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.:
Date of Patent:
Aug. 22, 2023
Filed:
Aug. 06, 2021
Applicant:
Raytheon Technologies 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:
RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); F01D 25/28 (2006.01); F02C 7/20 (2006.01); F02K 3/06 (2006.01); F02C 9/20 (2006.01); F02C 9/18 (2006.01); F02C 7/36 (2006.01); F02C 3/107 (2006.01); F01D 5/06 (2006.01); F01D 9/02 (2006.01); F01D 15/12 (2006.01); F01D 25/24 (2006.01); F02K 1/15 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); 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); F02K 3/06 (2013.01); B64D 2027/266 (2013.01); B64D 2027/268 (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, a gear train, a low spool and a high spool. A static structure includes a first case and a second case. A mount system includes a forward mount and an aft mount arranged in a plane containing an engine axis of rotation. The forward mount is secured to the first case. The aft mount is secured to the second case.