- 专利标题: Anti-torque rotor for a helicopter
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申请号: US17424294申请日: 2020-05-26
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公开(公告)号: US12071230B2公开(公告)日: 2024-08-27
- 发明人: Michele Delli Paoli , Fabio Nannoni , Roberto Vanni
- 申请人: LEONARDO S.P.A.
- 申请人地址: IT Rome
- 专利权人: LEONARDO S.P.A.
- 当前专利权人: LEONARDO S.P.A.
- 当前专利权人地址: IT Rome
- 代理机构: Leason Ellis LLP
- 优先权: EP 182436 2019.06.25
- 国际申请: PCT/IB2020/054976 2020.05.26
- 国际公布: WO2020/260979A 2020.12.30
- 进入国家日期: 2021-07-20
- 主分类号: B64C27/59
- IPC分类号: B64C27/59 ; B64C27/82
摘要:
An anti-torque rotor is described comprising: a mast rotatable about a first axis; a plurality of blades hinged on the mast and rotatable about respective second axes to vary the respective angles of attack; a control element sliding along the first axis with respect to the mast, rotatable with the mast and connected to the blades to cause the rotation about the second axes; a control mechanism, axially sliding and angularly fixed with respect to the mast; and a connection element interposed between the control mechanism and the control element, sliding integrally with the control mechanism along the mast; the control mechanism comprises a first and a second rod; the rotor comprises a coupling, which is configured to enable/prevent rotation of the second rod with respect to the first rod when the torque exerted by the first connection element on the second rod about the first axis is greater/less than a threshold value in the event of failure of the connection element.
公开/授权文献
- US20220073196A1 ANTI-TORQUE ROTOR FOR A HELICOPTER 公开/授权日:2022-03-10
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