WO2009065379A3 - Component connection for an aircraft - Google Patents

Component connection for an aircraft Download PDF

Info

Publication number
WO2009065379A3
WO2009065379A3 PCT/DE2008/001851 DE2008001851W WO2009065379A3 WO 2009065379 A3 WO2009065379 A3 WO 2009065379A3 DE 2008001851 W DE2008001851 W DE 2008001851W WO 2009065379 A3 WO2009065379 A3 WO 2009065379A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
component
fiber composite
component connection
metal component
Prior art date
Application number
PCT/DE2008/001851
Other languages
German (de)
French (fr)
Other versions
WO2009065379A2 (en
Inventor
Erwin Bayer
Juergen Steinwandel
Original Assignee
Eads Deutschland Gmbh
Mtu Aero Engines Gmbh
Erwin Bayer
Juergen Steinwandel
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 Eads Deutschland Gmbh, Mtu Aero Engines Gmbh, Erwin Bayer, Juergen Steinwandel filed Critical Eads Deutschland Gmbh
Publication of WO2009065379A2 publication Critical patent/WO2009065379A2/en
Publication of WO2009065379A3 publication Critical patent/WO2009065379A3/en

Links

Classifications

    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/0004—Joining sheets, plates or panels in abutting relationship
    • F16B5/0056—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane
    • F16B5/0068—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane and using I-shaped clamps with flanges moving towards each other
    • F16B5/0072—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates or panels or the interlocking key perpendicular to the main plane and using I-shaped clamps with flanges moving towards each other and using screw-thread
    • 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
    • F16B2/00—Friction-grip releasable fastenings
    • F16B2/02—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening
    • F16B2/06—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action
    • F16B2/065—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening external, i.e. with contracting action using screw-thread elements
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/0004—Joining sheets, plates or panels in abutting relationship
    • F16B5/0084—Joining sheets, plates or panels in abutting relationship characterised by particular locking means
    • F16B5/0088—Joining sheets, plates or panels in abutting relationship characterised by particular locking means with locking means moving substantially perpendicular to the main plane, e.g. pins, screws

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

The invention relates to a component connection (10) for a vehicle, especially an aircraft, comprising at least one metal component (20) and a fiber composite component (30) which are connected to one another by means of a fastening device (40). The fastening device (40) encompasses a bearing element (50) and a fastening element (70) for non-positively connecting the bearing element (50) and the metal component (20) and thus the metal component (20) and the fiber composite component (30). The fiber composite component (30) has no bore that is used for connecting the metal component (20) and the fiber composite component (30). The invention further relates to a method for connecting components for a vehicle, especially an aircraft.
PCT/DE2008/001851 2007-11-21 2008-11-10 Component connection for an aircraft WO2009065379A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200710056164 DE102007056164A1 (en) 2007-11-21 2007-11-21 Component connection for aircraft
DE102007056164.6 2007-11-21

Publications (2)

Publication Number Publication Date
WO2009065379A2 WO2009065379A2 (en) 2009-05-28
WO2009065379A3 true WO2009065379A3 (en) 2009-08-06

Family

ID=40568482

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2008/001851 WO2009065379A2 (en) 2007-11-21 2008-11-10 Component connection for an aircraft

Country Status (2)

Country Link
DE (1) DE102007056164A1 (en)
WO (1) WO2009065379A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010042970A1 (en) 2010-05-12 2011-11-17 Airbus Operations Gmbh Structural component with improved conductivity and mechanical strength and method for its production

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3651887A (en) * 1970-10-19 1972-03-28 Oliver C Eckel Acoustical assembly with connectors having lips

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3651887A (en) * 1970-10-19 1972-03-28 Oliver C Eckel Acoustical assembly with connectors having lips

Also Published As

Publication number Publication date
DE102007056164A1 (en) 2009-06-04
WO2009065379A2 (en) 2009-05-28

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