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. 01, 2022

Filed:

Feb. 19, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Lawrence Chih-Hui Cheung, Niskayuna, NY (US);

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

Kishore Ramakrishnan, Rexford, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/08 (2006.01); B64C 21/06 (2006.01); B64D 29/04 (2006.01); B64C 1/16 (2006.01); B64D 27/24 (2006.01); B64D 33/02 (2006.01); B64D 33/04 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 21/08 (2013.01); B64C 1/16 (2013.01); B64C 21/06 (2013.01); B64D 27/24 (2013.01); B64D 29/04 (2013.01); B64D 33/02 (2013.01); B64D 33/04 (2013.01); B64D 2027/026 (2013.01); B64D 2033/0226 (2013.01); Y02T 50/10 (2013.01); Y02T 50/60 (2013.01);
Abstract

An aircraft includes a fuselage extending between a forward end and an aft end; a propulsor mounted to the fuselage at the aft end of the fuselage, the propulsor comprising an outer nacelle, the outer nacelle defining an inlet to the propulsor; and a deployable assembly attached to at least one of the fuselage or the outer nacelle and moveable between a stowed position and an engaged position. The deployable assembly alters an airflow towards the propulsor or into the propulsor through the inlet defined by the outer nacelle when in the engaged position. The propulsor further comprises a tail cone, wherein the outer nacelle defines an exhaust with the tail cone, and wherein the plurality of nacelle panels are movable generally along the axial centerline to a position at least partially aft of the exhaust of the outer nacelle when in the engaged position.


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