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:
Mar. 02, 2021

Filed:

Sep. 25, 2018
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Bernd Ehlers, Hamburg, DE;

Stefan Behrens, Achim, DE;

Mark Herzog, Hamburg, DE;

Alexander Schulz, Hamburg, DE;

Max Strieth-Kalthoff, Hamburg, DE;

Hans-Gerhard Giesa, Hamburg, DE;

Soenke Jacobsen, Hamburg, DE;

Joerg Weifenbach, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 11/06 (2006.01); B60N 2/02 (2006.01); B60N 2/75 (2018.01); B61D 33/00 (2006.01); B60N 2/68 (2006.01);
U.S. Cl.
CPC ...
B64D 11/064 (2014.12); B60N 2/0292 (2013.01); B60N 2/682 (2013.01); B60N 2/77 (2018.02); B61D 33/0078 (2013.01); B61D 33/0085 (2013.01); B64D 11/0601 (2014.12); B64D 11/0602 (2014.12); B64D 11/0639 (2014.12); B60N 2002/684 (2013.01); B64D 11/0605 (2014.12); B64D 11/0648 (2014.12);
Abstract

A passenger seat arrangement for installation in an aircraft comprises a seat unit with a backrest element and a seat element. The seat arrangement also comprises a supporting frame carrying the seat unit and comprising at least one seat mounting, which has a first backrest holder, to which the backrest element can be releasably fixed in a load-transferring manner in a first position on the seat mounting, and a second backrest holder, to which the backrest element can be releasably fixed in a load-transferring manner in a second position on the seat mounting. When the passenger seat arrangement is installed in the aircraft, the backrest element is pivoted in relation to a longitudinal axis of the aircraft in a state in which it is fixed to the first backrest holder relative to a state in which it is fixed to the second backrest holder.


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