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. 04, 2022

Filed:

Dec. 16, 2019
Applicant:

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

Inventors:

Christopher Edward Foskey, Colleyville, TX (US);

Frank Bradley Stamps, Colleyville, TX (US);

Michael Reaugh Smith, Colleyville, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 27/22 (2006.01); B64C 27/10 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); B64C 27/10 (2013.01); B64C 27/22 (2013.01); B64C 27/82 (2013.01); B64C 2027/002 (2013.01); B64C 2027/8236 (2013.01); B64C 2027/8281 (2013.01);
Abstract

An advancing blade concept rotorcraft includes an airframe and a pylon assembly subject to vibration. The pylon assembly includes a dual rotor system having coaxially disposed top and bottom rotor assemblies that counter rotate relative to one another. The advancing blade concept rotorcraft includes a vibration isolation system including at least one pylon link coupled to the airframe and the pylon assembly. The pylon link includes a Liquid Inertia Vibration Eliminator unit operable to reduce transmission of the pylon assembly vibration to the airframe. The advancing blade concept rotorcraft includes active force generators adjacent to the pylon assembly. The active force generators include a first active force generator producing a force in a first direction and a second active force generator producing a force in a second direction to counteract multidirectional oscillations of the pylon assembly, thereby reducing vibration of the advancing blade concept rotorcraft.


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