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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 11286883 B1

PDFFull Text
Date of Patent:
Mar. 29, 2022

Filed:

May. 07, 2019

Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

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:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Alain Chau

Int. Cl.
CPC ...
F02K 3/06 (2006.01); B64D 27/26 (2006.01); F02C 7/36 (2006.01); F02C 3/107 (2006.01); F01D 5/06 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01); F02C 7/20 (2006.01); F02K 1/15 (2006.01); F02C 9/20 (2006.01); F02C 9/18 (2006.01); F01D 9/02 (2006.01); F01D 15/12 (2006.01); F01D 1/12 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); 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); 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 fan section including a fan rotor, a gear train defined about an engine axis of rotation, a high spool, and a low spool including a low pressure turbine that drives the fan rotor through the gear train. A static structure includes a first engine mount location and a second engine mount location.

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Quick Actions:

Suciu, Gabriel. (2022). Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement (U.S. Patent No. 11286883). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11286883

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

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