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. 20, 2020

Filed:

Oct. 13, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Michael T. Fox, Saint Charles, MO (US);

Jeffrey M. Roach, Saint Charles, MO (US);

Eric A. Howell, Ballwin, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16F 7/10 (2006.01); F16F 7/06 (2006.01); F16F 15/12 (2006.01); F16F 15/121 (2006.01); B64C 9/02 (2006.01);
U.S. Cl.
CPC ...
F16F 7/065 (2013.01); B64C 9/02 (2013.01); F16F 7/1022 (2013.01); F16F 15/1204 (2013.01); F16F 15/1208 (2013.01); F16F 15/1216 (2013.01);
Abstract

There is provided a translational inerter assembly for damping movement of a flight control surface of an aircraft with a support structure. The translational inerter assembly includes a press fit element rotatably disposed within the flight control surface. The translational inerter assembly further includes an inertia element disposed in the press fit element. The translational inerter assembly further includes a torsion bar coupled to the inertia element and to the support structure of the aircraft, such that when the flight control surface rotates, the inertia element translates, and movement of the flight control surface is dampened.


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