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:
Sep. 17, 2019

Filed:

Sep. 30, 2015
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventor:

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

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64C 27/22 (2006.01); B64C 27/57 (2006.01); B64C 11/30 (2006.01); B64C 27/10 (2006.01); B64C 27/82 (2006.01); B64D 35/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 11/305 (2013.01); B64C 27/10 (2013.01); B64C 27/57 (2013.01); B64C 27/82 (2013.01); B64D 35/00 (2013.01); B64C 2027/8236 (2013.01); B64C 2027/8281 (2013.01);
Abstract

One aspect is a flight control system for a rotary wing aircraft that includes flight control computer configured to interface with a main rotor system, a translational thrust system, and an engine control system. The flight control computer includes processing circuitry configured to execute control logic. The control logic includes a primary flight control configured to produce flight control commands for the main rotor system and the translational thrust system. Main rotor engine anticipation logic is configured to produce a rotor power demand associated with the main rotor system. Propulsor loads engine anticipation logic is configured to produce an auxiliary propulsor power demand associated with the translational thrust system. The auxiliary propulsor power is combined with the rotor power demand to produce a total power demand anticipation signal for the engine control system.


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