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    VORRICHTUNG ZUR DREHBAREN LAGERUNG VON WERKSTÜCKEN, INSBESONDERE KURBELWELLEN
    2.
    发明公开
    VORRICHTUNG ZUR DREHBAREN LAGERUNG VON WERKSTÜCKEN, INSBESONDERE KURBELWELLEN 有权
    维多利亚·维尔伯恩·维尔·韦克斯肯（VERRICHTUNG ZUR DREHBAREN LAGERUNG）

    公开(公告)号：EP3140631A1

    公开(公告)日：2017-03-15

    申请号：EP15722980.8

    申请日：2015-05-06

    申请人： Schenck RoTec GmbH

    发明人： BÄHR, Joachim ,  KREUZER, Sebastian

    IPC分类号： G01M1/04

    CPC分类号： G01M1/04 ,  F16C13/04 ,  F16C17/02 ,  F16C17/26 ,  F16C23/02 ,  F16C2370/00

    摘要： The invention relates to a device for receiving work pieces to be balanced in a machine for performing an imbalance compensation having a bearing device (2) arranged on a machine frame for rotatable mounting of the work piece (3) around a bearing axis (L), wherein the bearing device (2) has at least one bearing block (10) having two bearing shells (18, 19) having differing diameter which lie adjacent to each other, crosswise to the bearing axis (L). The bearing block (10) is movable crosswise to the bearing axis (L) of the bearing device (2) to two bearing positions and another of the two bearing shells (18, 19) is aligned centrally to the bearing axis (L) in each of the two bearing positions.

    摘要翻译： 本发明涉及一种用于接收在机器中平衡的工件以进行不平衡补偿的装置，该装置具有布置在机架上的用于将工件（3）围绕轴承轴线（L）可旋转地安装的轴承装置（2），其中 所述轴承装置（2）具有至少一个轴承座（10），所述至少一个轴承座（10）具有两个直径不同并且在横向于所述轴承轴线（L）的方向上彼此相邻的轴承壳体（18,19）。 所述轴承座（10）能够横向于所述轴承装置（2）的轴承轴线（L）移动到两个轴承位置，并且所述两个轴承壳体（18,19）中的另一个与所述轴承轴线（L） 在两个轴承位置的每一个中。

    VERMESSUNGSGERÄT MIT KUGELPUNKTLAGERUNG
    4.
    发明公开
    VERMESSUNGSGERÄT MIT KUGELPUNKTLAGERUNG 有权
    VERMESSUNGSGERÄTMIT KUGELPUNKTLAGERUNG

    公开(公告)号：EP3006894A1

    公开(公告)日：2016-04-13

    申请号：EP14188460.1

    申请日：2014-10-10

    申请人： Leica Geosystems AG

    发明人： Müller, Josef ,  Petkov, Stefan ,  Schöll, Benjamin

    IPC分类号： G01C15/00 ,  F16C11/06 ,  F16D3/22

    CPC分类号： G01C3/02 ,  F16C19/507 ,  F16C2370/00 ,  F16C2370/20 ,  G01C15/002

    摘要： In einem Vermessungsgerät (1) mit einer Basis (2) zur Positionierung des Vermessungsgerätes (1) und einer Neigkomponente (4) mit einem optischen Strahlengang zur Vermessung eines Zieles ist die Neigkomponente (4) in einer gegenüber der Basis (2) bewegbaren Gierkomponente (3) anhand eines in zwei Kavitäten (10, 11) selbstzentrierend eingespannten Rotationskörper (9) radial und axial gelagert und gegenüber der Gierkomponente (3) drehbar.

    摘要翻译： 在具有用于定位测量装置的基座和具有用于测量目标的光束路径的俯仰分量的测量装置中，俯仰分量被径向和轴向安装，并且在偏航分量中可相对于偏航分量旋转，即偏航分量 基于在两个空腔中以自定心方式夹紧的旋转体相对于基座移动。

    ROTATING SHAFT HOLDING MECHANISM AND ROTATIONAL VISCOMETER WITH SAME
    6.
    发明公开
    ROTATING SHAFT HOLDING MECHANISM AND ROTATIONAL VISCOMETER WITH SAME 有权
    保持机构旋转轴与SO旋转粘度计

    公开(公告)号：EP2851573A1

    公开(公告)日：2015-03-25

    申请号：EP12877072.4

    申请日：2012-05-18

    申请人： NATIONAL INSTITUTE OF ADVANCED INDUSTRIAL SCIENCE AND TECHNOLOGY

    发明人： NASHIMA Takeshi ,  YAMAMOTO Yasuyuki

    IPC分类号： F16C11/04 ,  G01N11/14

    CPC分类号： F16C27/02 ,  F16C1/02 ,  F16C11/12 ,  F16C2370/00 ,  G01N11/14

    摘要： A compact and high-precision rotating shaft holding mechanism is provided which can be utilized for a device that requires a small amount of rotation.
    A rotating shaft holding mechanism includes a plurality of parallel spring links, each of the plurality of parallel spring links including: a movable side connected to a rotating shaft by a hinge at a connection point at a distance h radially away from a center of rotation of the rotating shaft; a plurality of deformable sides which are parallel to each other; hinges each of which connects one end of a corresponding one of the deformable sides to the movable side; and hinges each of which connects the other end of a corresponding one of the deformable sides to the stationary section, the effective length of each of the deformable sides being set to h to permit the rotating shaft, which is connected to the movable side by the hinge at the connecting point at the distance h radially away from the center of rotation of the rotating shaft, to rotate within a range of finite angles, the plurality of parallel spring links including at least two parallel spring links oriented in different directions. A rotational viscometer uses the rotating shaft holding mechanism.

    Inertial measurement unit with gas plenums
    7.
    发明公开
    Inertial measurement unit with gas plenums 审中-公开
    惯性测量单元Gasplena

    公开(公告)号：EP2017575A3

    公开(公告)日：2015-02-25

    申请号：EP08160131.2

    申请日：2008-07-10

    申请人： Honeywell International Inc.

    发明人： Chappell, Charles D. ,  Bowen, David A.

    IPC分类号： G01C19/20 ,  G01C21/16 ,  F16C32/06 ,  G01P15/03

    CPC分类号： G01C21/16 ,  F16C32/0622 ,  F16C32/0666 ,  F16C2370/00 ,  G01C19/20 ,  G01P1/023 ,  G01P15/08

    摘要： An inertial measurement unit comprises a mounting plate with an opening therethrough, and a sensor assembly disposed in the opening of the mounting plate. Upper and lower support shells having shell flanges are attached to upper and lower surfaces of the mounting plate. The upper and lower support shells surround the sensor assembly. A plurality of gas bearing pads each extends through apertures in the upper and lower support shells. Upper and lower gas plenums have plenum flanges attached to the shell flanges of the upper and lower support shells, with the upper and lower gas plenums surrounding the upper and lower support shells. Pressure relief valves are coupled to the plenum flanges of the upper and lower gas plenums. The gas bearing pads and the sensor assembly are separated by a gap when pressurized gas is fed into the upper and lower gas plenums, thereby creating a gas bearing that allows the sensor assembly to be freely suspended and rotated in all directions.

    DIRECT TORQUE CONTROL MOMENT GYROSCOPE
    10.
    发明授权
    DIRECT TORQUE CONTROL MOMENT GYROSCOPE 失效
    STE ENT EL EL ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT ENT

    公开(公告)号：EP0675824B1

    公开(公告)日：1996-10-09

    申请号：EP94904084.4

    申请日：1993-12-13

    申请人： HONEYWELL INC.

    发明人： HAVENHILL, Douglas, D.

    IPC分类号： B64G1/28 ,  H02K7/09 ,  G01C19/30

    CPC分类号： F16C39/06 ,  B64G1/286 ,  F16C32/04 ,  F16C2326/47 ,  F16C2370/00 ,  G01C19/30 ,  H02K7/09 ,  Y10T74/1218 ,  Y10T74/125

    摘要： A control moment gyroscope (10) for providing directional control in a spacecraft. The control moment gyroscope has a rotor (50) which is electrostatically or magnetically supported within a gimbal housing (24) so as not to touch any of the interior surfaces of the housing. The housing is mounted on a gimbal support (14) which in turn is mounted on the spacecraft. Connected to the gimbal housing is a torque motor (12) which rotates the housing around a gimbal axis. In order to induce a direction changing torque on the spacecraft, the rotor (50) is first spun about its rotor axis. A torque is then induced on the rotor (50) about the output axis. This induced torque will cause the rotor (50) to precess about the gimbal axis which the torque motor follows. The torque induced around the output axis is transferred directly to the spacecraft.

    摘要翻译： 一种用于在航天器中提供方向控制的控制力矩陀螺仪。 控制力矩陀螺仪具有静电或磁力支撑在万向架壳体内的转子，以便不接触壳体的任何内表面。 外壳安装在万向架支架上，后者又安装在航天器上。 连接到万向节壳体的是扭矩马达，该马达使壳体围绕万向轴旋转。 为了在航天器上引起方向变化的扭矩，转子首先围绕其转子轴线旋转。 然后在转子上围绕输出轴线产生转矩。 这种引起的转矩将导致转子绕转矩马达跟随的万向节轴线进行。 输出轴周围产生的转矩直接转移到航天器。