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. 11, 2019

Filed:

Nov. 16, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:
Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/04 (2006.01); B64D 27/10 (2006.01); B64D 33/02 (2006.01); F02C 7/045 (2006.01); F02C 7/047 (2006.01); F02K 3/072 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); B64D 27/10 (2013.01); B64D 33/02 (2013.01); F02C 7/045 (2013.01); F02C 7/047 (2013.01); F02K 3/072 (2013.01); B64D 2033/0226 (2013.01); B64D 2033/0293 (2013.01); F05D 2220/323 (2013.01); F05D 2270/17 (2013.01);
Abstract

Air intake duct for supplying air to a turbine engine gas generator, in particular an aircraft turbine engine, extending axially between the air intake and the gas generator and having a deflection which may cause shedding of the boundary layer formed by the air flow along the wall of the duct, wherein said air intake duct comprises a guiding element located in the duct and designed to guide the air along the wall of the duct to a portion having the deflection, said guiding element extending transversely to the direction of the flow of air and having at the ends thereof two end profiles that form a non-zero angle with the guiding element, said two end profiles being able to produce eddies in the air flow.


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