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.

Patent No.:

US 10518605 B1

PDF
Full Text
Expired
Date of Patent:
Dec. 31, 2019

Filed:

Jul. 27, 2015
Applicant:

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Nicolas Molin, Nailloux, FR;

Guillaume Clairet, Toulouse, FR;

Cedric Leconte, Toulouse, FR;

Assignee:

Airbus Operations (SAS), Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/045 (2006.01); B64D 33/02 (2006.01); B60H 1/00 (2006.01); F02K 1/82 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
B60H 1/00564 (2013.01); B64D 33/02 (2013.01); F02C 7/045 (2013.01); F02C 9/18 (2013.01); F02K 1/827 (2013.01); B64C 2230/14 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0286 (2013.01); F05D 2250/182 (2013.01); F05D 2250/191 (2013.01); Y02T 50/166 (2013.01);
Abstract

An aircraft turbomachine comprising a fan conduit with a wall, a flow of air passing through the turbomachine via the fan conduit. An air passage comprising an air opening is arranged in the wall, the air passage configured to receive a portion of the flow of the air through the fan conduit. A deflector is fixed to the wall upstream of the air opening, the deflector comprising at least one cross-section extending in the fan conduit to capture the flow of air. The at least one cross-section is porous. The deflector protects the air passage structure and is easy to produce and to fix to the wall of the fan conduit when it is screwed or riveted directly thereto. The deflector, as a result of its location in the fan conduit, is easy to access and thus allows rapid maintenance operations without having to disassemble the air passage.


Find Patent Forward Citations

Molin, Nicolas. (2019). Aircraft turbomachine comprising a deflector (U.S. Patent No. 10518605). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10518605

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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