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:
Oct. 15, 2019
Filed:
Jul. 27, 2015
Applicant:
Sikorsky Aircraft Corporation, Stratford, CT (US);
Inventors:
Erez Eller, Oakville, CT (US);
William J. Eadie, Cheshire, CT (US);
Kevin L. Bredenbeck, Stuart, FL (US);
Steven D. Weiner, Orange, CT (US);
Assignee:
SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01); B64C 7/00 (2006.01); F02C 9/28 (2006.01); G05D 1/00 (2006.01); G05D 1/02 (2006.01); G05D 1/08 (2006.01); B64C 13/04 (2006.01); B64C 13/18 (2006.01); B64C 13/50 (2006.01); B64C 19/00 (2006.01); B64C 27/00 (2006.01); B64C 27/08 (2006.01); B64C 27/10 (2006.01); B64C 27/12 (2006.01); B64C 27/14 (2006.01); B64C 27/16 (2006.01); B64C 27/32 (2006.01); B64C 27/33 (2006.01); B64C 27/48 (2006.01); B64C 27/51 (2006.01); F16F 15/02 (2006.01); B64C 27/57 (2006.01); B64D 35/06 (2006.01); B64C 27/467 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
F16F 15/02 (2013.01); B64C 13/04 (2013.01); B64C 13/50 (2013.01); B64C 27/001 (2013.01); B64C 27/006 (2013.01); B64C 27/10 (2013.01); B64C 27/14 (2013.01); B64C 27/467 (2013.01); B64C 27/57 (2013.01); B64D 35/06 (2013.01); G05D 1/0816 (2013.01); G05D 1/0858 (2013.01); B64C 2027/004 (2013.01); B64C 2027/8236 (2013.01);
Abstract
A method of controlling noise of an aircraft includes storing a plurality of predefined noise modes; receiving a selection of a selected noise mode from the plurality of predefined noise modes, the selected noise mode identifying at least one operational parameter; and controlling the aircraft in response to the at least one operational parameter.