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. 28, 2017

Filed:

May. 06, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Sina Sam Golshany, Lynwood, WA (US);

Todd W. Erickson, Fife, WA (US);

Paul R. Tretow, Mukilteo, WA (US);

David M. Huntly, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 5/02 (2006.01); B64C 1/26 (2006.01); F16F 15/00 (2006.01); F16F 15/02 (2006.01);
U.S. Cl.
CPC ...
B64C 5/02 (2013.01); B64C 1/26 (2013.01); F16F 15/002 (2013.01); F16F 15/022 (2013.01); F16F 2228/066 (2013.01); F16F 2230/18 (2013.01);
Abstract

Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer of an aircraft. According to one aspect, a damper is coupled to a front portion of a horizontal stabilizer to dampen vibrations in a first degree of freedom, with another damper coupled to a mounting point of the horizontal stabilizer to dampen vibrations in a second degree of freedom. The dampers may be passive, operating independently to mitigate vibrational forces, or active, applying a mitigating force to the horizontal stabilizer based on real-time or estimated vibration states.


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