)
AT08828514T 2007-08-20 2008-06-12 Triebwerksgondel zum einbau in ein flugzeug ATE535443T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705922A FR2920141B1 (fr) 2007-08-20 2007-08-20 Nacelle de turboreacteur, destinee a equiper un aeronef
PCT/FR2008/000812 WO2009027590A1 (fr) 2007-08-20 2008-06-12 Nacelle de turboréacteur, destinée à équiper un aéronef

Publications (1)

Publication Number Publication Date
ATE535443T1 true ATE535443T1 (de) 2011-12-15

Family

ID=39247317

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08828514T ATE535443T1 (de) 2007-08-20 2008-06-12 Triebwerksgondel zum einbau in ein flugzeug

Country Status (10)

Country Link
US (1) US8333343B2 (de)
EP (1) EP2178760B1 (de)
CN (1) CN101778769B (de)
AT (1) ATE535443T1 (de)
BR (1) BRPI0813609A2 (de)
CA (1) CA2696765C (de)
ES (1) ES2377170T3 (de)
FR (1) FR2920141B1 (de)
RU (1) RU2480383C2 (de)
WO (1) WO2009027590A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2953492B1 (fr) * 2009-12-09 2012-04-06 Airbus Operations Sas Nacelle d'aeronef incorporant un dispositif de rapprochement de capots independant du mecanisme de verrouillage
FR2999239B1 (fr) * 2012-12-12 2015-02-20 Aircelle Sa Inverseur de poussee de nacelle et nacelle equipee d'au moins un inverseur
CN105508053A (zh) * 2015-12-29 2016-04-20 中国航空工业集团公司沈阳发动机设计研究所 一种内安装边结构的燃汽轮机进气内流道结构
CN106510040A (zh) * 2016-11-25 2017-03-22 深圳沃海森科技有限公司 通过内部风涌系统可进行滑翔的空调服
US10697396B2 (en) * 2017-10-17 2020-06-30 Rohr, Inc. Fan cowl mounted to thrust reverser
FR3081443B1 (fr) 2018-05-22 2020-12-18 Airbus Operations Sas Aeronef comprenant au moins un capot equipe d’un systeme d’articulation ameliore
US10906661B2 (en) * 2018-11-05 2021-02-02 Rohr, Inc. Nacelle cowl hinge
US11414200B2 (en) * 2019-04-29 2022-08-16 Rohr, Inc. Fan cowl securement retainers
FR3152795B1 (fr) 2023-09-07 2025-09-12 Safran Nacelles Ensemble propulsif avec blocage longitudinal d‘au moins un capot de nacelle

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4644806A (en) * 1985-04-22 1987-02-24 General Electric Company Airstream eductor
US5046689A (en) * 1989-04-19 1991-09-10 The Boeing Company Cowling interlock system
RU1766020C (ru) * 1989-12-20 1994-08-15 Авиационный комплекс им.С.В.Ильюшина Створка гондолы двигателя летательного аппарата
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
FR2756323B1 (fr) * 1996-11-28 1998-12-31 Hispano Suiza Sa Dispositif de liaison d'un inverseur de poussee a un turbomoteur
FR2771330B1 (fr) * 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
FR2772342B1 (fr) * 1997-12-16 2000-02-18 Aerospatiale Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
US6629712B2 (en) * 2001-03-30 2003-10-07 Hartwell Corporation Extendable latch
GB2384827A (en) * 2002-01-30 2003-08-06 Rolls Royce Plc A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine.
GB0320371D0 (en) * 2003-08-29 2003-10-01 Rolls Royce Plc A closure panel arrangement
FR2897339B1 (fr) * 2006-02-16 2008-04-11 Aircelle Sa Nacelle de turboreacteur a ouverture laterale des capots

Also Published As

Publication number Publication date
ES2377170T3 (es) 2012-03-23
US8333343B2 (en) 2012-12-18
CA2696765C (fr) 2015-02-17
FR2920141A1 (fr) 2009-02-27
EP2178760B1 (de) 2011-11-30
RU2480383C2 (ru) 2013-04-27
BRPI0813609A2 (pt) 2014-12-30
US20110272533A1 (en) 2011-11-10
EP2178760A1 (de) 2010-04-28
WO2009027590A1 (fr) 2009-03-05
CN101778769B (zh) 2013-10-16
CA2696765A1 (fr) 2009-03-05
CN101778769A (zh) 2010-07-14
RU2010109799A (ru) 2011-09-27
FR2920141B1 (fr) 2009-10-30

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