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. 06, 2020

Filed:

Jul. 01, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Jeffery F. Perlak, South Windsor, CT (US);

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

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

James D. Hill, Tolland, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 3/107 (2006.01); F02C 3/14 (2006.01); F02C 3/10 (2006.01);
U.S. Cl.
CPC ...
F02C 3/107 (2013.01); F02C 3/10 (2013.01); F02C 3/145 (2013.01); F05D 2210/44 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A gas turbine engine according to the present disclosure includes a first compressor and a first turbine for driving the first compressor. A core section includes a second compressor and a second turbine for driving the second compressor. A third turbine is arranged fluidly downstream of the first turbine and the second turbine and configured to drive a power take-off. A first duct system is arranged fluidly between the low-pressure compressor and the core section. The first duct system is arranged to reverse fluid flow before entry into the core section.


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