ROTARY ACTUATOR
    1.
    发明申请
    ROTARY ACTUATOR 审中-公开
    旋转执行器

    公开(公告)号:US20160177722A1

    公开(公告)日:2016-06-23

    申请号:US14974192

    申请日:2015-12-18

    摘要: A rotary actuator includes an output shaft, a housing, a piston, and a friction reducer. The housing includes an arcuate bore that extends around the output shaft. The piston is coupled to the output shaft and moved in the arcuate bore. Pressure fluid acts to move the piston. The friction reducer is configured to reduce friction between a peripheral surface of the piston and an inner circumferential surface of the housing forming the arcuate bore.

    摘要翻译: 旋转致动器包括输出轴,壳体,活塞和摩擦减速器。 壳体包括围绕输出轴延伸的弧形孔。 活塞联接到输出轴并在弓形孔中移动。 压力流体用于移动活塞。 摩擦减速器被构造成减小活塞的外周表面和形成弓形孔的壳体的内圆周表面之间的摩擦。

    ROTARY ACTUATOR
    2.
    发明申请
    ROTARY ACTUATOR 有权
    旋转执行器

    公开(公告)号:US20130104729A1

    公开(公告)日:2013-05-02

    申请号:US13662967

    申请日:2012-10-29

    IPC分类号: F16H29/02

    摘要: A cylinder is installed within a case. An output shaft is installed in a hollow space within the cylinder. A pair of pistons extend in an arc, and is supported so as to be able to slide and be displaced along a circumferential direction of the cylinder within the cylinder. The pair of pistons is able to urge an arm integrated with the output shaft from two sides of the arm. Pressure chambers into which a pressure medium is introduced are defined between the cylinder and each piston in the pair of pistons. The pressure medium is fed to one of the pressure chambers and drained from the other, and thus the arm is displaced, and the output shaft pivots in a rotational direction.

    摘要翻译: 气瓶安装在外壳内。 输出轴安装在气缸内的中空空间中。 一对活塞以弧形延伸,并且被支撑成能够沿着气缸内的气缸的圆周方向滑动并移位。 一对活塞能够从臂的两侧推动与输出轴一体化的臂。 气缸与活塞中的每个活塞之间形成有压力介质被引入的压力室。 将压力介质供给到一个压力室并从另一个排出,从而使臂移位,输出轴沿旋转方向转动。

    FLUID ACTUATOR
    3.
    发明申请

    公开(公告)号:US20210040962A1

    公开(公告)日:2021-02-11

    申请号:US16936082

    申请日:2020-07-22

    IPC分类号: F15B15/14 F15B13/04

    摘要: One object is to reduce a weight of a fluid actuator. The fluid actuator includes: a cylinder having an inner space and a first mounting portion, the inner space being partitioned into a first fluid chamber and a second fluid chamber, the first mounting portion being disposed on an end portion of the cylinder on an axial direction A side; and a piston rod configured to reciprocate in accordance with pressures in the fluid chambers. A wall portion defining the first fluid chamber in the cylinder is made of an iron-based alloy. A wall portion defining the second fluid chamber in the cylinder is made of an aluminum alloy. The piston rod is made of an iron-based alloy.

    ROTARY ACTUATOR
    4.
    发明申请
    ROTARY ACTUATOR 有权
    旋转执行器

    公开(公告)号:US20130133513A1

    公开(公告)日:2013-05-30

    申请号:US13686423

    申请日:2012-11-27

    发明人: Koji ITO

    IPC分类号: F04C9/00

    摘要: A cylinder is installed within a case, and an output shaft and an arm that is integrated thereto and extends in a radial direction are installed within the cylinder. A piston extending in an arc slides and is displaced in a circumferential direction of the cylinder within the cylinder. One end portion of the piston is rotatably connected to the arm. The cylinder is internally provided with a first pressure chamber in which the arm is housed and a second pressure chamber in which the other end portion of the arm is slidably installed. A pressure medium is fed into one of the first and second pressure chambers and discharged from the other, and the output shaft pivots in a rotational direction.

    摘要翻译: 气缸安装在壳体内,并且输出轴和与其一体并且沿径向方向延伸的臂安装在气缸内。 在圆弧中延伸的活塞滑动,并在气缸内的气缸的圆周方向上移位。 活塞的一个端部可旋转地连接到臂上。 气缸在内部设置有第一压力室,臂容纳在该第一压力室中,并且第二压力室中臂的另一端可滑动地安装在该第二压力室中。 压力介质被输送到第一和第二压力室中的一个并且从另一个排出,并且输出轴沿旋转方向枢转。

    DRIVE UNIT AND MAINTENANCE METHOD FOR THE SAME

    公开(公告)号:US20210155340A1

    公开(公告)日:2021-05-27

    申请号:US17094269

    申请日:2020-11-10

    摘要: A drive unit includes an actuator from which an output rod protrudes at one end of a cylinder and being coupled to a flap of an aircraft, an attachment disposed on the other side of the cylinder, a reaction link coupled to the flap at one end and to the attachment at the other end, and a connection-disconnection section allowing the cylinder and the attachment to be coupled to and separated from each other.

    TEST APPARATUS FOR ACTUATOR
    6.
    发明申请

    公开(公告)号:US20210080351A1

    公开(公告)日:2021-03-18

    申请号:US17001430

    申请日:2020-08-24

    IPC分类号: G01M13/022

    摘要: Provided is a test apparatus for an actuator, which can easily switch whether to establish or undo the coupling between an actuator to be tested and a load part configured to apply load to the actuator. A test apparatus for an actuator includes a load part for outputting load to be applied to an actuator to be tested, first levers for swinging around a rotational shaft in connection with an output from the load part, an idler link coupled to the output from the actuator to be tested, a second lever coupled to the idler link in a swingable manner and for swinging around a rotational shaft that is arranged coaxially with the rotational shaft of the first levers, and a clutch mechanism for coupling together the first levers and the second lever and undoing the coupling.

    AIRCRAFT HYDRAULIC VALVE
    8.
    发明申请
    AIRCRAFT HYDRAULIC VALVE 审中-公开
    飞机液压阀

    公开(公告)号:US20160098045A1

    公开(公告)日:2016-04-07

    申请号:US14870938

    申请日:2015-09-30

    发明人: Koji ITO

    摘要: An aircraft hydraulic valve includes a housing, a check valve, a valve opening component, and an auxiliary hydraulic pressure supply mechanism. The housing includes a first port communicated with a first chamber of a hydraulic actuator, a second port communicated with a switch valve bypass-communicating a second chamber of the hydraulic actuator with the first chamber, and an oil channel connecting the first and second ports. The check valve interrupts oil flow from the first port to the second port. The valve opening component is configured to open the check valve with pilot pressure supplied from the second chamber. The auxiliary hydraulic pressure supply mechanism obtains hydraulic pressure, for opening the check valve, from a closed hydraulic pressure section, which is defined in the oil channel between the check valve and the first port.

    摘要翻译: 飞机液压阀包括壳体,止回阀,阀开启部件和辅助液压供给机构。 壳体包括与液压致动器的第一室连通的第一端口,与连接第一室的液压致动器的第二室的开关阀旁路连通的第二端口以及连接第一和第二端口的油通道。 止回阀中断从第一个端口到第二个端口的油流量。 阀开启部件构造成以从第二室供应的先导压力来打开止回阀。 辅助液压供给机构从在止回阀和第一端口之间的油通道中限定的闭合液压部分获得用于打开止回阀的液压。

    HYDRAULIC ACTUATOR
    9.
    发明申请
    HYDRAULIC ACTUATOR 有权
    液压执行器

    公开(公告)号:US20160096617A1

    公开(公告)日:2016-04-07

    申请号:US14872406

    申请日:2015-10-01

    发明人: Koji ITO

    IPC分类号: B64C13/40 F15B15/20 F15B15/16

    摘要: A hydraulic actuator is adapted to drive a spoiler of a wing having a flap. When the hydraulic actuator drives the spoiler in an overlapping region where a driving range of the flap and a driving range of the spoiler overlap, an output suppressing structure suppress a drive output of the hydraulic actuator in the overlapping region to be less than that in a non-overlapping region other than the overlapping region.

    摘要翻译: 液压致动器适于驱动具有翼片的机翼的扰流板。 当液压致动器在翼片的驱动范围和扰流板的驱动范围重叠的重叠区域中驱动扰流板时,输出抑制结构抑制重叠区域中的液压致动器的驱动输出小于 重叠区域以外的非重叠区域。

    ROTARY ACTUATOR
    10.
    发明申请
    ROTARY ACTUATOR 有权
    旋转执行器

    公开(公告)号:US20130247754A1

    公开(公告)日:2013-09-26

    申请号:US13848591

    申请日:2013-03-21

    IPC分类号: F04B53/00

    摘要: An output shaft and arms are installed inside a cylinder. Pistons that are formed in an arc shape and rotatably connected to the arms slide and are displaced in the circumferential direction of the cylinder inside the cylinder. Inside the cylinder, a first pressure chamber on the arm side and second pressure chambers on the piston head portion side are provided. Third pressure chambers are provided on both sides of the cylinder. A pressure medium is supplied to one of the first pressure chamber and the second pressure chamber and discharged from the other, and the output shaft pivots in a rotational direction. When the pressure medium is supplied to the second pressure chambers, the pressure medium is also supplied to the third pressure chambers.

    摘要翻译: 输出轴和臂安装在气缸内。 形成为弧形并可旋转地连接到臂的活塞滑动并在气缸内的气缸的圆周方向上移位。 在气缸内,设置臂侧的第一压力室和活塞头部侧的第二压力室。 第三压力室设置在气缸的两侧。 将压力介质供给到第一压力室和第二压力室中的一个并从另一个排出,输出轴沿旋转方向枢转。 当将压力介质供应到第二压力室时,压力介质也被供应到第三压力室。