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:
Oct. 19, 2021

Filed:

Aug. 25, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventor:

Mark R. Alber, Milford, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/08 (2006.01); B64C 27/14 (2006.01); B64D 35/04 (2006.01); B64C 27/82 (2006.01); B64D 35/02 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B64C 27/14 (2013.01); B64C 27/82 (2013.01); B64D 35/02 (2013.01); B64D 35/04 (2013.01); F02C 6/20 (2013.01); B64C 2027/8236 (2013.01); F05D 2220/329 (2013.01);
Abstract

A drive system for a rotorcraft includes at least one engine, the engine including a compressor section, and a turbine section positioned rearward from the compressor section. A main rotor input shaft extends from a rotor power turbine of the turbine section and is connectable to a main rotor assembly of the rotorcraft to transfer rotational energy from the rotor power turbine to the main rotor assembly. An auxiliary input shaft extends from an auxiliary power turbine of the turbine section and is connectible to an auxiliary rotor assembly of the rotorcraft to transfer rotational energy from the auxiliary power turbine to the auxiliary rotor assembly.


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