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:
Oct. 06, 2020

Filed:

May. 08, 2018
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Guo Rong Yan, Montreal, CA;

Mark Huzzard Cunningham, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/04 (2006.01); B64D 33/02 (2006.01); B64D 27/10 (2006.01); F02C 7/052 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); B64D 27/10 (2013.01); B64D 33/02 (2013.01); F02C 7/052 (2013.01); B64D 2033/0293 (2013.01); F05D 2220/323 (2013.01); F05D 2220/324 (2013.01); F05D 2250/51 (2013.01);
Abstract

An aircraft intake duct for channeling a flow of ambient air toward an annular engine compressor inlet of a gas turbine engine having a compressor reference axis and a reference plane that extends from such compressor reference axis. The aircraft intake duct includes an oblong air intake inlet for receiving the flow of ambient air, the air intake inlet being offset radially outwardly relative to the compressor reference axis and located on a first side of the reference plane. Two distal intake channels fluidly link distal extremities of the oblong air intake inlet to a segment of the annular engine compressor inlet located on a second side of the reference plane. A central channel fluidly links a central section of the oblong air intake inlet to a segment of the annular engine compressor inlet located on a first side of the reference plane. The distal channels are blended together by the central channel so that a single intake duct is formed.


Find Patent Forward Citations

Yan, Guo. (2020). Air intake for gas turbine engine (U.S. Patent No. 10794280). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10794280

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

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