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    Floated gimbal optical platform
    2.
    发明授权
    Floated gimbal optical platform 有权
    浮动云台光学平台

    公开(公告)号：US6145393A

    公开(公告)日：2000-11-14

    申请号：US433345

    申请日：1999-11-04

    申请人： Dino Canton

    发明人： Dino Canton

    IPC分类号： G01C21/18 ,  G02B27/64 ,  G01C19/52 ,  F16M13/00 ,  G03B17/00

    CPC分类号： G01C21/18 ,  G02B27/644 ,  Y10T74/1239 ,  Y10T74/125

    摘要： The invention is a floated gimbal instrument platform that provides a stable optical path for optical instruments. The instrument platform has an outer vessel with a transparent viewing port, an inner vessel also with a transparent viewing port, a transparent suspending fluid filling the outer vessel and in which the inner vessel floats in neutral buoyancy, an optical instrument secured inside the inner vessel, spacing studs which centrally position the inner vessel within the outer vessel, and jets which align the second viewing port with the first viewing port, the jets being used to rotate the inner vessel in the suspending fluid. Any misalignment between the viewing ports can be compensated by rotating the inner vessel and any translational forces applied to the platform is dampened by the fluid, thereby eliminating jitter.

    摘要翻译： 本发明是提供光学仪器的稳定光路的浮动万向节仪器平台。 仪器平台具有外部容器，其具有透明观察口，内部容器也具有透明观察口，透明悬浮液填充外部容器，内部容器以中性浮力浮动，固定在内部容器内的光学仪器 将内部容器中心定位在外部容器内的间隔螺柱以及将第二观察口与第一观察口对准的射流，所述射流用于使内部容器在悬浮液中旋转。 可以通过旋转内部容器来补偿观察端口之间的任何不对准，并且施加到平台的任何平移力被流体阻尼，从而消除抖动。

    Erector
    3.
    发明授权
    Erector 失效
    演员

    公开(公告)号：US4669323A

    公开(公告)日：1987-06-02

    申请号：US696902

    申请日：1985-01-31

    申请人： Takeshi Hojo ,  Shinichi Kawada

    发明人： Takeshi Hojo ,  Shinichi Kawada

    IPC分类号： G01C19/52 ,  G01C19/30

    CPC分类号： G01C19/52 ,  Y10T74/1243 ,  Y10T74/1286

    摘要： An erector for holding a spin axis of a gyro rotor in the vertical direction used in a gyroscopic horizon or gyro vertical which comprises a gyro casing incorporating therein a gyro rotor rotating at high speed, a spin axis of the gyro rotor being held substantially in the vertical direction, first supporting member for rotatably supporting the gryo casing around a first horizontal axis which is perpendicular to the spin axis and second supporting member for rotatably supporting the first supporting member around a second horizontal axis which is perpendicular to both the spin axis and the first horizontal axis is disclosed, which includes a base plate, a motor mounted on the base plate, a rotation receptacle container having an annular shape cavity and rotated at low speed by the motor, and liquid charged into the annular shape cavity of the rotation receptacle container, the base plate being mounted on the gyro casing such that the rotation axis of the rotation receptacle container and the spin axis of the gyro rotor become parallel to each other.

    摘要翻译： 一种用于在陀螺仪水平仪或陀螺仪垂直方向上保持陀螺仪转子的旋转轴的竖立装置，该陀螺仪转子包括在其中结合有高速旋转的陀螺仪转子的陀螺仪套管，陀螺仪转子的旋转轴基本保持在 垂直方向的第一支撑构件，用于围绕垂直于旋转轴线的第一水平轴线可旋转地支撑冰球壳体;以及第二支撑构件，用于可旋转地支撑第一支撑构件围绕垂直于旋转轴线和第二支撑构件的第二水平轴线 公开了第一水平轴，其包括基板，安装在基板上的电动机，具有环形形状空腔并由电动机低速旋转的旋转容器容器，以及装入旋转容器的环形空腔中的液体 容器，基板安装在陀螺仪壳体上，使得旋转容器容器的旋转轴线a 并且陀螺转子的旋转轴彼此平行。

    Air erected gyro
    6.
    发明授权
    Air erected gyro 失效
    空气竖立陀螺仪

    公开(公告)号：US4088031A

    公开(公告)日：1978-05-09

    申请号：US764492

    申请日：1977-01-31

    申请人： Leonard D. Sholes

    发明人： Leonard D. Sholes

    IPC分类号： G01C19/30 ,  G01C19/52 ,  G01C19/44

    CPC分类号： G01C19/30 ,  G01C19/52 ,  Y10T74/1239 ,  Y10T74/1268 ,  Y10T74/1286

    摘要： An air erected gyro includes an erection-force producing air stream and gravity-responsive valve means whose gate portion is movable across the air stream so as to vary the erection force magnitude. Also included is a compensator means connected for movement with the gate and for also confronting the air stream so as to at least partially counteract air stream induced horizontal coercive effects on the valve means position.

    摘要翻译： 空气竖立的陀螺仪包括产生竖立力的气流和重力响应阀装置，其门部分可跨过气流移动，以便改变勃起力的大小。 还包括补偿器装置，其连接用于与闸门一起运动并且还面对空气流，以便至少部分地抵消空气流对阀装置位置的水平矫顽效应。

    Hydraulic rate gyro for an adaptive steering system
    7.
    发明授权
    Hydraulic rate gyro for an adaptive steering system 失效
    用于自适应转向系统的液压速度陀螺仪

    公开(公告)号：US3673875A

    公开(公告)日：1972-07-04

    申请号：US3673875D

    申请日：1970-03-19

    申请人： BENDIX CORP

    发明人： KASSELMANN JOHN T

    IPC分类号： G01C19/00 ,  G01C19/52

    CPC分类号： G01C19/00 ,  Y10T74/1239 ,  Y10T74/1282

    摘要： A rate gyro providing a fluidic output signal corresponding to the yaw rate of a vehicle, for use in an adaptive steering system. The gyro rotor is hydraulically supported and spun via tangential reaction jets connected in parallel with flapper nozzles situated to provide both a differential pressure signal corresponding to yaw rate and a centering spring force creating gyro natural frequencies well above the disturbance frequencies encountered. The support, jet, and nozzle fluid supplies are all incorporated into the power steering supply circuit.

    Control of gyroscope spin-up devices
    8.
    发明授权
    Control of gyroscope spin-up devices 失效
    陀螺旋转装置的控制

    公开(公告)号：US3667301A

    公开(公告)日：1972-06-06

    申请号：US3667301D

    申请日：1970-10-02

    申请人： PLESSEY TELECOMMUNICATIONS RES

    发明人： KENT ALAN HUGH ,  DAVIS JOHN CHRISTOPHER HAMMOND

    IPC分类号： G01C19/12 ,  G01C19/26 ,  G01C19/52

    CPC分类号： G01C19/12 ,  Y10T74/1239

    摘要： A gyroscope and spin-up system in which the gyroscope rotor is rotated by fluid from a spin-up device. Fluid pulses are generated as a result of fluid from the spin-up device striking pulse-generating fluid-receiving areas provided on the rotor. The number of pulses produced depends upon the speed of the rotor. The pulses act on a resonant means which operates at a predetermined rotor speed to cut off the supply of fluid to the spin-up system.

    摘要翻译： 陀螺仪和旋转系统，其中陀螺仪转子由旋转装置的流体旋转。 由于来自旋转装置的流体撞击设置在转子上的脉冲发生流体接收区域，产生流体脉冲。 产生的脉冲数取决于转子的速度。 脉冲作用在共振装置上，该谐振装置以预定的转子速度工作，以切断对旋转系统的流体供应。

    Air-driven gyroscope erection system with seal-free gimbal connections
    9.
    发明授权
    Air-driven gyroscope erection system with seal-free gimbal connections 失效
    具有无密封GIMBAL连接的空气驱动陀螺仪检测系统

    公开(公告)号：US3606794A

    公开(公告)日：1971-09-21

    申请号：US3606794D

    申请日：1969-04-28

    申请人： SOUTHWESTERN IND INC

    发明人： CULVER IRVEN H

    IPC分类号： G01C19/52 ,  G01C19/12

    CPC分类号： G01C19/52 ,  Y10T74/1239 ,  Y10T74/1286

    摘要： AN ERECTING SYSTEM FOR A VERTICAL GYROSCOPE USEFUL IN AIRCRAFT ATTITUDE-INDICATING INSTRUMENTS AND THE LIKE. A GIMBAL-SUPPORTED HOUSING IN THE GYRO ENCLOSES A GYRO ROTOR, AND IS SUPPLIED WITH AIR WHICH DRIVES THE ROTOR. AIR IS EXHAUSTED FROM THE HOUSING THROUGH FOUR DOWNWARDLY DIRECTED OUTLET PORTS AT THE CORNERS OF THE HOUSING UNDERSURFACE. CONTROL VANES ARE PENDULOUSLY SUPPORTED ON THE HOUSING AND EXTEND BENEATH THE OUTLET PORTS TO INTERCEPT THE EXHAUST AIR STREAMS AND THEREBY IMPART TORQUES TO THE GYROSCOPE TENDING TO ERECT THE ROTOR SPIN AXIS A SUBSTANTIALLY VERTICAL POSITION. AIR PASSAGES THROUGH OUTER AND INNER GIMBALS SUPPLY AIR TO THE HOUSING, AND THE PASSAGES ARE CONFIGURED SO A PRESSURE DIFFERENTIAL EXISTS ACROSS A ROTARY CONNECTION BETWEEN THE INNER AND OUTER GIMBALS. A PRESSURE DROP OCCURS GOING FROM THE OUTER GIMBAL TO THE INNER GIMBAL OR ROTOR HOUSING, WHEREBY AIR DELIVERED TO THE ROTOR DOES NOT TEND TO LEAK OUTWARDLY THROUGH THE ROTARY CONNECTION AND THE NEED FOR BULKY AND FRICTIONPRODUCING SEALS IS ELIMINATED.

    Luggage processing station and system thereof
    10.
    发明授权
    Luggage processing station and system thereof 有权

    公开(公告)号：US10252821B2

    公开(公告)日：2019-04-09

    申请号：US15904070

    申请日：2018-02-23

    申请人： ICM AIRPORT TECHNICS AUSTRALIA PTY LTD

    发明人： Richard Dinkelmann ,  Rainer Rudolf Dinkelmann

    IPC分类号： G06F7/00 ,  B64F1/36 ,  B07C5/04 ,  G01G11/00 ,  G01B11/02 ,  G06Q10/02 ,  G06Q50/28 ,  G01G19/414 ,  G01G19/52 ,  G01C11/00 ,  G01C19/52 ,  G06Q10/08

    摘要： A processing station for registering a piece of passenger's luggage for a trip, wherein the processing station comprises: an injector for receiving the piece of luggage associated with the passenger; at least one sensor associated with the injector, the at least one sensor, in combination with at least the floor of the injector, creating a zone around the piece of luggage; and a controller associated with the sensor being adapted to: monitor, via the at least one sensor, intrusions through the zone to determine one or more of whether a predetermined limit on dimensions of the piece of luggage has been exceeded or whether a foreign object has intruded the zone from outside, and allow further processing of the piece of luggage only if no intrusion of the zone is detected; and wherein the controller adjusts the area of the zone to accommodate different sizes of luggage.