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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.

Patent No.:

US 12421916 B1

PDFFull Text
Date of Patent:
Sep. 23, 2025

Filed:

Nov. 05, 2024

Engine mount system for a gas turbine engine

Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Gabriel L. Suciu, Glastonbury, CT (US);

Brian D. Merry, Andover, CT (US);

Christopher M. Dye, San Diego, CA (US);

Steven B. Johnson, Marlborough, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Alain Chau

Int. Cl.
CPC ...
F02K 3/06 (2006.01); B64D 27/40 (2024.01); F01D 5/06 (2006.01); F01D 9/02 (2006.01); F01D 15/12 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01); F02C 3/107 (2006.01); F02C 7/20 (2006.01); F02C 7/36 (2006.01); F02C 9/18 (2006.01); F02C 9/20 (2006.01); F02K 1/15 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); B64D 27/402 (2024.01); B64D 27/404 (2024.01); B64D 27/406 (2024.01); F01D 5/06 (2013.01); F01D 9/02 (2013.01); F01D 15/12 (2013.01); F01D 25/24 (2013.01); F01D 25/28 (2013.01); F02C 3/107 (2013.01); F02C 7/20 (2013.01); F02C 7/36 (2013.01); F02C 9/18 (2013.01); F02C 9/20 (2013.01); F02K 1/15 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/40311 (2013.01); F05D 2270/42 (2013.01);
Abstract

A gas turbine engine includes, among other things, a propulsor section including a rotor and blades, a geared architecture including a gear train, a compressor section and a turbine section. A static structure includes a first case and a second case. The first case includes a first engine mount location. The second case includes a second engine mount location. The first engine mount location is axially near the geared architecture.

Find Patent Forward Citations

Suciu, Gabriel. (2025). Engine mount system for a gas turbine engine (U.S. Patent No. 12421916). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12421916

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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