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:
Aug. 07, 2018

Filed:

Sep. 22, 2015
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventor:

Peter James Waltner, Royal Palm Beach, FL (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64D 27/24 (2006.01); B64D 35/08 (2006.01); B60K 6/20 (2007.10); F01D 13/00 (2006.01); F01D 15/12 (2006.01); B60L 11/14 (2006.01); B60L 11/16 (2006.01); B60L 11/18 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B60K 6/20 (2013.01); B60L 11/14 (2013.01); B60L 11/16 (2013.01); B60L 11/18 (2013.01); B64D 27/24 (2013.01); B64D 35/08 (2013.01); F01D 13/00 (2013.01); F01D 15/12 (2013.01); B60L 2200/10 (2013.01); B64D 2027/026 (2013.01); F05D 2220/329 (2013.01); F05D 2260/43 (2013.01); F05D 2270/09 (2013.01);
Abstract

A hybrid power drive system for an aircraft comprises a rotor that receives power and a first power drive sub-system including at least one engine in connection with the rotor is configured to provide a first power to the rotor. Further, the hybrid power drive system also includes a second power drive sub-system connected in parallel to the first power drive sub-system. The second power drive sub-system is configured to provide a second power to the rotor a second power drive sub-system connected in parallel to the first power drive sub-system and configured to provide a second power to the rotor when the first power provided by the first power drive sub-system is less than a power demand of the rotor.


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