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:
Nov. 05, 2019

Filed:

Oct. 02, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Darek Tomasz Zatorski, Fort Wright, KY (US);

Patrick John Lonneman, Erlanger, KY (US);

Alan Roy Stuart, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/66 (2006.01); F01D 7/00 (2006.01); F01D 25/06 (2006.01); F02K 1/12 (2006.01); F02K 1/30 (2006.01); F02K 1/32 (2006.01); F02K 1/70 (2006.01);
U.S. Cl.
CPC ...
F01D 7/00 (2013.01); F01D 25/06 (2013.01); F02K 1/12 (2013.01); F02K 1/30 (2013.01); F02K 1/32 (2013.01); F02K 1/66 (2013.01); F02K 1/70 (2013.01); Y02T 50/673 (2013.01);
Abstract

A gas turbine engine having a forward thrust mode and a reverse thrust mode is provided. The gas turbine engine includes a variable pitch fan configured for generating forward thrust in the forward thrust mode of the engine and reverse thrust in the reverse thrust mode of the engine. The engine also includes a fan cowl surrounding the variable pitch fan, wherein the fan cowl forms a bypass duct for airflow generated by the fan. The fan cowl includes an aft edge that defines a physical flow area of the bypass duct, and a deflection device configured for deflecting airflow near the aft edge, wherein the deflection device is configured for operation in the reverse thrust mode of the engine. The physical flow area of the bypass duct at the aft edge remains the same in the forward thrust mode of the engine and in the reverse thrust mode of the engine.


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