ATE473164T1 - Gondel für zweistromtriebwerk - Google Patents

Gondel für zweistromtriebwerk

Info

Publication number
ATE473164T1
ATE473164T1 AT07858440T AT07858440T ATE473164T1 AT E473164 T1 ATE473164 T1 AT E473164T1 AT 07858440 T AT07858440 T AT 07858440T AT 07858440 T AT07858440 T AT 07858440T AT E473164 T1 ATE473164 T1 AT E473164T1
Authority
AT
Austria
Prior art keywords
panel
framework
rear section
gondola
turbojet
Prior art date
Application number
AT07858440T
Other languages
English (en)
Inventor
Guy Vauchel
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 ATE473164T1 publication Critical patent/ATE473164T1/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
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Medicines Containing Material From Animals Or Micro-Organisms (AREA)
AT07858440T 2006-12-13 2007-10-15 Gondel für zweistromtriebwerk ATE473164T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0610850A FR2909974B1 (fr) 2006-12-13 2006-12-13 Nacelle pour turboreacteur double flux
PCT/FR2007/001678 WO2008093003A1 (fr) 2006-12-13 2007-10-15 Nacelle pour turboréacteur double flux

Publications (1)

Publication Number Publication Date
ATE473164T1 true ATE473164T1 (de) 2010-07-15

Family

ID=38235715

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07858440T ATE473164T1 (de) 2006-12-13 2007-10-15 Gondel für zweistromtriebwerk

Country Status (11)

Country Link
US (1) US8668441B2 (de)
EP (1) EP2102061B1 (de)
CN (1) CN101541635B (de)
AT (1) ATE473164T1 (de)
BR (1) BRPI0720298A2 (de)
CA (1) CA2671556C (de)
DE (1) DE602007007669D1 (de)
ES (1) ES2347923T3 (de)
FR (1) FR2909974B1 (de)
RU (1) RU2440280C2 (de)
WO (1) WO2008093003A1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920137B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Fixation d'une structure d'une nacelle de turboreacteur par bride couteau/gorge renforcee
ES2386136B1 (es) * 2009-03-30 2013-07-25 Airbus Operations, S.L. Estructura para el acoplamiento de la carena de una aeronave
FR2946621B1 (fr) * 2009-06-15 2013-02-08 Aircelle Sa Procede d'assemblage d'une protection thermique sur une structure interne fixe de nacelle de turboreacteur
FR2957894B1 (fr) * 2010-03-23 2013-06-14 Snecma Pylone de support d'un turbomoteur recouvert d'un materiau poreux, ensemble d'un turbomoteur et d'un pylone
GB201101609D0 (en) * 2011-01-31 2011-03-16 Rolls Royce Plc Attenuation of open rotor noise
US8979490B2 (en) * 2011-09-29 2015-03-17 Hamilton Sundstrand Corporation Fan inlet diffuser housing riveted center body retention
FR2985501B1 (fr) * 2012-01-05 2013-12-27 Aircelle Sa Joint d'etancheite pour pylone et nacelle de turboreacteur et ensemble de pylone et nacelle de turboreacteur incorporant un tel joint d'etancheite
US9856745B2 (en) * 2012-02-28 2018-01-02 United Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
US10837367B2 (en) * 2012-02-28 2020-11-17 Raytheon Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
US9347397B2 (en) 2012-08-02 2016-05-24 United Technologies Corporation Reflex annular vent nozzle
US9168716B2 (en) * 2012-09-14 2015-10-27 The Boeing Company Metallic sandwich structure having small bend radius
US9447700B2 (en) * 2013-02-19 2016-09-20 United Technologies Corporation Thermally free hanger with length adjustment feature
FR3006723B1 (fr) 2013-06-11 2015-12-04 Snecma Dispositif de fixation de deux pieces entre elles
US9909501B2 (en) * 2013-07-03 2018-03-06 Pratt & Whitney Canada Corp. Acoustic structure for a gas turbine engine
US10294863B2 (en) 2013-07-09 2019-05-21 United Technologies Corporation Preloaded AFT vent area for low pressure fan ducts
GB201314061D0 (en) * 2013-08-06 2013-09-18 Rolls Royce Plc Attachment device for non-permanently attaching a child component to a parent component
FR3010048B1 (fr) 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a cales de liaison
FR3010049B1 (fr) * 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a secteurs de virole pivotants
FR3059299B1 (fr) * 2016-11-30 2021-11-12 Safran Nacelles Nacelle de turboreacteur d’aeronef, ensemble propulsif et aeronef comportant une telle nacelle
US10460978B2 (en) * 2017-03-08 2019-10-29 Lam Research Corporation Boltless substrate support assembly
FR3071821B1 (fr) * 2017-09-29 2019-10-04 Airbus Operations Turboreacteur double flux pour un aeronef avec une ouverture amelioree
CN110466782B (zh) * 2019-07-26 2022-12-20 中国航发沈阳发动机研究所 一种航空发动机用弹性连接组件
US11518535B2 (en) * 2019-09-30 2022-12-06 Rohr, Inc. Nacelle cowl deflection limiter
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure
CN113548189A (zh) * 2021-09-08 2021-10-26 中国航空工业集团公司西安飞机设计研究所 一种无人机发动机舱结构
EP4488181A1 (de) * 2023-07-06 2025-01-08 Airbus Operations (S.A.S.) Antriebssystem für ein flugzeug mit einem strahltriebwerk, einem pylon und einer motorbefestigung

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1095605A (fr) * 1953-08-06 1955-06-03 Perfectionnements apportés aux dispositifs de fixation de panneaux, capots, couvercles, etc.
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4293053A (en) * 1979-12-18 1981-10-06 United Technologies Corporation Sound absorbing structure
EP0145809B1 (de) * 1983-12-19 1987-11-19 The Boeing Company Vorrichtung und Methode zur Verkleinerung der Achsenverbiegung eines Triebwerks
FR2560854B1 (fr) 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US4751979A (en) * 1985-05-16 1988-06-21 Airborne Express, Inc. Engine noise suppression kit for the nacelles of a jet aircraft
GB2244047B (en) * 1990-05-17 1994-02-16 Rolls Royce Plc Inspection aperture sealing
US5275529A (en) * 1992-03-16 1994-01-04 General Electric Company Sandwich panel joint
UA26001C2 (uk) * 1994-08-23 1999-02-26 Запорізьке Машинобудівне Конструкторське Бюро "Прогрес" Ім. Академіка О.Г. Івченка Пристрій кріплеhhя капота реактивhого двигуhа літальhого апарата
GB2312251B (en) * 1996-04-18 1999-10-27 Rolls Royce Plc Ducted fan gas turbine engine mounting
FR2767560B1 (fr) * 1997-08-19 1999-11-12 Aerospatiale Ensemble reducteur de bruit pour turboreacteur d'aeronef
US6330985B1 (en) * 2000-06-30 2001-12-18 General Electric Company Link component for aircraft engine mounting systems
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
US6913441B2 (en) * 2003-09-04 2005-07-05 Siemens Westinghouse Power Corporation Turbine blade ring assembly and clocking method
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
US7104756B2 (en) * 2004-08-11 2006-09-12 United Technologies Corporation Temperature tolerant vane assembly
GB0418454D0 (en) * 2004-08-19 2004-09-22 Rolls Royce Plc An engine mounting assembly
US7467687B2 (en) * 2004-11-12 2008-12-23 General Electric Company Thermal—acoustic enclosure
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2903076B1 (fr) 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante

Also Published As

Publication number Publication date
EP2102061A1 (de) 2009-09-23
RU2440280C2 (ru) 2012-01-20
BRPI0720298A2 (pt) 2014-02-04
RU2009125710A (ru) 2011-01-20
FR2909974A1 (fr) 2008-06-20
WO2008093003A1 (fr) 2008-08-07
EP2102061B1 (de) 2010-07-07
ES2347923T3 (es) 2010-11-25
US8668441B2 (en) 2014-03-11
CN101541635B (zh) 2012-05-02
CA2671556A1 (fr) 2008-08-07
US20100024435A1 (en) 2010-02-04
CN101541635A (zh) 2009-09-23
DE602007007669D1 (de) 2010-08-19
CA2671556C (fr) 2014-05-06
WO2008093003A8 (fr) 2008-10-09
FR2909974B1 (fr) 2009-02-06

Similar Documents

Publication Publication Date Title
ATE473164T1 (de) Gondel für zweistromtriebwerk
DE602007003981D1 (de) Strukturgondel
ATE444896T1 (de) Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel
EP2071155A3 (de) Gondelanordnung mit Turbulatorelementen
DE602007004959D1 (de) Abdeckstruktur für einen lufteinlass
RU2009104473A (ru) Силовая установка летательного аппарата, содержащая соединительный аэродинамический обтекатель, смонтированный на двух отдельных элементах
EP1895140A3 (de) Lüfterabgasdüse für den Motor eines Turbolüfters
ATE341483T1 (de) Aufhängevorrichtung eines flugzeugtriebwerks an einem flügelpylon
ATE539962T1 (de) Eintrittskante eines flugzeuges
BRPI0914686A8 (pt) sistema propulsor de aeronave
BRPI0818497A2 (pt) Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar.
EP2003309A3 (de) Gondel mit veränderlicher Geometrie mit nanoelektromechanischem System für ein Flugzeugtriebwerk und enstprechendes Betriebsverfahren
BRPI0815705A2 (pt) Conjunto motor para aeronave, e, aeronave.
RU2011109214A (ru) Внутренняя стенка гондолы газотурбинного двигателя
ATE343516T1 (de) Aufhängevorrichtung eines flugzeugtriebwerks an einem flügelpylon
ATE452825T1 (de) Motoranordnung für ein flugzeug mit einem motor sowie einer motormontagestruktur für einen derartigen motor
ATE445771T1 (de) Triebwerk für ein flugzeug
WO2009090327A3 (fr) Nacelle a capotage simplifie
EP2330036A3 (de) Träger einer Verdichterhaubenteil für ein Mantelstromtriebwerk
CA2576683C (en) Aircraft auxiliary gas turbine engine and method for operating
WO2009098402A3 (fr) Système de verrouillage pour structure d'entrée d'air d'une nacelle de turboréacteur
WO2009024662A3 (fr) Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur
DE602006006185D1 (de) Enteisungssystem für die Anströmkante einer Einlasshaube eines Turbinentriebwerks
WO2010061071A3 (fr) Nacelle integree sur aile volante
EP2327628A3 (de) Verfahren und Systeme zur Minderung von durch vorgelagerte Triebwerkaufhängungen verursachte Strömungsstörungen in Flugzeugpropellerschaufeln

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties