ATE515436T1 - Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung - Google Patents

Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung

Info

Publication number
ATE515436T1
ATE515436T1 AT08805587T AT08805587T ATE515436T1 AT E515436 T1 ATE515436 T1 AT E515436T1 AT 08805587 T AT08805587 T AT 08805587T AT 08805587 T AT08805587 T AT 08805587T AT E515436 T1 ATE515436 T1 AT E515436T1
Authority
AT
Austria
Prior art keywords
section
nachel
fastening
engine
knife edge
Prior art date
Application number
AT08805587T
Other languages
English (en)
Inventor
Etienne Germain
Jean-Yves Elegoot
Patrice Dhainault
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 ATE515436T1 publication Critical patent/ATE515436T1/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
    • B64D29/06—Attaching of nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
AT08805587T 2007-08-20 2008-05-19 Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung ATE515436T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705891A FR2920137B1 (fr) 2007-08-20 2007-08-20 Fixation d'une structure d'une nacelle de turboreacteur par bride couteau/gorge renforcee
PCT/FR2008/000691 WO2009024655A1 (fr) 2007-08-20 2008-05-19 Fixation d'une structure d'une nacelle de turboreacteur par bride couteau/gorge renforcee

Publications (1)

Publication Number Publication Date
ATE515436T1 true ATE515436T1 (de) 2011-07-15

Family

ID=39148655

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08805587T ATE515436T1 (de) 2007-08-20 2008-05-19 Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung

Country Status (10)

Country Link
US (1) US8887511B2 (de)
EP (1) EP2188177B1 (de)
CN (1) CN101765542B (de)
AT (1) ATE515436T1 (de)
BR (1) BRPI0813041A2 (de)
CA (1) CA2696204C (de)
ES (1) ES2369119T3 (de)
FR (1) FR2920137B1 (de)
RU (1) RU2463214C2 (de)
WO (1) WO2009024655A1 (de)

Families Citing this family (12)

* 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
FR2962492B1 (fr) * 2010-07-07 2012-08-03 Aircelle Sa Dispositif d'inversion de poussee avec jonction aerodynamique de cadre avant
FR2962765B1 (fr) * 2010-07-13 2012-07-27 Snecma Turboreacteur avec un element de nacelle fixe au carter intermediaire
FR2963949A1 (fr) * 2010-08-18 2012-02-24 Aircelle Sa Poutre notamment pour inverseur de poussee a grilles
US10107202B2 (en) * 2014-11-26 2018-10-23 United Technologies Corporation Composite fan housing assembly of a turbofan engine and method of manufacture
US10093429B2 (en) 2015-07-07 2018-10-09 Rohr, Inc Latch beam deflection support
DE102016101168A1 (de) * 2016-01-22 2017-07-27 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit einer in einer Ausnehmung einer Wandung anordenbaren Einsetzeinrichtung
US10605198B2 (en) * 2016-04-15 2020-03-31 Rohr, Inc. Nacelle thrust reverser
US11473527B2 (en) 2016-09-28 2022-10-18 The Boeing Company Nacelle with tangential restraint
US10589868B2 (en) 2016-09-28 2020-03-17 The Boeing Company Nacelle cowl tangential restraint
FR3065260B1 (fr) * 2017-04-14 2020-10-09 Safran Aircraft Engines Systeme inverseur de poussee pour turboreacteur
FR3117173A1 (fr) 2020-12-09 2022-06-10 Safran Aircraft Engines Ensemble propulsif d’aéronef et procédé d’adaptation d’un ensemble propulsif

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4826106A (en) * 1987-02-18 1989-05-02 Grumman Aerospace Corporation Advanced composite aircraft cowl
US4998409A (en) * 1989-09-25 1991-03-12 Rohr Industries, Inc. Thrust reverser torque ring
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
US5076514A (en) * 1990-08-03 1991-12-31 The Boeing Company Apparatus for latching two parts together
US5239822A (en) * 1992-01-14 1993-08-31 The Boeing Company Composite structure for thrust reverser torque box
DE4340951A1 (de) * 1992-12-04 1994-06-09 Grumman Aerospace Corp Einstückiges Triebwerkeinlaß-Schallrohr
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
FR2756323B1 (fr) * 1996-11-28 1998-12-31 Hispano Suiza Sa Dispositif de liaison d'un inverseur de poussee a un turbomoteur
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US6557799B1 (en) * 2001-11-09 2003-05-06 The Boeing Company Acoustic treated thrust reverser bullnose fairing assembly
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.
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
CN100575690C (zh) * 2005-09-12 2009-12-30 波音公司 包括锁定机构的反推力装置及其制造方法
US7730715B2 (en) * 2006-05-15 2010-06-08 United Technologies Corporation Fan frame
CN2928682Y (zh) * 2006-06-06 2007-08-01 江西洪都航空工业集团有限责任公司 一种可调的发动机前罩圈
US7721525B2 (en) * 2006-07-19 2010-05-25 Rohr, Inc. Aircraft engine inlet having zone of deformation
FR2909974B1 (fr) * 2006-12-13 2009-02-06 Aircelle Sa Nacelle pour turboreacteur double flux
GB0807137D0 (en) * 2008-04-21 2008-05-21 Rolls Royce Plc Rear fan case for a gas turbine engine

Also Published As

Publication number Publication date
ES2369119T3 (es) 2011-11-25
US8887511B2 (en) 2014-11-18
CN101765542A (zh) 2010-06-30
RU2463214C2 (ru) 2012-10-10
US20100229526A1 (en) 2010-09-16
FR2920137A1 (fr) 2009-02-27
CN101765542B (zh) 2013-03-20
WO2009024655A1 (fr) 2009-02-26
BRPI0813041A2 (pt) 2014-12-16
EP2188177B1 (de) 2011-07-06
RU2010109809A (ru) 2011-09-27
CA2696204A1 (fr) 2009-02-26
CA2696204C (fr) 2014-05-06
FR2920137B1 (fr) 2009-09-18
EP2188177A1 (de) 2010-05-26

Similar Documents

Publication Publication Date Title
ATE515436T1 (de) Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung
BR112012013131A2 (pt) estrutura de suporte para uma nacela de motor turbojato, nacela de aeronaves.
US11988283B2 (en) Non-metallic engine case inlet compression seal for a gas turbine engine
ATE444896T1 (de) Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel
EP2631434A3 (de) Turbinenummantelung mit geringer Leitfähigkeit
GB201112001D0 (en) Turbine blade assembly including a damper
BRPI0713172A2 (pt) motor a jato para aeronave
EP2336026A3 (de) Integrierte Gondelbaugruppe
EP2378072A3 (de) Nebenstromkanal eines Turbofantriebwerkes
US10145268B2 (en) Injection molded composite fan platform
MX2009012521A (es) Arreglo de alabes de rotor, especialmente para una turbina de gas.
EP2078826A3 (de) Gasturbinenmotorgehäuse
EP2706241A3 (de) Ventilatorschaufel
WO2015080781A3 (en) Ply architecture for integral platform and damper retaining features in cmc turbine blades
MX336351B (es) Turbomaquina axial con reducidas perdidas intersticiales.
EP2599959A3 (de) Keramikmatrix-Verbundstrukturen einer Schaufel mit Verstärkungs- Hinterkante für Gasturbinenmotor
FR2961846B1 (fr) Aube de turbomachine a geometrie asymetrique complementaire
EP2570641A3 (de) Fangehäuse mit Schubumkehrgitter, zugehöriger Fan und Gasturbinentriebwerk
BRPI0908165A2 (pt) distribuidor satorizado para uma turbomáquina, turbina baixa-pressão de turbomáquina e turbomáquina tal como um turborreator ou um turbopropulsor de avião
EP2537755A3 (de) Montageanordnung
GB0907580D0 (en) A duct wall for a fan or a gas turbine engine
ATE508045T1 (de) Propellerschaufelfixierung
EP2236757A3 (de) Geteilte Rotorscheibenanordnung für ein Gasturbinentriebwerk
WO2009024662A3 (fr) Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur
BRPI0907645A2 (pt) Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião

Legal Events

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