FR2883939B1 - ROD AND METHOD FOR MANUFACTURING SUCH ROD - Google Patents

ROD AND METHOD FOR MANUFACTURING SUCH ROD

Info

Publication number
FR2883939B1
FR2883939B1 FR0550794A FR0550794A FR2883939B1 FR 2883939 B1 FR2883939 B1 FR 2883939B1 FR 0550794 A FR0550794 A FR 0550794A FR 0550794 A FR0550794 A FR 0550794A FR 2883939 B1 FR2883939 B1 FR 2883939B1
Authority
FR
France
Prior art keywords
rod
manufacturing
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
FR0550794A
Other languages
French (fr)
Other versions
FR2883939A1 (en
Inventor
Olivier Teulou
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 FR0550794A priority Critical patent/FR2883939B1/en
Publication of FR2883939A1 publication Critical patent/FR2883939A1/en
Application granted granted Critical
Publication of FR2883939B1 publication Critical patent/FR2883939B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02—Constructions of connecting-rods with constant length
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
FR0550794A 2005-03-29 2005-03-29 ROD AND METHOD FOR MANUFACTURING SUCH ROD Expired - Fee Related FR2883939B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0550794A FR2883939B1 (en) 2005-03-29 2005-03-29 ROD AND METHOD FOR MANUFACTURING SUCH ROD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0550794A FR2883939B1 (en) 2005-03-29 2005-03-29 ROD AND METHOD FOR MANUFACTURING SUCH ROD

Publications (2)

Publication Number Publication Date
FR2883939A1 FR2883939A1 (en) 2006-10-06
FR2883939B1 true FR2883939B1 (en) 2008-09-05

Family

ID=35229761

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0550794A Expired - Fee Related FR2883939B1 (en) 2005-03-29 2005-03-29 ROD AND METHOD FOR MANUFACTURING SUCH ROD

Country Status (1)

Country Link
FR (1) FR2883939B1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007011613B4 (en) 2007-01-22 2011-07-28 Airbus Operations GmbH, 21129 Fitting for the introduction of high forces in a fuselage cell of an aircraft
DE102008044759B4 (en) 2008-08-28 2013-09-19 Airbus Operations Gmbh Support for an aircraft structural component which can be produced using the selective laser melting method
DE102009058359A1 (en) 2009-12-15 2011-06-16 Airbus Operations Gmbh Force introduction fitting for lightweight components
FR2965867B1 (en) * 2010-10-12 2013-08-09 Airbus Operations Sas STRUCTURAL ROD ADAPTED TO FILTER LONGITUDINAL VIBRATIONS
EP2607229B1 (en) * 2011-12-22 2016-05-11 Airbus Operations, S.L. Composite rod and manufacturing method
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2545556B1 (en) * 1983-05-03 1985-08-09 Skf Cie Applic Mecanique METHOD FOR MANUFACTURING DISMANTLABLE AND ADJUSTABLE SECURITY CONNECTING RODS AND CONNECTING RODS OBTAINED BY THIS PROCESS
FR2599793B1 (en) * 1986-06-09 1988-10-21 Aerospatiale CONNECTING ROD SYSTEM FOR RESISTING A THRESHOLD OF LONGITUDINAL STRAPS

Also Published As

Publication number Publication date
FR2883939A1 (en) 2006-10-06

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

ST Notification of lapse

Effective date: 20151130