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:
Apr. 16, 2019

Filed:

Sep. 21, 2015
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Matthew T. Luszcz, Hamden, CT (US);

Matthew A. White, Milford, CT (US);

Kenneth S. Wittmer, Sandy Hook, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/57 (2006.01); B64C 27/10 (2006.01); B64C 27/605 (2006.01); B64C 27/22 (2006.01);
U.S. Cl.
CPC ...
B64C 27/57 (2013.01); B64C 27/10 (2013.01); B64C 27/605 (2013.01); B64C 27/22 (2013.01);
Abstract

A system and method for counteracting a rotor moment of one or more rotors of a coaxial rotor helicopter includes receiving signals with a processor indicative of a displacement command from a controller during a flight maneuver; receiving one or more signals with the processor from a sensor indicative of an airspeed and air density for the helicopter; determining a commanded rate of acceleration for the helicopter during the flight maneuver; and adjusting with one or more control servos a cyclic pitch for the one or more rotors to counteract the rotor moment during the flight maneuver.


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