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:
Jan. 24, 2023

Filed:

Oct. 16, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Timothy Leo Schelfaut, Lebanon, OH (US);

Anthony M. Metz, Harrison, OH (US);

Michael A. Riehle, West Chester, OH (US);

Jonathan E. Coleman, Mason, OH (US);

Illya Emmanuel Arcos Perez, Mason, OH (US);

Brian Michael Dixon, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F16F 15/023 (2006.01); F16F 15/027 (2006.01); F16F 15/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/00 (2013.01); F05D 2220/323 (2013.01); F05D 2260/96 (2013.01); F16F 15/023 (2013.01); F16F 15/0237 (2013.01); F16F 15/0275 (2013.01); F16F 15/06 (2013.01); F16F 2222/12 (2013.01); F16F 2228/066 (2013.01); F16F 2230/18 (2013.01);
Abstract

Damper engine mount links are disclosed. An example engine assembly includes a core including a fore portion and an aft portion, the fore portion of the core to couple to a fan hub frame, the aft portion of the core to couple to a turbine rear frame or a turbine center frame. The engine assembly further includes a forward mount to couple the fan hub frame to an aircraft, and a damper link to couple the turbine rear frame or the turbine center frame to an aircraft mount.


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