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. 23, 2020

Filed:

Jan. 05, 2017
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Tibor Urac, Mississauga, CA;

Peter Townsend, Mississauga, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/54 (2006.01); F02C 7/04 (2006.01); F01D 5/14 (2006.01); F04D 27/00 (2006.01); F01D 21/00 (2006.01);
U.S. Cl.
CPC ...
F04D 29/541 (2013.01); F01D 5/143 (2013.01); F01D 5/146 (2013.01); F02C 7/04 (2013.01); F01D 5/141 (2013.01); F01D 5/142 (2013.01); F01D 5/145 (2013.01); F01D 21/003 (2013.01); F04D 27/001 (2013.01); F04D 29/542 (2013.01); F04D 29/544 (2013.01); F05D 2220/36 (2013.01); F05D 2240/122 (2013.01); F05D 2240/127 (2013.01); F05D 2250/182 (2013.01); F05D 2250/184 (2013.01); F05D 2260/83 (2013.01); F05D 2270/80 (2013.01);
Abstract

A turbofan engine is disclosed which includes a nacelle assembly, having an interior surface for directing airflow, and a flow disruptor positioned on the interior surface upstream of the fan, the flow disruptor extending towards the axis a height greater than the anticipated boundary layer height of the airflow. A turbofan engine which includes an array of circumferentially disposed flow disruptors extending from a fan case inner surface is also disclosed. A method of mitigating fan flutter in a gas turbine engine by generating a circumferential asymmetrically in the airflow, upstream of the fan, is also described.


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