FR2973086B1 - STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT - Google Patents

STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT

Info

Publication number
FR2973086B1
FR2973086B1 FR1152456A FR1152456A FR2973086B1 FR 2973086 B1 FR2973086 B1 FR 2973086B1 FR 1152456 A FR1152456 A FR 1152456A FR 1152456 A FR1152456 A FR 1152456A FR 2973086 B1 FR2973086 B1 FR 2973086B1
Authority
FR
France
Prior art keywords
opening
rod
aircraft
braid
main
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.)
Active
Application number
FR1152456A
Other languages
French (fr)
Other versions
FR2973086A1 (en
Inventor
Olivier Gau
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 FR1152456A priority Critical patent/FR2973086B1/en
Publication of FR2973086A1 publication Critical patent/FR2973086A1/en
Application granted granted Critical
Publication of FR2973086B1 publication Critical patent/FR2973086B1/en
Active 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • 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
    • F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

The rod (1) has two opposite ends (2), where each end has a main through opening (8) for allowing assembly of the rod on an upper/lower structure of an aircraft structural part i.e. wing box. Each end has a secondary through opening (14) whose dimension is smaller than that of the main opening. The secondary opening allows fixation of a bonding braid with the structure and the rod via respective ends of the braid, where the rod is made of composite material e.g. mixture of epoxy resin-impregnated carbon and/or glass fibers. A metal paint coating (22) is arranged around the secondary opening.
FR1152456A 2011-03-24 2011-03-24 STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT Active FR2973086B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1152456A FR2973086B1 (en) 2011-03-24 2011-03-24 STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1152456A FR2973086B1 (en) 2011-03-24 2011-03-24 STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT

Publications (2)

Publication Number Publication Date
FR2973086A1 FR2973086A1 (en) 2012-09-28
FR2973086B1 true FR2973086B1 (en) 2014-01-10

Family

ID=44548490

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1152456A Active FR2973086B1 (en) 2011-03-24 2011-03-24 STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT

Country Status (1)

Country Link
FR (1) FR2973086B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2829546B1 (en) * 2001-09-11 2004-02-20 Eurocopter France ENERGY ABSORPTION CONNECTION BAR, AND ITS APPLICATION AS A TRANSMISSION BOX SUSPENSION BAR FOR AIRCRAFT
DE102005038849A1 (en) * 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Aerofoil supporting structure for use in airplane, has bar unit with connection mechanism which is formed, such that power is centrally transferred between bar unit and node unit, when mechanism is in contact with node unit
US7788993B2 (en) * 2008-03-01 2010-09-07 The Boeing Company Tie rod assembly
US8667754B2 (en) * 2008-08-26 2014-03-11 The Boeing Company Composite tie rod and method for making the same

Also Published As

Publication number Publication date
FR2973086A1 (en) 2012-09-28

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FR2973086B1 (en) STRUCTURAL ROD, PREFERABLY FOR AIRCRAFT

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