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:
Nov. 05, 2019

Filed:

Mar. 14, 2017
Applicant:

Airbus Operations (S.a.s.), Toulouse, FR;

Inventors:

Olivier Pautis, Merville, FR;

Wolfgang Brochard, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/18 (2006.01); B64D 27/26 (2006.01); B64D 29/06 (2006.01);
U.S. Cl.
CPC ...
B64D 27/18 (2013.01); B64D 27/26 (2013.01); B64D 29/06 (2013.01); B64D 2027/264 (2013.01); B64D 2027/266 (2013.01); Y02T 50/44 (2013.01);
Abstract

To reduce flexural deformations of an engine, an engine assembly comprises a device for attaching the engine onto a structure of an aircraft, the attachment device including a primary structure, an attachment device for attaching the engine onto the primary structure of the attachment pylon, and a nacelle including thrust reversal cowls, each equipped with an inner structure arranged around a case portion of the engine. The assembly includes flexible devices for transmitting forces, arranged between the case portion and the inner structures of the cowls, each device including an elastically deformable device configured so that in the closed position of the cowl, with the engine at a standstill, it adopts a partial elastic deformation state allowing the device to apply a prestress force on the case portion.


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