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公开(公告)号：US20190352000A1
公开(公告)日：2019-11-21
申请号：US16473701
申请日：2017-12-29
Applicant: LEONARDO S.P.A.
Inventor： Luigi BOTTASSO , Antonio ZOCCHI , Massimo BRUNETTI , Luca MEDICI , James WANG , Giorgio LUCCHI
Abstract: There is disclosed a rotor for an aircraft capable of hovering, comprising: a stationary support structure; a rotative element, which is rotatable about a first axis with respect to said stationary support structure with a first rotational speed; at least one blade, which is operatively connected with said rotative element; and a transmission group, which comprises an output element rotatable about first axis with a second rotational speed different from first rotational speed.
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