DEVICE FOR SWITCHABLE PILOT CONTROL FORCES
    1.
    发明申请
    DEVICE FOR SWITCHABLE PILOT CONTROL FORCES 有权
    用于可切换的引导控制力的装置

    公开(公告)号:US20100123045A1

    公开(公告)日:2010-05-20

    申请号:US12620893

    申请日:2009-11-18

    Inventor: Wolfram Grieser

    Abstract: A device for controlling vehicles having a manual control unit configured to influence the direction of movement of a vehicle. The manual control unit provides, in a neutral position of the manual control unit, a trim point to determine a preferred direction of movement. The device further includes a force generating device, generating at least one force acting in the direction of the neutral position of the manual control unit; a trim coupling operable to reduce the at least one force acting on the manual control unit; and a trim control unit configured to store and retain the trim point existing prior to an operation of the trim coupling.

    Abstract translation: 一种用于控制车辆的装置,其具有构造成影响车辆的移动方向的手动控制单元。 手动控制单元在手动控制单元的中立位置提供修剪点以确定优选的移动方向。 该装置还包括力产生装置,产生沿手动控制单元的中立位置的方向作用的至少一个力; 修剪联接器,可操作以减小作用在手动控制单元上的至少一个力; 以及修剪控制单元,其构造成在修剪联接器的操作之前存储和保持现有的修剪点。

    Hydraulic system
    2.
    发明授权
    Hydraulic system 有权
    液压系统

    公开(公告)号:US07581486B2

    公开(公告)日:2009-09-01

    申请号:US11624597

    申请日:2007-01-18

    Inventor: Wolfram Grieser

    CPC classification number: F15B1/02 F15B2201/31 F15B2201/32

    Abstract: A hydraulic system includes a reservoir for a hydraulic fluid, a pump, a high-pressure line network, a low-pressure line network and operating cylinders each of which can be connected to the high-pressure line network or to the low-pressure line network via control units, each operating cylinder is associated with a local compensation volume element.

    Abstract translation: 液压系统包括用于液压流体的储存器,泵,高压线路网络,低压线路网络和操作气缸,每个可连接到高压线路网络或低压线路 网络通过控制单元,每个操作缸与局部补偿体积元件相关联。

    Device for switchable pilot control forces
    3.
    发明授权
    Device for switchable pilot control forces 有权
    用于切换先导控制力的装置

    公开(公告)号:US08376283B2

    公开(公告)日:2013-02-19

    申请号:US12620893

    申请日:2009-11-18

    Inventor: Wolfram Grieser

    Abstract: A device for controlling vehicles having a manual control unit configured to influence the direction of movement of a vehicle. The manual control unit provides, in a neutral position of the manual control unit, a trim point to determine a preferred direction of movement. The device further includes a force generating device, generating at least one force acting in the direction of the neutral position of the manual control unit; a trim coupling operable to reduce the at least one force acting on the manual control unit; and a trim control unit configured to store and retain the trim point existing prior to an operation of the trim coupling.

    Abstract translation: 一种用于控制车辆的装置,其具有构造成影响车辆的移动方向的手动控制单元。 手动控制单元在手动控制单元的中立位置提供修剪点以确定优选的移动方向。 该装置还包括力产生装置,产生沿手动控制单元的中立位置的方向作用的至少一个力; 修剪联接器,可操作以减小作用在手动控制单元上的至少一个力; 以及修剪控制单元,其构造成在修剪联接器的操作之前存储和保持现有的修剪点。

    HYDRAULIC SYSTEM
    4.
    发明申请
    HYDRAULIC SYSTEM 有权
    液压系统

    公开(公告)号:US20070163251A1

    公开(公告)日:2007-07-19

    申请号:US11624597

    申请日:2007-01-18

    Inventor: Wolfram Grieser

    CPC classification number: F15B1/02 F15B2201/31 F15B2201/32

    Abstract: A hydraulic system includes a reservoir for a hydraulic fluid, a pump, a high-pressure line network, a low-pressure line network and operating cylinders each of which can be connected to the high-pressure line network or to the low-pressure line network via control units, each operating cylinder is associated with a local compensation volume element.

    Abstract translation: 液压系统包括用于液压流体的储存器,泵,高压线路网络,低压线路网络和操作气缸,每个可连接到高压线路网络或低压线路 网络通过控制单元,每个操作缸与局部补偿体积元件相关联。

    Method for deploying a parachute on a drone
    5.
    发明授权
    Method for deploying a parachute on a drone 失效
    在无人机上部署降落伞的方法

    公开(公告)号:US06471160B2

    公开(公告)日:2002-10-29

    申请号:US09865106

    申请日:2001-05-24

    Inventor: Wolfram Grieser

    CPC classification number: B64D17/80 B64C2201/185

    Abstract: A flying drone includes a flight control computer, a parachute system with a parachute, a power supply system, a propulsion system, and an actuating drive system, without any of these systems being redundantly duplicated. To prevent uncontrolled crashing of the drone due to a critical error of any subsystem, signals or data are supplied from the power supply system, the propulsion system, and the actuating drive system, to an error detection or recognition device, which detects defined errors or error combinations in the provided signals or data and then supplies a deployment signal to the parachute system, which responsively generates a control signal that triggers an ejection mechanism to eject the parachute.

    Abstract translation: 飞行无人机包括飞行控制计算机,具有降落伞的降落伞系统,电源系统,推进系统和致动驱动系统,而没有任何这些系统被冗余地重复。 为了防止由于任何子系统的关键错误导致的无人驾驶飞机的不受控制的撞击,信号或数据从电源系统,推进系统和致动驱动系统提供给检错定义的错误或错误检测或识别装置 所提供的信号或数据中的错误组合,然后将部署信号提供给降落伞系统,其响应地产生触发弹射机构以弹出降落伞的控制信号。

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