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:
Nov. 28, 2023

Filed:

May. 20, 2022
Applicant:

Textron Aviation Inc., Wichita, KS (US);

Inventor:

Stephen M. Eddy, Derby, KS (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02D 29/02 (2006.01); F02D 9/02 (2006.01); F02D 11/04 (2006.01); B64C 11/30 (2006.01); B64D 31/04 (2006.01);
U.S. Cl.
CPC ...
F02D 9/02 (2013.01); B64C 11/30 (2013.01); B64D 31/04 (2013.01); F02D 11/04 (2013.01); F02D 29/02 (2013.01); F02D 2009/021 (2013.01); F02D 2009/0277 (2013.01);
Abstract

An automatic aircraft powerplant control system includes a throttle servo for adjusting a throttle valve via a throttle control linkage. A throttle control lever provides a user input to the throttle servo, and a throttle controller controls the throttle servo for controlling a throttle valve. A dual-redundant propellor servo drive provides propellor control, and a dual-redundant mixture servo drive controls an air-fuel mixture. A first processor and a second processor are communicatively coupled with the dual-redundant propellor servo drive and the dual-redundant mixture servo drive and with each other to provide dual-redundant propellor and mixture control. The throttle control lever provides a single lever for pilot control of aircraft power, and the throttle control configuration is compatible with an auto-land capability.


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