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:
Dec. 09, 2014

Filed:

Dec. 20, 2012
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Joseph W. Wendelsdorf, Arlington, TX (US);

Keith Hale, Joshua, TX (US);

Walter West Riley, Richardson, TX (US);

Charles Eric Covington, Colleyville, TX (US);

Brian E. Tucker, Fort Worth, TX (US);

Assignee:

Bell-Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 17/00 (2006.01); G01M 13/02 (2006.01); G01M 5/00 (2006.01); B64C 27/04 (2006.01);
U.S. Cl.
CPC ...
G06F 17/00 (2013.01); G01M 13/02 (2013.01); G01M 5/0016 (2013.01); B64C 27/04 (2013.01);
Abstract

A method of optimizing an operation of a rotorcraft includes measuring actual usage of the tail rotor drive shaft during operation of the rotorcraft, the actual usage including at least a torque measurement. The method further includes a step of adjusting a life of the tail rotor drive shaft based upon the measuring of the actual usage. Another method of the present disclosure includes determining a main rotor mast torque by measuring a tail rotor drive shaft torque and deriving a main rotor mast torque by considering the measured tail rotor drive shaft torque and a total torque output of an engine. A system of the present disclosure is configured for determining the main rotor mast torque in part by measuring the tail rotor torque.


Find Patent Forward Citations

Loading…