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:
Sep. 10, 2024

Filed:

Nov. 07, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Karl L. Hasel, Manchester, CT (US);

Joseph B. Staubach, Colchester, CT (US);

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

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

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

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F02C 3/04 (2006.01); F02C 3/06 (2006.01); F02C 3/107 (2006.01); F02K 3/02 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F02C 3/04 (2013.01); F02C 3/06 (2013.01); F02C 3/107 (2013.01); F02K 3/025 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2220/323 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A gas turbine engine includes, among other things, a propulsor section including a propulsor, a core engine, a gear arrangement that drives the propulsor. A compressor section includes a first compressor section and a second compressor section. A turbine section includes a first turbine and a second turbine. An overall pressure ratio is provided by the combination of a pressure ratio across the first compressor section and a pressure ratio across the second compressor section, and greater than 40. The pressure ratio across the second compressor section is between 7 and 15, and the pressure ratio across the first compressor section is between 4 and 8.


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