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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C17/00—Overhead 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
- B66C17/06—Overhead 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/50—Handling or transporting aircraft components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C1/00—Load-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
- B66C1/10—Load-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
- B66C1/107—Load-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
-
- 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
- Y10T29/00—Metal working
- Y10T29/53—Means 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.
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)
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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)
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 |
-
2008
- 2008-12-24 US US12/343,848 patent/US8262050B2/en active Active
-
2009
- 2009-12-15 ES ES09179294.5T patent/ES2456490T3/es active Active
- 2009-12-15 EP EP09179294.5A patent/EP2202156B1/en not_active Not-in-force
- 2009-12-17 MX MX2009013967A patent/MX2009013967A/es active IP Right Grant
- 2009-12-17 CA CA2688753A patent/CA2688753C/en not_active Expired - Fee Related
- 2009-12-20 IL IL202844A patent/IL202844A/en not_active IP Right Cessation
- 2009-12-23 BR BRPI0905611-4A patent/BRPI0905611A2/pt not_active Application Discontinuation
- 2009-12-24 CN CN200910215943.5A patent/CN101797981B/zh active Active
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 |
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Legal Events
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FG | Grant or registration |