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. 06, 2019

Filed:

Jul. 11, 2017
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Charles R. Berezin, Trumbull, CT (US);

Christopher M. Sutton, Milford, CT (US);

William A. Welsh, North Haven, CT (US);

Shyam Neerarambam, Shelton, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F28D 15/02 (2006.01); B64C 27/10 (2006.01); B64C 27/72 (2006.01); B64C 27/59 (2006.01); B64D 29/00 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F28D 15/0275 (2013.01); B64C 27/10 (2013.01); B64C 27/59 (2013.01); B64C 27/72 (2013.01); B64D 29/00 (2013.01); F28D 15/025 (2013.01); F28D 15/0266 (2013.01); B64C 2027/7205 (2013.01); F28D 2021/0021 (2013.01);
Abstract

A rotor system including a rotor hub, and a plurality of rotor blades. Each of the plurality of rotor blades includes a hub end. A plurality of rotor blade actuators is operatively connected to the hub end of a corresponding one of the plurality of rotor blades. A fairing is mounted to the rotor hub. The fairing includes an external surface and an internal surface defining an interior portion. The hub end and rotor blade actuator of each of the plurality of rotor blades is arranged in the interior portion. A cooling system is arranged in the interior portion. The cooling system includes a first heat exchanger thermally connected to each of the plurality of rotor blade actuators, a second heat exchanger mounted to the fairing, and at least one fluid conduit extending therebetween.


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