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:
Jul. 18, 2017

Filed:

Dec. 20, 2013
Applicant:

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

Inventors:

Thierry Surply, Cornebarrieu, FR;

Cyril Bonnaud, Toulouse, FR;

David Grossein, Toulouse, FR;

Stéve Bedoin, Toulouse, FR;

Amadou AndréSylla, Toulouse, FR;

Guillaume Drochon, Toulouse, FR;

Marjorie Clottes, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64C 7/02 (2006.01); B64D 29/02 (2006.01); B64D 33/04 (2006.01); F01D 25/14 (2006.01); F02C 7/12 (2006.01); F02K 1/82 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64C 7/02 (2013.01); B64D 29/02 (2013.01); B64D 33/04 (2013.01); F01D 25/14 (2013.01); F02C 7/12 (2013.01); B64D 2027/268 (2013.01); F05D 2220/327 (2013.01); F05D 2260/202 (2013.01); Y02T 50/675 (2013.01);
Abstract

The invention proposes to protect a rear part of a floor of an aft fairing of a pylon of an aircraft bypass turbojet engine using a film of cool air formed of part of a bypass flow of the jet engine which is guided under the floor by two lateral wall portions of this fairing which have been profiled for this purpose. To do that, these two lateral wall portions delimit respective air passage spaces formed between a forward part of the floor and a jetpipe of the turbojet engine and which open laterally and towards the rear.


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