FR2836890B1 - Dispositif de fixation pour un carenage - Google Patents

Dispositif de fixation pour un carenage

Info

Publication number
FR2836890B1
FR2836890B1 FR0202951A FR0202951A FR2836890B1 FR 2836890 B1 FR2836890 B1 FR 2836890B1 FR 0202951 A FR0202951 A FR 0202951A FR 0202951 A FR0202951 A FR 0202951A FR 2836890 B1 FR2836890 B1 FR 2836890B1
Authority
FR
France
Prior art keywords
fairing
fixing device
fixing
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
FR0202951A
Other languages
English (en)
Other versions
FR2836890A1 (fr
Inventor
Francois Rouyre
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 FR0202951A priority Critical patent/FR2836890B1/fr
Priority to FR0206472A priority patent/FR2836963A1/fr
Priority to EP03352004A priority patent/EP1342927B1/fr
Priority to DE60305360T priority patent/DE60305360T2/de
Priority to AT03352004T priority patent/ATE327444T1/de
Priority to BRPI0300431-7A priority patent/BR0300431B1/pt
Priority to US10/383,664 priority patent/US6889939B2/en
Priority to CA2420352A priority patent/CA2420352C/fr
Publication of FR2836890A1 publication Critical patent/FR2836890A1/fr
Application granted granted Critical
Publication of FR2836890B1 publication Critical patent/FR2836890B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C7/00Structures or fairings not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B35/00Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B37/00Nuts or like thread-engaging members
    • F16B37/04Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/041Releasable devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B37/00Nuts or like thread-engaging members
    • F16B37/04Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/048Non-releasable devices
FR0202951A 2002-03-08 2002-03-08 Dispositif de fixation pour un carenage Expired - Fee Related FR2836890B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0202951A FR2836890B1 (fr) 2002-03-08 2002-03-08 Dispositif de fixation pour un carenage
FR0206472A FR2836963A1 (fr) 2002-03-08 2002-05-28 Dispositif de fixation d'un element sur une structure d'aeronef
DE60305360T DE60305360T2 (de) 2002-03-08 2003-03-04 Vorrichtung zum Befestigen eines Bauteils an einer Luftfahrzeugstruktur
AT03352004T ATE327444T1 (de) 2002-03-08 2003-03-04 Vorrichtung zum befestigen eines bauteils an einer luftfahrzeugstruktur
EP03352004A EP1342927B1 (fr) 2002-03-08 2003-03-04 Dispositif de fixation d'un élément sur une structure d'aéronef
BRPI0300431-7A BR0300431B1 (pt) 2002-03-08 2003-03-06 dispositivo de fixaÇço de um elemento em uma estrutura de aeronave.
US10/383,664 US6889939B2 (en) 2002-03-08 2003-03-07 Device for fixing a member to an aircraft structure
CA2420352A CA2420352C (fr) 2002-03-08 2003-03-07 Dispositif de fixation d'un element sur une structure d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0202951A FR2836890B1 (fr) 2002-03-08 2002-03-08 Dispositif de fixation pour un carenage

Publications (2)

Publication Number Publication Date
FR2836890A1 FR2836890A1 (fr) 2003-09-12
FR2836890B1 true FR2836890B1 (fr) 2004-06-11

Family

ID=27763655

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0202951A Expired - Fee Related FR2836890B1 (fr) 2002-03-08 2002-03-08 Dispositif de fixation pour un carenage

Country Status (1)

Country Link
FR (1) FR2836890B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.
DE102007011611B4 (de) 2007-01-22 2010-12-09 Airbus Deutschland Gmbh Befestigungsanordnung für Verzurrbügel in einem Frachtraumboden eines Flugzeugs
FR2936489B1 (fr) 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
US10773788B2 (en) 2017-08-15 2020-09-15 The Boeing Company Fairing assembly and method therefor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3563131A (en) * 1969-04-23 1971-02-16 Lockheed Aircraft Corp Spacer
US5542777A (en) * 1994-07-12 1996-08-06 Martin Marietta Corporation Fastener for composite structures

Also Published As

Publication number Publication date
FR2836890A1 (fr) 2003-09-12

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20111130