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:
Jan. 07, 2020

Filed:

Sep. 27, 2016
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

David Heverly, Arlington, TX (US);

David A. Popelka, Colleyville, TX (US);

Frank B. Stamps, Colleyville, TX (US);

Assignee:

Textron Innovations Inc., Providence, DE (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 11/00 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); B64C 11/008 (2013.01); B64C 29/0033 (2013.01); B64C 2027/003 (2013.01); B64C 2027/004 (2013.01); B64C 2027/005 (2013.01);
Abstract

A vibration attenuator for an aircraft has at least one weight mounted in a rotating system of a rotor hub of the aircraft, each weight being rotatable about an axis of rotation of the hub relative to the hub and to each other weight. Drive means are provided for rotating each weight about the axis of rotation at a selected speed for creating oscillatory shear forces that oppose and attenuate rotor-induced vibrations having a selected frequency. A vertically oriented vibration attenuator is configured to oppose and attenuate vertical rotor induced oscillatory forces that would otherwise travel vertical down the rotor mast and into the airframe. A vibration attenuator having weights rotating about separate axes offset from each other.


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