ATE327444T1 - Vorrichtung zum befestigen eines bauteils an einer luftfahrzeugstruktur - Google Patents

Vorrichtung zum befestigen eines bauteils an einer luftfahrzeugstruktur

Info

Publication number
ATE327444T1
ATE327444T1 AT03352004T AT03352004T ATE327444T1 AT E327444 T1 ATE327444 T1 AT E327444T1 AT 03352004 T AT03352004 T AT 03352004T AT 03352004 T AT03352004 T AT 03352004T AT E327444 T1 ATE327444 T1 AT E327444T1
Authority
AT
Austria
Prior art keywords
spoke
aircraft structure
attaching
component
cooperating
Prior art date
Application number
AT03352004T
Other languages
English (en)
Inventor
Francois Rouyre
Lay Loic Le
Original Assignee
Airbus France
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
Priority claimed from FR0202951A external-priority patent/FR2836890B1/fr
Application filed by Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE327444T1 publication Critical patent/ATE327444T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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
    • F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • 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
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/041—Releasable devices
    • 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
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
    • F16B37/048—Non-releasable devices
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S411/00—Expanded, threaded, driven, headed, tool-deformed, or locked-threaded fastener
    • Y10S411/955—Locked bolthead or nut
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S411/00—Expanded, threaded, driven, headed, tool-deformed, or locked-threaded fastener
    • Y10S411/955—Locked bolthead or nut
    • Y10S411/965—Locked bolthead or nut with retainer
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/71—Rod side to plate or side
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/71—Rod side to plate or side
    • Y10T403/7129—Laterally spaced rods

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Surgical Instruments (AREA)
AT03352004T 2002-03-08 2003-03-04 Vorrichtung zum befestigen eines bauteils an einer luftfahrzeugstruktur ATE327444T1 (de)

Applications Claiming Priority (2)

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

Publications (1)

Publication Number Publication Date
ATE327444T1 true ATE327444T1 (de) 2006-06-15

Family

ID=27758819

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03352004T ATE327444T1 (de) 2002-03-08 2003-03-04 Vorrichtung zum befestigen eines bauteils an einer luftfahrzeugstruktur

Country Status (7)

Country Link
US (1) US6889939B2 (de)
EP (1) EP1342927B1 (de)
AT (1) ATE327444T1 (de)
BR (1) BR0300431B1 (de)
CA (1) CA2420352C (de)
DE (1) DE60305360T2 (de)
FR (1) FR2836963A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7265378B2 (en) 2002-07-10 2007-09-04 E. I. Du Pont De Nemours And Company Electronic devices made with electron transport and/or anti-quenching layers
US20060182513A1 (en) * 2005-02-15 2006-08-17 Dortch John P Fastener and method for using same
FR2883548B1 (fr) * 2005-03-23 2007-06-15 Airbus France Sas Dispositif et procede d'eclissage mixte carbone-metal dissymetrique
US20120017736A1 (en) * 2005-11-22 2012-01-26 Robert Bosch Tool Corporation Power cord routing system for miter saw with hinge linkage linear guide
US8631734B2 (en) 2005-11-22 2014-01-21 Robert Bosch Gmbh Glide movement controller and power miter saw including such controller
US8857303B2 (en) 2005-11-22 2014-10-14 Robert Bosch Gmbh Locking mechanism for miter saw with hinge linkage linear guide
FR2894225B1 (fr) * 2005-12-07 2008-01-11 Airbus France Sa Sa Mur de cloisonnement pour carenage ventral d'aeronef et aeronef muni d'un carenage ventral
GB0526084D0 (en) * 2005-12-21 2006-02-01 Airbus Uk Ltd An aircraft structure and a fastener for use therewith
ES2317762B1 (es) * 2006-10-31 2010-02-10 Airbus España, S.L. Carena ventral para un avion.
DE102007011621B4 (de) 2007-01-22 2010-10-07 Airbus Deutschland Gmbh Vorrichtung, insbesondere Samerstange, zur Aussteifung einer Rumpfzellenstruktur eines Luftfahrzeugs und/oder zur Befestigung eines Bauteils
US7637686B2 (en) * 2007-03-02 2009-12-29 The Boeing Company Swivel fitting attachment apparatus
US20090003970A1 (en) * 2007-06-29 2009-01-01 Illinois Tool Works Inc. Threaded anchor having a head portion comprising a hexagonally configured drive section, and an integral projection having a transverse bore formed therein
US20090016843A1 (en) * 2007-07-13 2009-01-15 Igor Komsitsky Spacer Assemblies, Apparatus and Methods of Supporting Hardware
US7997530B2 (en) * 2008-06-12 2011-08-16 The Boeing Company Airplane fairing panel adjustable fitting assembly, kit and method
ES2399262B1 (es) * 2010-12-31 2014-04-29 Airbus Operations, S.L. Herraje regulable para la instalación y ajuste de carenas en aeronaves.
US8727686B2 (en) * 2012-03-23 2014-05-20 B/E Aerospace, Inc. Device for attaching an aircraft monument
DE102013001041B4 (de) * 2013-01-22 2025-01-30 Audi Ag Verbindungsanordnung mit einem Strukturbauteil
JP6336362B2 (ja) 2014-09-10 2018-06-06 三菱航空機株式会社 航空機
FR3031082B1 (fr) * 2014-12-30 2017-02-10 Airbus Operations Sas Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere
CA2936180C (en) 2015-07-24 2025-05-06 Pratt & Whitney Canada Corp. MULTI-RADIUS COOLING SYSTEM AND METHOD
US10443449B2 (en) 2015-07-24 2019-10-15 Pratt & Whitney Canada Corp. Spoke mounting arrangement
US10247035B2 (en) 2015-07-24 2019-04-02 Pratt & Whitney Canada Corp. Spoke locking architecture
US10655663B2 (en) * 2017-09-29 2020-05-19 Lockheed Martin Corporation Apparatus, system, and method for aligning apertures of structures

Family Cites Families (4)

* 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
US4627590A (en) * 1984-12-03 1986-12-09 The Boeing Company Stowage receiver for fixed length rod
US5542777A (en) * 1994-07-12 1996-08-06 Martin Marietta Corporation Fastener for composite structures
PL188790B1 (pl) * 1998-03-19 2005-04-29 Andrzej Czechowski Sposób łączenia elementów metalowych za pomocą łącznika śrubowego

Also Published As

Publication number Publication date
US20030168554A1 (en) 2003-09-11
DE60305360T2 (de) 2007-04-12
FR2836963A1 (fr) 2003-09-12
CA2420352C (fr) 2011-02-01
BR0300431B1 (pt) 2011-12-27
EP1342927B1 (de) 2006-05-24
DE60305360D1 (de) 2006-06-29
US6889939B2 (en) 2005-05-10
EP1342927A1 (de) 2003-09-10
BR0300431A (pt) 2004-08-17
CA2420352A1 (fr) 2003-09-08

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