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:
Oct. 14, 2014

Filed:

Mar. 31, 2011
Applicants:

Karim Khial, Seymour, CT (US);

James J. Howlett, North Haven, CT (US);

Stuart C. Wright, Woodbridge, CT (US);

Inventors:

Karim Khial, Seymour, CT (US);

James J. Howlett, North Haven, CT (US);

Stuart C. Wright, Woodbridge, CT (US);

Assignee:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2011.01); B64C 25/00 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 25/00 (2013.01); B64D 45/00 (2013.01); B64D 2045/008 (2013.01);
Abstract

A system for sensing a force applied to an aircraft includes a first sensor, a second sensor, and a processor operative to define a first velocity vector as a function of a first velocity due to a rotation motion of the aircraft, define a second velocity vector as a function of a second velocity due to the rotation motion of the aircraft, define an instant axis of rotation of the aircraft as a function of the first velocity vector and the second velocity vector, determine whether a force has been exerted on a first portion of the aircraft, and output an indication that a force has been exerted on the first portion of the aircraft responsive to determining that the force has been exerted on the first portion of the aircraft.


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