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. 24, 2018

Filed:

Feb. 24, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Eugene Gekht, Brossard, CA;

Francois Bisson, Vallee-Jonction, CA;

Mark Cunningham, Montreal, CA;

Michel Desjardins, St-Hubert, CA;

Guo Rong Yan, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/042 (2006.01); B64D 33/02 (2006.01); F02C 7/04 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
F02C 7/042 (2013.01); B64D 33/02 (2013.01); F02C 6/206 (2013.01); F02C 7/04 (2013.01); B64D 2033/0246 (2013.01); B64D 2033/0293 (2013.01); F05D 2250/51 (2013.01); Y02T 50/671 (2013.01);
Abstract

An air intake for efficiently channeling a flow of ambient air toward an air inlet of a turboprop or turboshaft gas turbine engine is disclosed. The air intake comprises an intake inlet for receiving the flow of air, an intake duct for channelling the flow of air, and an intake outlet for discharging the flow of air toward the air inlet of the gas turbine engine. The air intake may comprise a scroll portion and a strutted portion configured to receive the flow of air from the intake duct and channel the flow of air toward the intake outlet. The strutted portion may comprise one or more vanes for interacting with the flow of air. The intake duct may be oriented toward a flow direction of the air pushed aft by a propeller coupled to the gas turbine engine.


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