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. 17, 2020

Filed:

Jan. 19, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

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

Hung Duong, Unionville, CT (US);

Jonathan F. Zimmitti, Glastonbury, CT (US);

William G. Sheridan, Southington, CT (US);

Michael E. McCune, Colchester, CT (US);

Brian Merry, Andover, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F02C 7/277 (2006.01); F02C 7/22 (2006.01); F01D 15/10 (2006.01); F01D 15/08 (2006.01); F01D 15/12 (2006.01); F01D 5/06 (2006.01); F01D 25/20 (2006.01); F01D 25/16 (2006.01); F02C 7/36 (2006.01); F01D 5/02 (2006.01); F02C 7/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 5/026 (2013.01); F01D 5/06 (2013.01); F01D 15/08 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 25/16 (2013.01); F01D 25/20 (2013.01); F02C 7/06 (2013.01); F02C 7/22 (2013.01); F02C 7/277 (2013.01); F02C 7/36 (2013.01); F05D 2220/32 (2013.01); F05D 2220/50 (2013.01); F05D 2240/60 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A gas turbine engine assembly includes a turbine section having first and second turbines mounted for rotation about a common rotational axis within an engine static structure, first and second turbine shafts coaxial with one another and to which the first and second turbines are respectively operatively mounted, first and second towershafts respectively coupled to the first and second turbine shafts, an accessory drive gearbox mounted to the engine static structure, a hydraulic pump, and a transmission. The transmission is transitionable between a first mode where the hydraulic pump is driven at a first speed relative to a first towershaft, a second mode where the hydraulic pump is driven at a different, second speed relative to the first towershaft, and a third mode where the hydraulic pump is driven at a different, third speed relative to the first towershaft.


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