The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 12, 2016

Filed:

Dec. 13, 2011
Applicant:

Frank-michael Klaukien, Ellerbek, DE;

Inventor:

Frank-Michael Klaukien, Ellerbek, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16B 17/00 (2006.01); F21V 21/08 (2006.01); B64C 1/40 (2006.01); F16B 11/00 (2006.01); B64G 1/66 (2006.01); A47G 1/17 (2006.01);
U.S. Cl.
CPC ...
F16B 17/002 (2013.01); B64C 1/406 (2013.01); F16B 11/006 (2013.01); F21V 21/0808 (2013.01); A47G 1/17 (2013.01); B64G 1/66 (2013.01); Y02T 50/46 (2013.01); Y10T 403/472 (2015.01);
Abstract

A fastening arrangement for fastening a component, in particular a cabin component, to a structural component of an aircraft or spacecraft, including a structural component which has a connection surface; a fastening fitting which has a geometry matched to the geometrical shape of the structural component, has a connection portion associated with the connection surface of the structural component and is produced from a thermoplastic injection-moulding material; and an elastomeric adhesive joint for stable fastening of the connection portion of the fastening fitting to the associated connection surface of the structural component. A corresponding fastening fitting and an aircraft or spacecraft comprising a fastening arrangement of this type and/or a fastening fitting of this type are also described.


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