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:
Oct. 10, 2023

Filed:

Jan. 20, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Glenn Levasseur, Colchester, CT (US);

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

Gary M. Stetson, Tolland, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F02C 3/06 (2006.01); F02C 7/32 (2006.01); F01D 17/16 (2006.01); F02C 9/20 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F01D 17/162 (2013.01); F02C 3/064 (2013.01); F02C 7/32 (2013.01); F02C 9/20 (2013.01); F05D 2220/32 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A gas turbine engine includes a propulsor having a plurality of blades, a compressor section including a first compressor and a second compressor aft of the first compressor. The first compressor includes at least one array of first variable guide vanes that control operation of the first compressor. The second compressor includes at least one array of second variable guide vanes that control operation of the second compressor. A turbine section includes a first turbine and a second turbine. A geared architecture is driven by the second turbine for rotating the propulsor.


Find Patent Forward Citations

Loading…