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. 09, 2024

Filed:

May. 26, 2020
Applicant:

Leonardo S.p.a., Rome, IT;

Inventors:

Attilio Colombo, Samarate, IT;

Gabriele Cazzulani, Samarate, IT;

Simone Cinquemani, Samarate, IT;

Ferruccio Resta, Samarate, IT;

Francesco Braghin, Samarate, IT;

Assignee:

LEONARDO S.P.A., Rome, IT;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 27/06 (2006.01); B64C 27/46 (2006.01);
U.S. Cl.
CPC ...
B64C 27/001 (2013.01); B64C 27/06 (2013.01); B64C 27/46 (2013.01); B64C 2027/003 (2013.01); B64C 2027/004 (2013.01); B64C 2027/005 (2013.01);
Abstract

A rotor for a hover-capable aircraft includes an attenuating device to attenuate the transmission of vibrations from a mast to the aircraft. The attenuating device includes a first mass free to oscillate parallel to a hub rotation axis with respect to a casing of the attenuating device and elastically connected to the casing. The attenuating device further includes a second mass free to oscillate parallel to the hub rotation axis, connection means adapted to make the first and second masses integrally movable along the hub rotation axis when the angular speed of the mast assumes a first value, and actuator means activatable to decouple the first and second masses when the angular speed of the mast assumes a second value, different from the first value.


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