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:
Nov. 29, 2016

Filed:

Apr. 09, 2015
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Harshad S. Sane, Southbury, CT (US);

Joseph T. Driscoll, Prospect, CT (US);

Igor Cherepinsky, Sandy Hook, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); G01P 5/16 (2006.01); B64C 13/16 (2006.01); B64D 43/02 (2006.01); G01P 5/02 (2006.01); B64C 5/02 (2006.01); B64C 5/10 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
G01P 5/16 (2013.01); B64C 13/16 (2013.01); B64C 27/00 (2013.01); B64D 43/02 (2013.01); G01P 5/02 (2013.01); B64C 5/02 (2013.01); B64C 5/10 (2013.01); B64C 2027/8263 (2013.01);
Abstract

An aircraft is provided and includes an airframe. The airframe includes first and second rotor apparatuses at upper and tail portions of the aircraft, respectively, to provide for control and navigational drive. The aircraft further includes a stabilizer component disposed at the tail portion in a position displaced from downwash of the first and second rotor apparatuses at airspeed ranges and a control system configured to apply a dither actuation signal to the stabilizer component at the airspeed ranges by which an aircraft response to a stabilizer component input is measurable for airspeed estimation purposes.


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