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:
Apr. 17, 2018
Filed:
Feb. 10, 2015
Applicant:
Sikorsky Aircraft Corporation, Stratford, CT (US);
Inventors:
Robert J. Andrejczyk, Sandy Hook, CT (US);
David H. Sweet, Jupiter, FL (US);
Assignee:
SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2011.01); G06G 7/70 (2006.01); B64D 31/06 (2006.01); F02D 41/02 (2006.01); F02D 41/10 (2006.01); B60R 16/03 (2006.01); B64D 43/00 (2006.01); B64D 45/00 (2006.01); F02D 41/14 (2006.01); F02D 29/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B60R 16/03 (2013.01); B64D 43/00 (2013.01); B64D 45/00 (2013.01); F02D 29/02 (2013.01); F02D 41/021 (2013.01); F02D 41/10 (2013.01); F02D 41/1497 (2013.01); B64D 2221/00 (2013.01); F02D 2250/18 (2013.01); F02D 2250/22 (2013.01);
Abstract
A method of adaptive engine acceleration for accessory loads includes receiving an accessory load indicator corresponding to an accessory load of an engine. The accessory load indicator is compared to an adjustment threshold. An acceleration rate of the engine is increased based on determining that the accessory load indicator is below the adjustment threshold. The acceleration rate of the engine is decreased based on determining that the accessory load indicator is above the adjustment threshold.