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:
Jun. 08, 2021

Filed:

Aug. 03, 2020
Applicant:

Geoffrey S. M. Hedrick, Malvern, PA (US);

Inventor:

Geoffrey S. M. Hedrick, Malvern, PA (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); B64D 31/10 (2006.01); B64D 43/00 (2006.01); G08G 5/04 (2006.01); F02C 7/26 (2006.01); F02C 9/26 (2006.01); F02C 9/54 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01); G05D 3/12 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/10 (2013.01); B64D 43/00 (2013.01); F02C 7/26 (2013.01); F02C 9/26 (2013.01); F02C 9/54 (2013.01); G05D 1/0072 (2013.01); G05D 1/0816 (2013.01); G05D 3/12 (2013.01); G08G 5/0008 (2013.01); G08G 5/04 (2013.01); F05D 2220/323 (2013.01); F05D 2270/051 (2013.01); F05D 2270/093 (2013.01); F05D 2270/12 (2013.01); F05D 2270/13 (2013.01); F05D 2270/20 (2013.01); F05D 2270/303 (2013.01);
Abstract

Aircraft autothrottle system, having a motor to impart rotational movement to a shaft extending from the motor. An actuator is connected to the shaft and to an attachment end of a throttle lever having a control end, opposite the attachment end. The actuator has bearings to apply thrust to a longitudinal surface of the shaft such that the actuator is translated longitudinally along the shaft surface in response to motor-imparted rotation of the shaft. The shaft surface being smoothly continuous and longitudinally unbroken along its elongation to allow the actuator to longitudinally slip along the shaft irrespective of any shaft rotation by the motor when the thrust force exceeds a linear force manually applied at the throttle lever. An electronic controller for the motor to move the throttle lever so the motor moves the actuator assembly along the shaft based on an engine parameter monitored by the controller.


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