ANTI-TORQUE ROTOR FOR A HELICOPTER
    1.
    发明公开

    公开(公告)号:US20240270381A1

    公开(公告)日:2024-08-15

    申请号:US18646221

    申请日:2024-04-25

    CPC classification number: B64C27/82 B64C27/72 B64C27/59

    Abstract: An anti-torque rotor includes a mast rotatable about a first axis; a plurality of blades; an element slidable along the first axis, rotating integrally with the mast and operatively connected to the blades. The rotor also has a slidable control rod; a first bearing with a rotatable first ring, a second ring radially internal to the first ring and a plurality of first rolling bodies; a third ring slidable along the first axis and angularly fixed with respect to the first axis; and a locking element arranged in a first configuration, in which it prevents the relative rotation of the second and third rings and is movable from the first configuration to at least one emergency configuration, in which it renders the second ring free to rotate with respect to the third ring, when the first bearing is in a failure condition.

    ANTI-TORQUE ROTOR FOR A HELICOPTER
    2.
    发明公开

    公开(公告)号:US20240270380A1

    公开(公告)日:2024-08-15

    申请号:US18646214

    申请日:2024-04-25

    CPC classification number: B64C27/82 B64C27/72 B64C27/59

    Abstract: An anti-torque rotor includes a mast rotatable about a first axis; a plurality of blades; an element slidable along the first axis, rotating integrally with the mast and operatively connected to the blades. The rotor also has a slidable control rod; a first bearing with a rotatable first ring, a second ring radially internal to the first ring and a plurality of first rolling bodies; a third ring slidable along the first axis and angularly fixed with respect to the first axis; and a locking element arranged in a first configuration, in which it prevents the relative rotation of the second and third rings and is movable from the first configuration to at least one emergency configuration, in which it renders the second ring free to rotate with respect to the third ring, when the first bearing is in a failure condition.

    Anti-torque rotor for a helicopter

    公开(公告)号:US12091168B2

    公开(公告)日:2024-09-17

    申请号:US17621475

    申请日:2020-05-26

    CPC classification number: B64C27/82 B64C27/72 B64C27/59

    Abstract: An anti-torque rotor includes a mast rotatable about a first axis; a plurality of blades; an element slidable along the first axis, rotating integrally with the mast and operatively connected to the blades. The rotor also has a slidable control rod; a first bearing with a rotatable first ring, a second ring radially internal to the first ring and a plurality of first rolling bodies; a third ring slidable along the first axis and angularly fixed with respect to the first axis; and a locking element arranged in a first configuration, in which it prevents the relative rotation of the second and third rings and is movable from the first configuration to at least one emergency configuration, in which it renders the second ring free to rotate with respect to the third ring, when the first bearing is in a failure condition.

    ANTI-TORQUE ROTOR FOR A HELICOPTER

    公开(公告)号:US20220340272A1

    公开(公告)日:2022-10-27

    申请号:US17621475

    申请日:2020-05-26

    Abstract: An anti-torque rotor is described comprising: a mast rotatable about a first axis; a plurality of blades rotatable about respective second axes; an element slidable along the first axis with respect to the mast, rotating integrally with the mast and operatively connected to the blades; a control rod slidable along axis; a first bearing with a first ring rotating integrally with element, a second ring radially internal to the first ring with respect to the first axis and a plurality of first rolling bodies; a third ring sliding integrally with the control rod along the first axis and angularly fixed with respect to the first axis; and a locking element arranged in a standard configuration, in which it prevents the relative rotation of the second and third rings and movable from the standard configuration to at least one emergency configuration, in which it renders the second ring free to rotate with respect to the third ring, when the first bearing is in a failure condition.

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