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:
Aug. 08, 2017

Filed:

Jan. 07, 2013
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Sebastian Umlauft, Hamburg, DE;

Dirk Humfeldt, Hamburg, DE;

Thomas Helck, Hamburg, DE;

Mathias Schwenger, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 11/00 (2006.01); B64D 47/00 (2006.01); B64C 1/06 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B64D 47/00 (2013.01); B64C 1/066 (2013.01); B64D 11/003 (2013.01); B64F 5/10 (2017.01); B64D 2011/0046 (2013.01); Y10T 29/49826 (2015.01); Y10T 29/53961 (2015.01);
Abstract

An interior component carrier system for use in assembly of aircraft interior components in an aircraft includes a retaining system with at least one retaining element. A first connection device for connecting the retaining element to a first aircraft interior component and a second connection device are provided on the retaining element. On the retaining element a structural retainer is provided for fastening the retaining element to an aircraft structure. The interior component carrier system includes a hinge connectable to a second and a third aircraft interior component such that the third aircraft interior component is pivotable about a longitudinal axis of the hinge relative to the second aircraft interior component. The second connection device mounted on the retaining element is configured to be connected to the hinge and/or to a region of the second or third aircraft interior component, that is adjacent to the hinge.


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