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. 26, 2019

Filed:

Sep. 26, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nikolai N. Pastouchenko, Glenville, NY (US);

Ivan Malcevic, Niskayuna, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 5/06 (2006.01); B64C 5/02 (2006.01); B64C 21/06 (2006.01); B64C 1/16 (2006.01); B64D 27/18 (2006.01); B64D 29/04 (2006.01); B64D 27/20 (2006.01);
U.S. Cl.
CPC ...
B64C 21/06 (2013.01); B64C 1/16 (2013.01); B64C 5/02 (2013.01); B64C 5/06 (2013.01); B64D 27/18 (2013.01); B64D 27/20 (2013.01); B64D 29/04 (2013.01); B64C 2230/04 (2013.01); Y02T 50/166 (2013.01);
Abstract

An aircraft is provided including a boundary layer ingestion fan mounted to an aft end of a fuselage. A stabilizer is mounted to the fuselage and extends between a root portion and a tip portion to define a span-wise length and extends between a leading edge and a trailing edge along the longitudinal direction. The stabilizer defines a line of maximum thickness that corresponds to the thickest cross sectional portion of the stabilizer along the span-wise length of the stabilizer. The line of maximum thickness is closer to the leading edge of the stabilizer proximate the root portion than at the tip portion, resulting in a pressure distribution that draws higher velocity air away from an inlet of the boundary layer ingestion fan.


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