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. 30, 2021

Filed:

Apr. 13, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Joseph L. Simonetti, Southbury, CT (US);

Mark D. Bystry, Jr., Stratford, CT (US);

Michael P. Strauss, New Haven, CT (US);

Michael J. DeVita, Cos Cob, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/26 (2006.01); F01D 13/00 (2006.01); F02C 6/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/26 (2013.01); F01D 13/00 (2013.01); F02C 6/02 (2013.01); F05D 2220/329 (2013.01); F05D 2260/85 (2013.01);
Abstract

A system for starting a gas turbine engine includes a rotor drive system and a hydraulic motor system operatively connected to the rotor drive system. A gas turbine engine is operatively connected to the hydraulic motor system for starting the gas turbine engine. A method for starting an engine includes initiating single-engine-operation on a multi-engine aircraft. Single-engine operation includes operating a first engine and powering down a second engine. The method includes running a hydraulic motor system. The hydraulic motor system is driven by the rotor drive system and is operatively connected to the second engine. The method includes identifying a need to start the second engine and starting the second engine using the hydraulic motor system.


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