CONTACT DETECTION
    1.
    发明申请
    CONTACT DETECTION 有权
    接触检测

    公开(公告)号:US20110266396A1

    公开(公告)日:2011-11-03

    申请号:US13098513

    申请日:2011-05-02

    IPC分类号: B64C13/46

    摘要: The invention relates to a method for detecting a contact state between at least one driver/operator of a vehicle and a control input device designed to control the vehicle were a frequency spectrum is calculated from sensors detected movement signals based on which the contact state between the control input device and the driver/operator is determined.

    摘要翻译: 本发明涉及一种用于检测车辆的至少一个驾驶员/驾驶员与被设计成控制车辆的控制输入装置之间的接触状态的方法,其特征在于,根据传感器检测到的运动信号来计算频谱, 控制输入​​设备和驾驶员/操作员被确定。

    Early identification of a vortex ring phase
    2.
    发明授权
    Early identification of a vortex ring phase 有权
    早期鉴定涡环相

    公开(公告)号:US09037316B2

    公开(公告)日:2015-05-19

    申请号:US13809628

    申请日:2011-07-13

    IPC分类号: G06F17/00 B64C27/00

    CPC分类号: G06F17/00 B64C27/006

    摘要: A method for early detection of the vortex ring state in a helicopter includes steps of establishing flight control signals for flight control with regard to the vertical movement axis of the helicopter, detecting resultant movements in the vertical movement axis of the helicopter, and detecting an impending vortex ring state of the helicopter in accordance with a correlation between the flight control signals and the vertical movements in the vertical movement axis.

    摘要翻译: 一种用于在直升机中早期检测涡环状态的方法包括建立关于直升机的垂直运动轴的飞行控制信号的飞行控制信号的步骤,检测直升机的垂直运动轴中的合成运动,以及检测即将到来的 根据飞行控制信号与垂直运动轴上的垂直运动之间的相关性,直升机的涡环状态。

    EARLY IDENTIFICATION OF A VORTEX RING PHASE
    3.
    发明申请
    EARLY IDENTIFICATION OF A VORTEX RING PHASE 有权
    早期识别VORTEX戒指相位

    公开(公告)号:US20130173091A1

    公开(公告)日:2013-07-04

    申请号:US13809628

    申请日:2011-07-13

    IPC分类号: G06F17/00

    CPC分类号: G06F17/00 B64C27/006

    摘要: The invention relates to a method for early detection of the vortex ring state in a helicopter, having the following steps: establishing flight control signals for flight control with regard to the vertical movement axis of the helicopter and detecting resultant movements in the vertical movement axis of the helicopter, and detecting early the vortex ring state of the helicopter in accordance with a correlation between the flight control signals and the vertical movements in the vertical movement axis.

    摘要翻译: 本发明涉及一种用于在直升机中早期检测涡环状态的方法,具有以下步骤:建立关于直升机的垂直运动轴的飞行控制的飞行控制信号,并检测直升机的垂直运动轴的合成运动 直升机,并且根据飞行控制信号与垂直运动轴线的垂直运动之间的相关性早期检测直升机的涡环状态。

    Rotatable antifriction bearing
    5.
    发明申请
    Rotatable antifriction bearing 审中-公开
    可旋转减摩轴承

    公开(公告)号:US20120068575A1

    公开(公告)日:2012-03-22

    申请号:US13232352

    申请日:2011-09-14

    申请人: Max Abildgaard

    发明人: Max Abildgaard

    IPC分类号: H01L41/113 H01L41/04

    摘要: The invention relates to a rotatable antifriction bearing (1) having a first bearing ring (2), a second bearing ring (3) which can be rotated with respect to the first bearing ring (2), and a plurality of rolling bodies (4) which are arranged between the first and the second bearing ring (2, 3), at least one rolling body (4) being configured as an electric sensor in such a way that the rolling body (4) is set up for changing a directly electrically detectable characteristic variable as a function of a force which is exerted on said rolling body (4). Moreover, the invention relates to a rolling body for an antifriction bearing of this type, and to a device having an antifriction bearing and an electric monitoring device.

    摘要翻译: 本发明涉及一种具有第一轴承环(2),能相对于第一轴承环(2)旋转的第二轴承环(3)的旋转减摩轴承(1),以及多个滚动体 )设置在第一和第二轴承环(2,3)之间,至少一个滚动体(4)被构造为电传感器,使得滚动体(4)被设置成直接改变 作为施加在所述滚动体(4)上的力的函数的电可检测特性变量。 此外,本发明涉及一种用于这种类型的减摩轴承的滚动体以及具有减摩轴承和电监测装置的装置。