FR3017668A1 - - Google Patents

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Publication number
FR3017668A1
FR3017668A1 FR1551401A FR1551401A FR3017668A1 FR 3017668 A1 FR3017668 A1 FR 3017668A1 FR 1551401 A FR1551401 A FR 1551401A FR 1551401 A FR1551401 A FR 1551401A FR 3017668 A1 FR3017668 A1 FR 3017668A1
Authority
FR
France
Prior art keywords
fairing
carrier structure
flow
composite material
body component
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.)
Granted
Application number
FR1551401A
Other languages
English (en)
French (fr)
Other versions
FR3017668B1 (fr
Inventor
olaf Steffen
Christian Uckert
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of FR3017668A1 publication Critical patent/FR3017668A1/fr
Application granted granted Critical
Publication of FR3017668B1 publication Critical patent/FR3017668B1/fr
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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • 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
    • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04—Rivets; Spigots or the like fastened by riveting
    • F16B19/05—Bolts fastening by swaged-on collars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
FR1551401A 2014-02-19 2015-02-19 Procede et agencement d'assemblage pour relier un constituant de corps d'ecoulement avec un ou plusieurs composants Expired - Fee Related FR3017668B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014102117.7A DE102014102117B4 (de) 2014-02-19 2014-02-19 Verfahren und Verbindungsanordnung zum Verbinden eines Strömungskörper-Bauelementes mit einem oder mehreren Bauteilen
DE102014102117.7 2014-02-19

Publications (2)

Publication Number Publication Date
FR3017668A1 true FR3017668A1 (https=) 2015-08-21
FR3017668B1 FR3017668B1 (fr) 2019-10-18

Family

ID=53758765

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1551401A Expired - Fee Related FR3017668B1 (fr) 2014-02-19 2015-02-19 Procede et agencement d'assemblage pour relier un constituant de corps d'ecoulement avec un ou plusieurs composants

Country Status (2)

Country Link
DE (1) DE102014102117B4 (https=)
FR (1) FR3017668B1 (https=)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3243743A1 (en) * 2016-05-11 2017-11-15 Airbus Operations Limited Aircraft joint
CN110015401A (zh) * 2017-12-13 2019-07-16 空中客车营运有限公司 零件套件、翼型结构和用于组装翼型结构的方法

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3521162B1 (en) 2018-02-02 2022-06-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A helicopter with a fuselage and a tail boom which are connected via a shear connection
DE102021105806B4 (de) 2021-03-10 2024-04-11 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerodynamischer Profilkörper für Luftfahrzeuge
DE102023102200B3 (de) 2023-01-31 2024-02-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerodynamischer Profilkörper für Luftfahrzeuge

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20010048048A1 (en) * 1999-01-13 2001-12-06 Brian L Riedel Backside fitting attachment for nacelle acoustic panels
FR2905739B1 (fr) * 2006-09-08 2008-11-07 Airbus France Sas Assemblage de panneaux et procede de montage d'un assemblage de panneaux
GB0805963D0 (en) * 2008-04-02 2008-05-07 Airbus Uk Ltd Aircraft structure
DK2368699T3 (en) * 2010-03-22 2019-01-14 Vestas Wind Sys As Process for manufacturing a wing bar for a wind turbine
DE102011107624A1 (de) 2011-06-30 2013-01-03 Eads Deutschland Gmbh Verbindungsanordnung zur aerodynamisch glatten Verbindung zweier Profilelemente, Verfahren zu deren Fertigung und Vorrichtung zur Durchführung des Verfahrens

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3243743A1 (en) * 2016-05-11 2017-11-15 Airbus Operations Limited Aircraft joint
US10472044B2 (en) 2016-05-11 2019-11-12 Airbus Operations Limited Aircraft joint
CN110015401A (zh) * 2017-12-13 2019-07-16 空中客车营运有限公司 零件套件、翼型结构和用于组装翼型结构的方法

Also Published As

Publication number Publication date
DE102014102117A1 (de) 2015-08-20
DE102014102117B4 (de) 2015-10-01
FR3017668B1 (fr) 2019-10-18

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