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. 14, 2023

Filed:

Oct. 15, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

David William Crall, Loveland, OH (US);

Nicholas Joseph Kray, Mason, OH (US);

Douglas Duane Ward, West Chester, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/30 (2006.01); F01D 5/14 (2006.01); F01D 5/18 (2006.01); F01D 7/00 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F02K 5/00 (2006.01); F02K 3/06 (2006.01); F02C 6/20 (2006.01); F02C 9/00 (2006.01); F02C 9/22 (2006.01); F02C 7/26 (2006.01); F02C 7/32 (2006.01); F02C 7/36 (2006.01); F02C 3/113 (2006.01); B32B 7/022 (2019.01); B64C 1/38 (2006.01); B64D 45/00 (2006.01); F01D 17/16 (2006.01); F01D 25/12 (2006.01); F02C 7/264 (2006.01); F02K 1/66 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B32B 7/022 (2019.01); B64C 1/38 (2013.01); F01D 5/146 (2013.01); F01D 5/187 (2013.01); F01D 5/30 (2013.01); F01D 5/3007 (2013.01); F01D 7/00 (2013.01); F01D 9/041 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 17/162 (2013.01); F01D 25/12 (2013.01); F02C 6/206 (2013.01); F02C 7/264 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/00 (2013.01); F02C 9/22 (2013.01); F02K 1/66 (2013.01); F02K 1/76 (2013.01); B32B 2307/558 (2013.01); B32B 2307/72 (2013.01); B32B 2307/732 (2013.01); B32B 2571/02 (2013.01); B32B 2605/18 (2013.01); F02C 3/113 (2013.01); F05D 2220/323 (2013.01); F05D 2220/325 (2013.01); F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01); F05D 2250/37 (2013.01); F05D 2260/201 (2013.01); F05D 2260/30 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/70 (2013.01); F05D 2270/05 (2013.01); F05D 2270/051 (2013.01); F05D 2270/121 (2013.01); F05D 2270/304 (2013.01); F05D 2270/71 (2013.01); F05D 2270/81 (2013.01);
Abstract

An aircraft defining a longitudinal direction and a lateral direction is provided. The aircraft includes: a fuselage; an engine mounted at a location spaced from the fuselage of the aircraft, the engine comprising a plurality of rotor blades; and a fuselage shield attached to or formed integrally with the fuselage at a location in alignment with the plurality of rotor blades along the lateral direction, the fuselage shield comprising a first layer defining a first density and a second layer defining a second density, the first density being different than the second density.


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