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. 25, 2024

Filed:

Oct. 31, 2022
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Eray Akcayoz, Cote-Saint-Luc, CA;

Mark Cunningham, Montreal, CA;

Raja Ramamurthy, Montreal, CA;

Roberto Marrano, Boucherville, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/057 (2006.01); B64D 27/10 (2006.01); B64D 33/02 (2006.01); F02C 7/052 (2006.01);
U.S. Cl.
CPC ...
F02C 7/057 (2013.01); B64D 27/10 (2013.01); B64D 33/02 (2013.01); F02C 7/052 (2013.01);
Abstract

An air intake for an aircraft propulsion system includes an air inlet duct, a core flow duct, a bypass flow duct, and a flow control device. The air inlet duct includes an intake inlet of the air intake. The core flow duct includes a core flow outlet. The core flow duct extends between and to the air inlet duct and the core flow outlet. The bypass flow duct includes a bypass flow outlet. The bypass flow duct extends between and to the air inlet duct and the bypass flow outlet. The bypass flow duct includes an interior surface forming and surrounding a bypass flow passage through the bypass flow duct. The flow control device is disposed on the interior surface. The flow control device is configured to variably control an area of a cross-sectional flow area of the bypass flow passage.


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