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:
Jun. 27, 2023

Filed:

Sep. 16, 2022
Applicant:

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

Inventors:

Stephen Howard Fagan, Wichita, KS (US);

Paul Stokholm Warren, Wichita, KS (US);

Emily O'Kelley Pearson, Wichita, KS (US);

Jeremy Joseph Kneuper, Hesston, KS (US);

Phillip Anthony Kendrick, Wichita, KS (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 11/06 (2006.01);
U.S. Cl.
CPC ...
B64D 11/0619 (2014.12); B64D 11/064 (2014.12); B64D 11/06395 (2014.12);
Abstract

A seat base includes a plurality of linear actuators each having a first end pivotally mounted to a base member and a second end pivotally mounted to a seat member. A controller is adapted for controlling an extension length of each of the plurality of linear actuators in a coordinated manner for adjusting a position of the seat member with six degrees-of-freedom and for damping vibration of the seat member. An active vibration mitigation method for reducing vibrations of an aircraft seat includes receiving vibration data from one or more accelerometers mounted to the aircraft seat and determining a vibration profile based on the vibration data. When vibration mitigation is warranted, control signals for damping vibration are determined and transmitted to a plurality of linear actuators adapted to support the aircraft seat.


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