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. 16, 2022

Filed:

May. 29, 2018
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Aaron Kellner, Bloomfield, CT (US);

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

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

Assignee:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B60R 16/03 (2006.01); H01R 39/08 (2006.01); H01R 39/34 (2006.01); B64C 27/32 (2006.01); H02K 13/00 (2006.01); B64C 27/04 (2006.01); H01R 39/18 (2006.01);
U.S. Cl.
CPC ...
H01R 39/08 (2013.01); B60R 16/03 (2013.01); B64C 27/04 (2013.01); B64C 27/32 (2013.01); H01R 39/18 (2013.01); H01R 39/34 (2013.01); H02K 13/003 (2013.01); B64D 2221/00 (2013.01);
Abstract

A computer-implemented method and system for transmitting power and data together in a rotorcraft using a slip ring assembly is disclosed. According to one example, a computer-implemented method includes providing a slip ring assembly comprising a stationary element coupled to an airframe of a rotorcraft and a rotatable element rotatable relative to the stationary element and coupled to a rotor assembly of the rotorcraft. Power is transmitted from a power source associated with the airframe to an electronic device associated with the rotor assembly, the slip ring assembly being configured to complete an electrical circuit between the power source and the electronic device to provide power from the power source to the electronic device. Data is transmitted from a first data transceiver associated with the airframe to a second data transceiver associated with the rotor assembly via the electrical circuit completed by the slip ring assembly.


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