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FR2958266B1 - AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL - Google Patents

AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL

Info

Publication number
FR2958266B1
FR2958266B1 FR1052533A FR1052533A FR2958266B1 FR 2958266 B1 FR2958266 B1 FR 2958266B1 FR 1052533 A FR1052533 A FR 1052533A FR 1052533 A FR1052533 A FR 1052533A FR 2958266 B1 FR2958266 B1 FR 2958266B1
Authority
FR
France
Prior art keywords
mat
link assembly
reactor under
axis system
aircraft
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.)
Expired - Fee Related
Application number
FR1052533A
Other languages
French (fr)
Other versions
FR2958266A1 (en
Inventor
Pascal Gardes
Stephane Combes
Michael Berjot
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1052533A priority Critical patent/FR2958266B1/en
Publication of FR2958266A1 publication Critical patent/FR2958266A1/en
Application granted granted Critical
Publication of FR2958266B1 publication Critical patent/FR2958266B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • F16B21/12—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with locking-pins or split-pins thrust into holes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
FR1052533A 2010-04-02 2010-04-02 AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL Expired - Fee Related FR2958266B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1052533A FR2958266B1 (en) 2010-04-02 2010-04-02 AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052533A FR2958266B1 (en) 2010-04-02 2010-04-02 AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL

Publications (2)

Publication Number Publication Date
FR2958266A1 FR2958266A1 (en) 2011-10-07
FR2958266B1 true FR2958266B1 (en) 2012-03-23

Family

ID=43063897

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052533A Expired - Fee Related FR2958266B1 (en) 2010-04-02 2010-04-02 AXIS SYSTEM FOR LINK ASSEMBLY OF MAT-REACTOR UNDER AN AIRCRAFT VESSEL

Country Status (1)

Country Link
FR (1) FR2958266B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
FR3073824B1 (en) * 2017-11-23 2019-12-20 Airbus Operations AIRCRAFT ASSEMBLY COMPRISING A PRIMARY STRUCTURE OF A HANGING MAT FIXED TO A VEHICLE BOX BY FASTENERS PARTIALLY BURIED IN THE PRIMARY STRUCTURE

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1348727A (en) * 1918-02-23 1920-08-03 James R Mckinlay Bolt
US3831888A (en) * 1972-07-27 1974-08-27 Mc Donnell Douglas Corp Aircraft engine suspension system
FR2862610B1 (en) * 2003-11-25 2007-03-23 Airbus France ATTACHING DEVICE CONNECTING AN ENGINE AND AN AIRCRAFT SAIL
FR2878229B1 (en) * 2004-11-23 2008-04-18 Airbus France Sas SYSTEM FOR ATTACHING A MOTOR MAT TO THE WING OF AN AIRCRAFT
FR2915178B1 (en) * 2007-04-23 2009-07-10 Airbus France Sa ATTACHMENT OF A MAT BOX ON A SAIL, PINCING A SIDE PANEL OF THE HOUSING

Also Published As

Publication number Publication date
FR2958266A1 (en) 2011-10-07

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