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. 20, 2022

Filed:

Aug. 21, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel Bernard Kupratis, Wallingford, CT (US);

Mark Tu, East Hampton, CT (US);

Paul R Hanrahan, Farmington, CT (US);

Arthur M. Salve, Jr., Tolland, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/113 (2006.01); F02C 3/14 (2006.01); F02C 9/56 (2006.01); F02K 3/10 (2006.01); F02C 9/00 (2006.01);
U.S. Cl.
CPC ...
F02C 3/113 (2013.01); F02C 3/14 (2013.01); F02C 9/56 (2013.01); F02K 3/10 (2013.01); F02C 9/00 (2013.01); F05D 2220/32 (2013.01);
Abstract

A gas turbine engine is disclosed. In various embodiments, the gas turbine engine includes a high pressure turbine having a first stage and a second stage, the first stage connected to a high pressure turbine first stage spool and the second stage connected to a high pressure turbine second stage spool; a high pressure compressor connected to a high pressure compressor spool; and a differential system having a first stage input gear connected to the high pressure turbine first stage spool, a second stage input gear connected to the high pressure turbine second stage spool and an output gear connected to the high pressure compressor spool.


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