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.
Patent No.:
Date of Patent:
Jun. 23, 2020
Filed:
Feb. 08, 2018
Applicant:
Sikorsky Aircraft Corporation, Stratford, CT (US);
Inventors:
David L. Adams, Wallingford, CT (US);
Kevin Ron Fimbers, Seymour, CT (US);
Assignee:
SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01L 3/08 (2006.01); B64C 27/00 (2006.01); B64C 27/08 (2006.01); B64D 43/02 (2006.01); B64D 45/00 (2006.01); G01C 23/00 (2006.01); G05D 1/08 (2006.01); B64C 27/22 (2006.01);
U.S. Cl.
CPC ...
G01L 3/08 (2013.01); B64C 27/08 (2013.01); B64D 43/02 (2013.01); B64D 45/0005 (2013.01); G01C 23/005 (2013.01); B64C 27/22 (2013.01); G05D 1/0858 (2013.01);
Abstract
A torque indicator for an aircraft having a main rotor system and a translational thrust system driven by at least one engine includes a first indicator operable to display an actual torque of an engine of the aircraft relative to an engine torque limit, a second indicator operable to display an actual torque of the translational thrust system of the aircraft relative to a translational thrust system torque limit, and a third indicator operable to display an actual torque of the main rotor system of the aircraft relative to a main rotor system torque limit.