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. 02, 2022

Filed:

Sep. 28, 2017
Applicants:

Safran Electronics & Defense, Boulogne Billancourt, FR;

Safran Electrical & Power, Blagnac, FR;

Inventors:

François Guillot, Boulogne Billancourt, FR;

Jean-Marc Blineau, Blagnac, FR;

Philippe Avignon, Blagnac, FR;

Serge Roques, Blagnac, FR;

Franck Albero, Blagnac, FR;

Assignees:

SAFRAN ELECTRICAL & POWER, Blagnac, FR;

SAFRAN ELECTRONICS & DEFENSE, Boulogne Billancourt, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H05K 7/14 (2006.01); H05K 7/20 (2006.01); G06F 1/20 (2006.01); B64D 43/00 (2006.01); B64D 13/06 (2006.01); H01R 12/71 (2011.01);
U.S. Cl.
CPC ...
H05K 7/1497 (2013.01); B64D 43/00 (2013.01); G06F 1/20 (2013.01); H05K 7/1412 (2013.01); H05K 7/1487 (2013.01); H05K 7/1489 (2013.01); H05K 7/20736 (2013.01); B64D 2013/0614 (2013.01); B64D 2221/00 (2013.01); H01R 12/71 (2013.01); H01R 12/714 (2013.01);
Abstract

An aircraft comprising a fuselage () subdivided by a floor () into a top volume () and a bottom value () in which girders () extend supporting the floor and co-operating with the fuselage and the floor to define two lateral housings () that are of substantially triangular cross-section and that extend parallel to a longitudinal axis of the fuselage. Calculation units () are arranged in the lateral housings and each comprises a box () defining a main compartment containing calculation modules () insertable into the main compartment along an insertion axis through an opening in the compartment and connectable to the connectors () carried by a back wall () of the compartment so as to extend into the main compartment opposite from the opening, the insertion axis being substantially parallel to the longitudinal axis of the fuselage.


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