MX2009013967A - Metodo y aparato para montar y desmontar un motor de aeronave. - Google Patents

Metodo y aparato para montar y desmontar un motor de aeronave.

Info

Publication number
MX2009013967A
MX2009013967A MX2009013967A MX2009013967A MX2009013967A MX 2009013967 A MX2009013967 A MX 2009013967A MX 2009013967 A MX2009013967 A MX 2009013967A MX 2009013967 A MX2009013967 A MX 2009013967A MX 2009013967 A MX2009013967 A MX 2009013967A
Authority
MX
Mexico
Prior art keywords
engine
movable
aircraft engine
aircraft
frame
Prior art date
Application number
MX2009013967A
Other languages
English (en)
Inventor
Mark Linz
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of MX2009013967A publication Critical patent/MX2009013967A/es

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C17/00Overhead travelling cranes comprising one or more substantially horizontal girders the ends of which are directly supported by wheels or rollers running on tracks carried by spaced supports
    • B66C17/06Overhead travelling cranes comprising one or more substantially horizontal girders the ends of which are directly supported by wheels or rollers running on tracks carried by spaced supports specially adapted for particular purposes, e.g. in foundries, forges; combined with auxiliary apparatus serving particular purposes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50Handling or transporting aircraft components
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C1/00Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
    • B66C1/10Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
    • B66C1/107Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means for lifting engines
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/53Means to assemble or disassemble

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Assembly (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
  • Connection Of Plates (AREA)
  • Wind Motors (AREA)

Abstract

Se describen un aparato y método para remover un motor de aeronave. El método incluye montar un ensamble de marco en conexión soportada con un miembro de soporte de una aeronave asociada. El ensamble de marco incluye un miembro de marco, un ensamble movible montado en una relación móvil al miembro de marco, y una pluralidad de manivelas de motor montada en conexión soportada con el miembro móvil. Cada manivela de motor tiene un cable de motor asociado operablemente conectado a la misma. El ensamble móvil se puede mover entre posiciones hacia adelante y hacia atrás. El método además incluye soportar el peso de por lo menos una porción de un motor de aeronave con los cables de motor y mover el miembro móvil con relación al miembro de marco para desplazar la porción del motor de aeronave.
MX2009013967A 2008-12-24 2009-12-17 Metodo y aparato para montar y desmontar un motor de aeronave. MX2009013967A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/343,848 US8262050B2 (en) 2008-12-24 2008-12-24 Method and apparatus for mounting and dismounting an aircraft engine

Publications (1)

Publication Number Publication Date
MX2009013967A true MX2009013967A (es) 2010-06-25

Family

ID=41694623

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2009013967A MX2009013967A (es) 2008-12-24 2009-12-17 Metodo y aparato para montar y desmontar un motor de aeronave.

Country Status (8)

Country Link
US (1) US8262050B2 (es)
EP (1) EP2202156B1 (es)
CN (1) CN101797981B (es)
BR (1) BRPI0905611A2 (es)
CA (1) CA2688753C (es)
ES (1) ES2456490T3 (es)
IL (1) IL202844A (es)
MX (1) MX2009013967A (es)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2952921B1 (fr) * 2009-11-20 2012-05-25 Snecma Chariot de transport d'un module de moteur d'aeronef
FR2952922B1 (fr) * 2009-11-20 2012-05-25 Snecma Ensemble de manutention d'un module de moteur d'aeronef
US8720059B2 (en) * 2010-04-29 2014-05-13 Spirit Aerosystems, Inc. Apparatus and method for aircraft engine core exchange
CN102092663B (zh) * 2010-12-02 2012-10-03 中冶北方工程技术有限公司 混合机挡辊的简易拆装方法
US9228451B2 (en) 2011-05-03 2016-01-05 Pratt & Whitney Canada Corp. Gas turbine engine module adapter to a carrier
FR2978729B1 (fr) * 2011-08-03 2013-07-19 Aircelle Sa Poutre composite pour structure support de nacelle de turboreacteur
FR2985980B1 (fr) * 2012-01-25 2014-10-10 Airbus Dispositif de montage et/ou demontage d'un element propulsif et procede associe
CN103318415B (zh) * 2012-03-21 2015-10-14 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机安装维护用升降装置
CN103818815B (zh) * 2012-11-16 2016-01-27 中航商用航空发动机有限责任公司 发动机吊装结构
CN103303483B (zh) * 2013-04-16 2015-12-30 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机安装维护用旋转机构
WO2014206380A1 (en) * 2013-06-27 2014-12-31 Hennlich S.R.O. Mounting set for mounting and dismounting of aircraft engines
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
WO2015015262A1 (en) * 2013-07-29 2015-02-05 Bombardier Inc. Method for attachment of a pre-assembled powerplant and pylon assembly to an aircraft
CN103557752B (zh) * 2013-10-29 2016-03-30 北京航天发射技术研究所 导弹冷弹射的动力装置用装填设备
WO2015168637A1 (en) * 2014-05-02 2015-11-05 Morey Joel T Aircraft engine stand
JP6533043B2 (ja) * 2014-08-25 2019-06-19 三菱航空機株式会社 航空機エンジンの取り付け方法
JP6137103B2 (ja) * 2014-09-30 2017-05-31 Jfeスチール株式会社 天井クレーンの走行桁補強工法及びこの工法で使用する吊り治具
CN104724300B (zh) * 2015-03-27 2016-12-07 沈阳飞机工业(集团)有限公司 飞机发动机安装车用定位系统及其定位方法
FR3039824B1 (fr) * 2015-08-07 2018-11-09 Safran Aircraft Engines Kit pour le guidage d'une turbomachine d'aeronef pendant sa pose / depose le long d'un berceau
CN105798594B (zh) * 2016-04-25 2018-02-02 中国南方电网有限责任公司超高压输电公司曲靖局 一种同轴电缆2m数字端子投退装置
FR3058704B1 (fr) * 2016-11-14 2018-11-16 Safran Aircraft Engines Berceau bipartite a coulissement pour turbopropulseur
US10899463B2 (en) 2017-05-16 2021-01-26 Rohr, Inc. Segmented pylon for an aircraft propulsion system
CN107738223B (zh) * 2017-11-13 2023-11-10 山东太古飞机工程有限公司 飞机发动机第一级静子叶片整流罩的拆装辅助工装
EP3489146B1 (en) 2017-11-24 2022-03-30 Airbus Operations, S.L. Aircraft with a system for rearward mounting and dismounting an engine and method for rearward dismounting an engine
DE102018209890A1 (de) * 2018-06-19 2019-12-19 MTU Aero Engines AG Montageträger zum hängenden Aufnehmen einer Gasturbine
SG11202111294QA (en) * 2019-04-25 2021-11-29 Aerovironment Inc Ground support equipment for a high altitude long endurance aircraft
US11518514B2 (en) 2019-04-25 2022-12-06 Aerovironment, Inc Off-center parachute flight termination system including latch mechanism disconnectable by burn wire
JP7472169B2 (ja) 2019-04-25 2024-04-22 エアロバイロメント,インコーポレイテッド 高高度長航続時間航空機の上昇及び滑空動作の方法
DE102019113437A1 (de) * 2019-05-21 2020-11-26 Airbus Operations Gmbh Verfahren und ein System zum Installieren einer Komponente in einem Innenraum eines Rumpfes eines Transportmittels
CN111408918B (zh) * 2020-03-31 2022-04-26 中国航发动力股份有限公司 一种发动机低压涡轮的牵引工装
US11873727B2 (en) * 2021-04-15 2024-01-16 General Electric Company System and method for hoisting gas engine assemblies

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB273912A (en) * 1926-07-24 1927-07-14 Blackburn Aeroplane & Motor Co Improvements in or connected with means for changing or installing engines on aircraft
DE742348C (de) * 1940-09-10 1943-11-30 Ernst Heinkel Flugzeugwerke G Montagekran fuer Flugzeugmotoren
US3071349A (en) * 1958-12-12 1963-01-01 Herbert L Glaze Hoist
GB2044358B (en) * 1979-03-10 1983-01-19 Rolls Royce Gas turbine jet engine mounting
IT1142775B (it) * 1981-05-22 1986-10-15 Alitalia Spa Posizionatore idro-pneumatico per il cambio di motori alari di velivoli a simili
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
GB8822798D0 (en) 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
FR2677954B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere du carter d'echappement d'un turboreacteur.
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5284011A (en) * 1992-12-14 1994-02-08 General Electric Company Damped turbine engine frame
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
GB2303884B (en) * 1995-04-13 1999-07-14 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5816367A (en) * 1995-11-30 1998-10-06 Stanley Aviation Corporation Jet aircraft engine transport apparatus
US5645389A (en) * 1995-11-30 1997-07-08 Stanley Aviation Corporation Shipping frame from fan section of aircraft engine
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
US6223524B1 (en) * 1998-01-23 2001-05-01 Diversitech, Inc. Shrouds for gas turbine engines and methods for making the same
US6170141B1 (en) * 1998-09-25 2001-01-09 Stanley Aviation Corporation Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
GB9921935D0 (en) * 1999-09-17 1999-11-17 Rolls Royce A nacelle assembly for a gas turbine engine
US6401448B1 (en) * 2000-08-31 2002-06-11 General Electric Company System for mounting aircraft engines
FR2867156B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
US7175168B2 (en) * 2005-05-26 2007-02-13 Hardaker John C Wing positioner for installing and removing an aircraft wing
FR2903076B1 (fr) * 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
US7810799B2 (en) * 2006-07-31 2010-10-12 Prw Industries, Inc. Collapsible engine test stand
US7610819B2 (en) * 2006-08-01 2009-11-03 Avl North America Inc. Transmission headstock for test stands
FR2905990A1 (fr) * 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
US8523516B2 (en) * 2006-10-11 2013-09-03 Aircelle Bypass turbojet engine nacelle
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
US20090278021A1 (en) * 2008-05-06 2009-11-12 Eads Construcciones Aeronauticas, S.A. Device for removing and installing aircraft components
US7963542B2 (en) * 2008-08-29 2011-06-21 Solar Turbines Incorporated Modular cart for a gas turbine engine

Also Published As

Publication number Publication date
EP2202156B1 (en) 2014-03-05
EP2202156A2 (en) 2010-06-30
EP2202156A3 (en) 2013-01-09
BRPI0905611A2 (pt) 2011-03-29
CN101797981A (zh) 2010-08-11
US20100155566A1 (en) 2010-06-24
ES2456490T3 (es) 2014-04-22
IL202844A (en) 2015-03-31
US8262050B2 (en) 2012-09-11
CN101797981B (zh) 2014-08-20
CA2688753A1 (en) 2010-06-24
CA2688753C (en) 2017-02-14

Similar Documents

Publication Publication Date Title
MX2009013967A (es) Metodo y aparato para montar y desmontar un motor de aeronave.
EP2318709A4 (en) MAINTENANCE SYSTEM FOR WIND TURBINE EQUIPMENT
WO2009048266A3 (en) System and method for installing filtering membrane module to frame structure
EP2607658A3 (en) Accessory mounting for a gas turbine
BRPI0716661A2 (pt) Aparelho e método para prover compensação de levantamento para uma carga suspensa de uma extremidade de um cabo em um ambiente marinho, com a outra extremidade do cabo.
BRPI0820602A2 (pt) método de manuseio e/ou manutenção de componentes de turbina eólica, dispositivo de fixação para a montagem de equipamentos em turbina eólica, método de suspensão de cabos, lança de nacele, método de instalação de turbina eólica e turbina eólica
MY154527A (en) Flexible pipe support
EP2604851A3 (en) A wind turbine nacelle cover and a method for installing a generator on a mainframe in a nacelle
IN2012DN03852A (es)
GB2498293A (en) Windscreen installation apparatus and method
EP2468596A3 (en) A method of monitoring aircraft brake performance and apparatus for performing such a method
EP2818667A3 (en) An accessory mounting for a gas turbine engine
WO2011101669A3 (en) Service platform
CN102426900B (zh) 可移动式变压器安装平台
AR057177A1 (es) Instalacion de ascensor con equipamiento para la compensacion de la diferencia de peso entre los ramales de la cabina y los ramales del contrapeso del medio de soporte y metodo para realizar tal compensacion
NZ598572A (en) Hydraulic turbine engines, typically as stacked modules, lifted and lowered with guiding winching cables connected to base seat
SG169308A1 (en) Crane device and method
SG127859A1 (en) Support means with mechanically positive connection for connecting several cables
WO2009130023A3 (de) Modulare wasserturbine und verfahren für deren montage
CN202978103U (zh) 一种绝缘子用卡具
WO2009129949A3 (de) Vorrichtung und verfahren für die montage und den service von unterwasserkraftwerken
FR2975372B1 (fr) Aeronef comprenant des moyens ameliores de support d'une structure de plancher
PL2175087T3 (pl) Sposób montażu i demontażu rusztowania przejezdnego
CN103879915A (zh) 电动环链葫芦导链座系统
CN203740934U (zh) Dy系列电动环链葫芦导链座系统

Legal Events

Date Code Title Description
FG Grant or registration