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:
Sep. 26, 2023

Filed:

Sep. 26, 2021
Applicant:

Textron Innovations Inc., Fort Worth, TX (US);

Inventors:

Jon Damon Bennett, Melbourne, FL (US);

Joshua Allan Edler, Dallas, TX (US);

Matthew Wade Hendricks, Grand Prairie, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 27/08 (2023.01); B64D 27/26 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); B64C 27/08 (2013.01); B64D 27/26 (2013.01); B64C 2027/002 (2013.01); B64D 2041/002 (2013.01);
Abstract

One example of a mount for a rotorcraft comprises a structural support member, a bracket, and an elastomer. The bracket is configured to attach to a component of the rotorcraft. The component of the rotorcraft produces vibrations at a first frequency. The structural support member configured to transfer a weight of the component of a rotorcraft to an airframe of the rotorcraft. A rotor system of the aircraft vibrates the airframe of the rotorcraft at a second frequency. The elastomer is located between a structural support member and a bracket. The elastomer is configured to attenuate noise caused by the vibrations at the first frequency by isolating the vibrations at the first frequency from reaching the airframe of the rotorcraft while the airframe vibrates at the second frequency.


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