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:
Apr. 13, 2021

Filed:

Oct. 24, 2018
Applicant:

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

Inventors:

Michael Reaugh Smith, Colleyville, TX (US);

Jouyoung Jason Choi, Southlake, TX (US);

Assignee:

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

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); F16F 7/10 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); F16F 7/1022 (2013.01); B64C 2027/005 (2013.01); F16F 2222/08 (2013.01);
Abstract

An anti-tail buffet device leverages existing rotorcraft components to attenuate a tailboom's lateral 'ringing' from air buffeting. Anti-buffet masses are tuned to the tailboom's lateral-bending or torsional natural frequency such that when lateral motion occurs, the response at this frequency is cancelled by the anti-buffet system, preventing this vibration from entering into the tailboom structure. Motion stops prevent over-travel. The mass of the tail rotor actuator is soft-mounted, such that its natural frequency is equal to the tailboom's lateral-bending or torsional natural frequency. When lateral loading occurs on the tail rotor disk, the lateral response at this frequency is attenuated by the soft-mounted tail rotor actuator, thereby preventing the vibration in the tailboom structure.


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