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. 12, 2021

Filed:

Aug. 01, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Paul R. Hanrahan, Farmington, CT (US);

Daniel Bernard Kupratis, Wallingford, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02K 3/077 (2006.01); F02C 7/36 (2006.01); F02K 3/06 (2006.01); F02C 3/13 (2006.01); F02K 3/12 (2006.01);
U.S. Cl.
CPC ...
F02K 3/077 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F02C 3/13 (2013.01); F02C 6/08 (2013.01); F02K 3/12 (2013.01); F05D 2260/4023 (2013.01);
Abstract

A gas turbine engine includes a first spool, a second spool, a primary combustor, and a diffuser. The first spool includes a first compressor rotationally driven by a first turbine via a first shaft. The second spool includes a second compressor driven by a second turbine via a second shaft. The first compressor, the diffuser, and the primary combustor are arranged in series to provide a compressed airflow discharged from the first compressor to the primary combustor via the diffuser, which includes walls that diverge towards the primary combustor. The second compressor is fluidly coupled to the diffuser to receive at least a portion of the compressed airflow from the diffuser. The second turbine is fluidly coupled to the diffuser to discharge an expanded airflow to the diffuser.


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