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:
Mar. 21, 2023

Filed:

Feb. 13, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Hung Duong, Unionville, CT (US);

Marc J. Muldoon, Marlborough, CT (US);

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

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F02C 7/36 (2006.01); F02C 3/113 (2006.01); F02K 3/06 (2006.01); F02C 6/08 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F02C 3/113 (2013.01); F02C 6/08 (2013.01); F02C 7/185 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F05D 2220/76 (2013.01); F05D 2260/211 (2013.01); F05D 2260/213 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/532 (2013.01);
Abstract

A gas turbine engine has a low speed input shaft drives a first plurality of accessories. A high speed input shaft drives a second plurality of accessories. The first plurality of accessories rotating about a first set of rotational axes perpendicular to a first plane. The second plurality of accessories rotating about a second set rotational axes perpendicular to a second plane. The first and second planes extending in opposed directions away from a drive input axis. Compressed air is tapped and passes through a heat exchanger, then to a boost compressor, and then to at least one rotatable components in a main compressor section and a main turbine section. The boost compressor driven on a boost axis, which is non-parallel to the first set of rotational axes and the second set of rotational axes.


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