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:
Apr. 23, 2024

Filed:

Oct. 31, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Raja Ramamurthy, Montreal, CA;

Eray Akcayoz, Cote-Saint-Luc, CA;

Mark Cunningham, Montreal, CA;

Roberto Marrano, Boucherville, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/05 (2006.01); F02C 7/042 (2006.01); F02C 7/057 (2006.01); F02C 9/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/05 (2013.01); F02C 7/042 (2013.01); F02C 7/057 (2013.01); F02C 9/18 (2013.01); F05D 2220/323 (2013.01);
Abstract

An air intake for an aircraft propulsion system includes an air inlet duct, a core flow duct, a bypass flow duct, a splitter, and a flow control device. The air inlet duct includes an intake inlet and a gas path floor. The core flow duct includes a core flow outlet. The bypass flow duct includes a bypass flow outlet. The bypass flow duct includes the gas path floor. The splitter separates the core flow duct and the bypass flow duct. The flow control device is disposed on a portion of the gas path floor. The flow control device is configured to be selectively positioned to control an air flow path for air flowing through the air inlet duct, the core flow duct, and the bypass flow duct.


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