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. 17, 2020

Filed:

Aug. 22, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kenneth Arthur Gould, Winchester, MA (US);

Martin Miles D'Angelo, Boston, MA (US);

Daniel Waslo, Marblehead, MA (US);

Brian Lewis Devendorf, Georgetown, MA (US);

Mark Gregory Wotzak, Chestnut Hill, MA (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); F02C 7/20 (2006.01); F01D 25/24 (2006.01); F02C 3/10 (2006.01); F02C 3/14 (2006.01); F02C 6/20 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); F01D 25/24 (2013.01); F01D 25/28 (2013.01); F02C 3/103 (2013.01); F02C 3/145 (2013.01); F02C 6/206 (2013.01); F02C 7/20 (2013.01); B64D 2027/262 (2013.01); B64D 2027/268 (2013.01); F05D 2220/324 (2013.01); F05D 2230/53 (2013.01); F05D 2240/90 (2013.01);
Abstract

An apparatus and method for mounting a turbine engine to an aircraft can include an engine core for the turbine engine including a compressor section, a combustor section, and a turbine section in flow arrangement. At least one strut couples to the engine core about a single mount plane. A structural wall at least partially defining a mainstream flow path couples to the at least one strut and passes through the compressor section and the turbine section.


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