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:
Mar. 30, 2010

Filed:

Nov. 19, 2007
Applicants:

Askari Badre-alam, Apex, NC (US);

Douglas Swanson, Cary, NC (US);

Jeffrey Cranmer, Holly Springs, NC (US);

Inventors:

Askari Badre-Alam, Apex, NC (US);

Douglas Swanson, Cary, NC (US);

Jeffrey Cranmer, Holly Springs, NC (US);

Assignee:

Lord Corporation, Cary, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method/system for controlling helicopter vibrations is provided that includes a vibration canceling force generator for actively generating a vibration canceling force. The system includes a resonant actuator having a natural resonant frequency and a resonant actuator electronic control system. The resonant actuator electronic control system provides an electrical drive current to the resonant actuator to drive the resonant actuator about the resonant frequency when commanded by a received command signal. The resonant actuator has a feedback output with the feedback output fed back into the resonant actuator electronic control system wherein the resonant actuator electronic control system adjusts the electrical drive current based on the resonant actuator feedback output to generate the vibration canceling force.


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