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:
Jun. 30, 2020

Filed:

Dec. 21, 2015
Applicant:

Airbus Operations S.l., Getafe, ES;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 5/02 (2006.01); B64C 1/26 (2006.01); B64C 1/06 (2006.01); B64C 1/12 (2006.01); B64C 1/14 (2006.01); B64C 1/16 (2006.01); B64C 7/00 (2006.01); B64D 41/00 (2006.01); B64D 29/04 (2006.01); B64D 29/08 (2006.01); B64C 1/10 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 5/02 (2013.01); B64C 1/061 (2013.01); B64C 1/12 (2013.01); B64C 1/1446 (2013.01); B64C 1/16 (2013.01); B64C 1/26 (2013.01); B64C 7/00 (2013.01); B64C 1/10 (2013.01); B64C 2001/0072 (2013.01); B64D 29/04 (2013.01); B64D 29/08 (2013.01); B64D 2041/002 (2013.01);
Abstract

A fuselage rear end of an aircraft, comprising a structural part comprising a skin and longitudinal and transversal reinforcing members and a fairing. The structural part longitudinally spans over the whole rear end and comprises a first portion in which the transversal reinforcing members occupy the whole perimeter of the corresponding fuselage section and at least a second portion in which the transversal reinforcing members occupy only a portion of the perimeter of the corresponding fuselage section. The fairing is located below the second portion of the structural part.


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