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FR2985980A1 - Device for assembling and/or disassembling engine on reactor mast, in aircraft, has connection rod whose end is connected to fastener while another end of rod is connected to fixing unit attached with traction system - Google Patents

Device for assembling and/or disassembling engine on reactor mast, in aircraft, has connection rod whose end is connected to fastener while another end of rod is connected to fixing unit attached with traction system Download PDF

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Publication number
FR2985980A1
FR2985980A1 FR1250711A FR1250711A FR2985980A1 FR 2985980 A1 FR2985980 A1 FR 2985980A1 FR 1250711 A FR1250711 A FR 1250711A FR 1250711 A FR1250711 A FR 1250711A FR 2985980 A1 FR2985980 A1 FR 2985980A1
Authority
FR
France
Prior art keywords
aircraft
fastener
assembling
rod
traction system
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR1250711A
Other languages
French (fr)
Other versions
FR2985980B1 (en
Inventor
Philippe Mereau
Mickael Matignon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus SAS
Original Assignee
Airbus SAS
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 Airbus SAS filed Critical Airbus SAS
Priority to FR1250711A priority Critical patent/FR2985980B1/en
Publication of FR2985980A1 publication Critical patent/FR2985980A1/en
Application granted granted Critical
Publication of FR2985980B1 publication Critical patent/FR2985980B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

L'objet principal de l'invention est un dispositif (1) de montage et/ou démontage d'un élément propulsif (2) porté par une structure de support (3), caractérisé en ce qu'il comporte : - au moins un élément de fixation (7) destiné à être placé sur la structure de support (3), - au moins un organe d'accrochage (8) destiné à être solidarisé à un système de traction (10), - au moins une bielle de raccordement (9) dont une extrémité est reliée audit au moins un élément de fixation (7) et l'autre extrémité est reliée audit au moins un organe d'accrochage (8).The main object of the invention is a device (1) for mounting and / or dismounting a propulsive element (2) carried by a support structure (3), characterized in that it comprises: - at least one fastening element (7) intended to be placed on the support structure (3), - at least one fastening member (8) intended to be secured to a traction system (10), - at least one connecting rod (9) one end of which is connected to said at least one fastening element (7) and the other end is connected to said at least one fastening member (8).

FR1250711A 2012-01-25 2012-01-25 DEVICE FOR MOUNTING AND / OR DISASSEMBLING A PROPULSIVE ELEMENT AND ASSOCIATED METHOD Expired - Fee Related FR2985980B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1250711A FR2985980B1 (en) 2012-01-25 2012-01-25 DEVICE FOR MOUNTING AND / OR DISASSEMBLING A PROPULSIVE ELEMENT AND ASSOCIATED METHOD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1250711A FR2985980B1 (en) 2012-01-25 2012-01-25 DEVICE FOR MOUNTING AND / OR DISASSEMBLING A PROPULSIVE ELEMENT AND ASSOCIATED METHOD

Publications (2)

Publication Number Publication Date
FR2985980A1 true FR2985980A1 (en) 2013-07-26
FR2985980B1 FR2985980B1 (en) 2014-10-10

Family

ID=45873094

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1250711A Expired - Fee Related FR2985980B1 (en) 2012-01-25 2012-01-25 DEVICE FOR MOUNTING AND / OR DISASSEMBLING A PROPULSIVE ELEMENT AND ASSOCIATED METHOD

Country Status (1)

Country Link
FR (1) FR2985980B1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104229158A (en) * 2014-09-03 2014-12-24 上海交通大学 Six-degree-of-freedom positioning gesture adjusting equipment used for automatic assembling of large barrel-shaped thin-wall construction member
CN112407317A (en) * 2020-12-31 2021-02-26 南京迪沃航空技术有限公司 Multi-angle dismounting platform for aircraft engine and working method of multi-angle dismounting platform

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
DE8627720U1 (en) * 1986-10-17 1987-06-25 Becker, Günter, 5600 Wuppertal Mounting device
US5451134A (en) * 1991-10-22 1995-09-19 Bryfogle; Mark D. Material handling devices and controllers
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
US20040084916A1 (en) * 2002-10-31 2004-05-06 Cronk David W. Lift tool
US20100155566A1 (en) * 2008-12-24 2010-06-24 Mark Linz Method and apparatus for mounting and dismounting an aircraft engine
US20110265327A1 (en) * 2010-04-29 2011-11-03 Spirit Aerosystems, Inc. Apparatus and method for aircraft engine core exchange

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
DE8627720U1 (en) * 1986-10-17 1987-06-25 Becker, Günter, 5600 Wuppertal Mounting device
US5451134A (en) * 1991-10-22 1995-09-19 Bryfogle; Mark D. Material handling devices and controllers
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
US20040084916A1 (en) * 2002-10-31 2004-05-06 Cronk David W. Lift tool
US20100155566A1 (en) * 2008-12-24 2010-06-24 Mark Linz Method and apparatus for mounting and dismounting an aircraft engine
US20110265327A1 (en) * 2010-04-29 2011-11-03 Spirit Aerosystems, Inc. Apparatus and method for aircraft engine core exchange

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104229158A (en) * 2014-09-03 2014-12-24 上海交通大学 Six-degree-of-freedom positioning gesture adjusting equipment used for automatic assembling of large barrel-shaped thin-wall construction member
CN104229158B (en) * 2014-09-03 2016-05-25 上海交通大学 For the large tube-like thin-wall member six degree of freedom location posture adjustment equipment of assembling automatically
CN112407317A (en) * 2020-12-31 2021-02-26 南京迪沃航空技术有限公司 Multi-angle dismounting platform for aircraft engine and working method of multi-angle dismounting platform

Also Published As

Publication number Publication date
FR2985980B1 (en) 2014-10-10

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