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    PLATEAU CYCLIQUE SUR ROTORS
    2.
    发明申请
    PLATEAU CYCLIQUE SUR ROTORS 审中-公开
    转子切换

    公开(公告)号：WO2009092898A2

    公开(公告)日：2009-07-30

    申请号：PCT/FR2008/001539

    申请日：2008-10-31

    Applicant: GUILHOT-GAUDEFFROY, Michel ,  WILLINGER, Yann

    Inventor： GUILHOT-GAUDEFFROY, Michel ,  WILLINGER, Yann

    IPC: B64C27/59

    CPC classification number: B64C27/605

    Abstract: Le plateau cyclique sur rotor utilise une partie cylindrique du rotor pour se centrer par rapport à l'axe principal de rotation. Plus compact, plus robuste, avec moins de pièces ce dispositif où la rotule-couronne porte au centre un dispositif de rotation représenté ici par un roulement et dont la partie interne porte un plan interne qui est manœuvré en au moins trois points, forme l'ensemble du plateau cyclique (rotule-couronne, roulement, et la partie interne), cette partie qui entraine l'ensemble du plateau cyclique est représenté ici par la couronne triangulaire, elle peut être déplacée dans le sens de l'axe du rotor, et également de telle sorte que son plan soit libre de mouvement angulaire par rapport à cet axe, et rend ainsi possible d'agir cycliquement sur l'angle du pas des pales par des liens entre la rotule couronne et les pieds de pale, toutes les manœuvres des voilures tournantes sont assurées.

    Abstract translation: 转子上的旋转斜盘使用转子的圆柱形部分相对于主轴线旋转自身。 更紧凑，更坚固并且更少的部件，该装置中的球接头环在其中心处承载有由滚动轴承表示的旋转装置，其内部部分具有至少三个位置的内部平面 形成斜盘组件（球接头环，滚动轴承和内部部件），驱动斜板组件的部件由三角形环表示，可以在转子的轴线方向上移动， 也以这样的方式使得其平面相对于该轴线自由地成角度地运动，并且因此通过球窝接头环和叶片根部之间的连接允许对叶片的俯仰角产生周期性的影响，所有旋翼机动​​作都被设置。

    CONNECTOR ASSEMBLY FOR ROTOR HEAD SWASHPLATE
    4.
    发明申请
    CONNECTOR ASSEMBLY FOR ROTOR HEAD SWASHPLATE 审中-公开
    转子头冲洗用连接器总成

    公开(公告)号：WO2016171849A1

    公开(公告)日：2016-10-27

    申请号：PCT/US2016/024620

    申请日：2016-03-29

    Applicant: SIKORSKY AIRCRAFT CORPORATION

    Inventor： HALCOM, Lance

    IPC: B64C27/605 ,  B64C27/59

    CPC classification number: B64C27/605 ,  B64C27/10

    Abstract: A connector assembly to connect a swashplate and a rotor shaft or hub is provided. The connector assembly includes a mount configured to fixedly connect to the rotor shaft or hub, a sleeve pivotably attached to the mount, and a translating element translationally retained within the sleeve and configured to engage with the swashplate such that the swashplate and the rotor shaft or hub rotate at the same rotational speed.

    Abstract translation: 提供连接斜盘和转子轴或毂的连接器组件。 连接器组件包括安装件，其被构造成固定地连接到转子轴或轮毂，可枢转地附接到安装件的套筒和平移保持在套筒内并被配置成与斜盘接合的平移元件，使得斜盘和转子轴或 轮毂以相同的转速旋转。

    ROTOR SWASHPLATE
    5.
    发明申请
    ROTOR SWASHPLATE 审中-公开
    转盘SWASHPLATE

    公开(公告)号：WO2009092898A3

    公开(公告)日：2009-09-24

    申请号：PCT/FR2008001539

    申请日：2008-10-31

    Applicant: GUILHOT-GAUDEFFROY MICHEL ,  WILLINGER YANN

    Inventor： GUILHOT-GAUDEFFROY MICHEL ,  WILLINGER YANN

    IPC: B64C27/59

    CPC classification number: B64C27/605

    Abstract: The swashplate (2) on a rotor (1) uses a cylindrical part (3) of the rotor to centre itself with respect to the main axis of rotation (8). More compact, more robust and with fewer parts, this device in which the ball joint-ring (4) bears at its centre a rotation device here represented by a rolling bearing (5) and the internal part of which bears an internal plane which is operated at at least three points, forms the swashplate (2) assembly (ball joint-ring, rolling bearing, and the internal part), this part which drives the swashplate assembly is represented here by the triangular ring, it can be moved in the direction of the axis of the rotor, and also in such a way that its plane is free to move angularly relative to this axis and thus allows a cyclic influence on the pitch angle of the blades through connections between the ball joint ring and the blade roots, all rotary wing manoeuvres being provided for.

    Abstract translation: 转子（1）上的斜盘（2）使用转子的圆柱形部分（3）使其自身相对于主旋转轴线（8）居中。 更紧凑，更坚固并且具有更少的部件，其中球窝接头环（4）在其中心支承着旋转装置，在此由滚动轴承（5）代表并且其内部部分具有内部平面，该内部平面是 至少在三个点上操作，形成斜盘（2）组件（球窝接头环，滚动轴承和内部部件），驱动斜盘组件的这部分在此用三角形环表示，它可以在 并且还以这样的方式使得其平面相对于该轴线成角度地自由移动并且因此允许通过球窝接头环与叶片根部之间的连接而对叶片的桨距角产生循环影响 ，所有旋翼机动​​都被提供。

    POSITION AND CONTROL SYSTEM FOR HELICOPTER BLADE ACTUATION
    6.
    发明申请
    POSITION AND CONTROL SYSTEM FOR HELICOPTER BLADE ACTUATION 审中-公开
    用于直升机叶片执行的位置和控制系统

    公开(公告)号：WO1985001490A1

    公开(公告)日：1985-04-11

    申请号：PCT/US1984001468

    申请日：1984-09-17

    Applicant: SUNDSTRAND CORPORATION

    Inventor： SUNDSTRAND CORPORATION ,  ALDRICH, Allyn, M.

    IPC: B64C27/59

    CPC classification number: B64C27/58 ,  B64C11/32

    Abstract: A helicopter blade position and control mechanism including a hollow rotor shaft (14) for mounting a plurality of rotor blades (22) with provision for pitch adjustment. A control shaft (28) is disposed within the rotor shaft and is rotatable relative thereto and is associated with actuators (20) for the blades such that the pitch of the blades is changed when the control shaft rotates relative to the rotor shaft. A planetary gear assembly (44) interconnects to control shaft and a source of power fixed to the helicopter fuselage (10) and is such that when an input to the planetary gear assembly is quiescent, the control shaft will rotate in the same direction and at the same rate as the rotor shaft to maintain a desired blade pitch. Conversely, when an input is placed on the planetary gear system, relative rotation between the control shaft and the rotor shaft will occur to provide the desired adjustment in blade pitch. The system allows accurate blade position feedback signals to be taken from a feedback device stationarily mounted on the fuselage.

    ANTI-TORQUE ROTOR FOR A HELICOPTER
    8.
    发明申请
    ANTI-TORQUE ROTOR FOR A HELICOPTER 审中-公开

    公开(公告)号：WO2020254894A1

    公开(公告)日：2020-12-24

    申请号：PCT/IB2020/054977

    申请日：2020-05-26

    Applicant: LEONARDO S.P.A.

    Inventor： DELLI PAOLI, Michele ,  NANNONI, Fabio ,  VANNI, Roberto

    IPC: B64C27/82 ,  B64C27/59 ,  B64C27/605 ,  B64C27/78 ,  B64C11/32 ,  F16C39/02 ,  F16C21/00 ,  F16C19/52 ,  B64C27/54

    Abstract: An anti-torque rotor (4) is described for a helicopter (1), comprising: a mast (6) rotatable about a first axis (A); a plurality of blades (8) hinged on the mast (6), extending along respective second axes (B) transversal to said first axis (A) and rotatable about respective said second axes (B) to alter the respective angles of attack; a control element (16) sliding and rotating with respect to the mast (6), and operatively connected to said blades (8) to cause the rotation of said blades (8) about respective second axes (B) following a translation of said element (16) along the first axis (A); a control rod (10) sliding axially along first axis (A) with respect to the mast (6) and angularly fixed with respect to the first axis (A); and a connection element (17) interposed between the control rod (10) and the control element (16), sliding along the first axis (A) with respect to the mast (6) and integrally with the control rod (10); the anti-torque rotor (4) further comprises an interface (18, 93) made of an antifriction material interposed between said control rod (10) and said connection element (17).

    MAGNETORHEOLOGICAL FLUID CLUTCH APPARATUS WITH CYLINDRICAL FLUID GAP
    9.
    发明申请
    MAGNETORHEOLOGICAL FLUID CLUTCH APPARATUS WITH CYLINDRICAL FLUID GAP 审中-公开
    具有圆柱形流体动力学的磁流体流体离合器装置

    公开(公告)号：WO2016168934A1

    公开(公告)日：2016-10-27

    申请号：PCT/CA2016/050464

    申请日：2016-04-21

    Applicant: EXONETIK INC.

    Inventor： PLANTE, Jean-Sebastien ,  DENNINGER, Marc ,  JULIO, Guifré ,  CHOUINARD, Patrick ,  LAROSE, Pascal

    IPC: F16D37/02 ,  B64C27/59 ,  F16D29/00

    CPC classification number: F16D37/02 ,  B64C27/59 ,  F16D29/00 ,  F16D37/008 ,  F16D2037/001 ,  F16D2037/004 ,  F16D2037/007

    Abstract: A magnetorheological fluid clutch apparatus comprises a stator having at least an annular wall; a first rotor rotatably mounted to the stator, the first rotor having at least one first shear surface; a second rotor rotatably mounted to the stator for rotating about a common axis with the first rotor, the second rotor having at least one second shear surface opposite the at least one first shear surface, the shear surfaces separated by at least one annular space. A magnetorheological (MR) fluid is in an MR fluid chamber including the at least one annular space, the MR fluid configured to generate a variable amount of torque transmission between the rotors when subjected to a magnetic field. An inner magnetic core and an outer magnetic core with an annular cavity therebetween receive the annular wall of the stator, the inner magnetic core and the outer magnetic core connected to at least one of the rotors to rotate therewith so as to be rotatably mounted to the stator. Outer and inner fluid gaps are between the inner magnetic core and the annular wall, and between the outer magnetic core and the annular wall, the outer and inner fluid gaps filled with at least one fluid. At least one coil is supported by the annular wall and actuatable to deliver a magnetic field through the MR fluid, the magnetic field following a path comprising the annular wall, the outer fluid gap, the outer magnetic core, the at least one first shear surface and the at least one second shear surface, the inner magnetic core and the inner fluid gap, wherein one of the rotors is adapted to be coupled to a power input and the other of the rotors is adapted to be connected to an output whereby actuation of the at least one coil results in a variation of torque transmission between the rotors.

    Abstract translation: 磁流变流体离合器装置包括至少具有环形壁的定子; 可转动地安装在所述定子上的第一转子，所述第一转子具有至少一个第一剪切面; 可旋转地安装到定子上的第二转子，用于与第一转子围绕公共轴线旋转，第二转子具有与至少一个第一剪切表面相对的至少一个第二剪切表面，剪切表面由至少一个环形空间分隔开。 磁流变（MR）流体在包括至少一个环形空间的MR流体室中，MR流体被配置为当经受磁场时在转子之间产生可变量的转矩传递。 内部磁芯和具有环形空腔的外部磁芯接收定子的环形壁，内部磁芯和外部磁芯连接至至少一个转子以与其一起旋转，以便可旋转地安装在 定子。 外部和内部流体间隙在内部磁芯和环形壁之间，以及在外部磁芯和环形壁之间，外部和内部流体间隙填充有至少一种流体。 至少一个线圈由环形壁支撑并且可致动以通过MR流体输送磁场，磁场遵循包括环形壁，外部流体间隙，外部磁芯，至少一个第一剪切表面 和所述至少一个第二剪切表面，所述内部磁芯和所述内部流体间隙，其中所述转子中的一个适于联接到动力输入，并且所述转子中的另一个适于连接到输出端，从而致动 所述至少一个线圈导致转子之间的扭矩传递的变化。

    ROTOR SWASHPLATE
    10.
    发明申请
    ROTOR SWASHPLATE 审中-公开
    转子切换

    公开(公告)号：WO2009092898A4

    公开(公告)日：2009-11-19

    申请号：PCT/FR2008001539

    申请日：2008-10-31

    Applicant: GUILHOT-GAUDEFFROY MICHEL ,  WILLINGER YANN

    Inventor： GUILHOT-GAUDEFFROY MICHEL ,  WILLINGER YANN

    IPC: B64C27/59

    CPC classification number: B64C27/605

    Abstract: The swashplate (2) on a rotor (1) uses a cylindrical part (3) of the rotor to centre itself with respect to the main axis of rotation (8). More compact, more robust and with fewer parts, this device in which the ball joint-ring (4) bears at its centre a rotation device here represented by a rolling bearing (5) and the internal part of which bears an internal plane which is operated at at least three points, forms the swashplate (2) assembly (ball joint-ring, rolling bearing, and the internal part), this part which drives the swashplate assembly is represented here by the triangular ring, it can be moved in the direction of the axis of the rotor, and also in such a way that its plane is free to move angularly relative to this axis and thus allows a cyclic influence on the pitch angle of the blades through connections between the ball joint ring and the blade roots, all rotary wing manoeuvres being provided for.

    Abstract translation: 转子（1）上的旋转斜盘（2）使用转子的圆柱形部分（3）相对于主轴线（8）自身居中。 更紧凑，更坚固和更少的部件，该装置中球形接头环（4）在其中心处具有由滚动轴承（5）表示的旋转装置，其内部部分承载着内部平面 在至少三点操作，形成斜盘（2）组件（球形接头环，滚动轴承和内部部件），驱动旋转斜盘组件的部件由三角形环表示，可以在 转子的轴线方向，并且也使得其平面相对于该轴线自由地成角度地移动，从而通过球形接头环和叶片根部之间的连接允许对叶片的桨距角的周期性影响 所有的旋翼机动作都被提供。

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