Motor vehicle door lock, bonnet lock or the like
    8.
    发明授权
    Motor vehicle door lock, bonnet lock or the like 失效
    机动车门锁,发动机罩锁等

    公开(公告)号:US06113161A

    公开(公告)日:2000-09-05

    申请号:US147579

    申请日:1999-01-26

    摘要: A motor vehicle door lock has a rotary latch with a holding recess formed in it. The rotary latch has a main catch with a catch surface formed on it. A key collar has a pin that is adapted to be received in the holding recess. A pivotally mounted detent pawl is biased in an engagement direction and has a catch lever having an opposing catch surface formed on it which is adapted to engage the catch surface of the main catch in a catch position. The catch lever and a support lever are pivotally mounted on an axle to pivot with respect to one another about an axis in the catch position in which the detent pawl is biased by a spring element into an extended position. An actuating element is disposed on the rotary latch, and the spring element cooperates with the actuating element to bias the detent pawl into the extended position when said actuating element engages the spring element. The rotary latch executes an overstroke when the motor vehicle door closes, and the spring element biases the detent pawl into the extended position prior to or during the overstroke.

    摘要翻译: PCT No.PCT / DE97 / 01262 Sec。 371日期1999年1月26日 102(e)日期1999年1月26日PCT提交1997年6月19日PCT公布。 出版物WO98 / 04800 日期1998年2月5日机动车门锁具有形成在其中的保持凹部的旋转闩锁。 旋转闩锁具有形成在其上的捕获表面的主抓。 钥匙圈具有适于容纳在保持凹部中的销。 枢转地安装的止动爪被沿着接合方向偏置并且具有一个卡扣杆,该卡扣杆具有形成在其上的相对的卡扣表面,其适于在主扣件的卡扣表面处于卡扣位置。 锁定杆和支撑杆枢转地安装在轴上以相对于彼此围绕锁定位置的轴线枢转,其中止动爪被弹簧元件偏压到延伸位置。 致动元件设置在旋转闩锁上,并且当所述致动元件接合弹簧元件时,弹簧元件与致动元件配合以将止动爪偏压到伸出位置。 当机动车门关闭时,旋转闩锁执行过冲程,并且弹簧元件在超行程之前或期间将制动棘爪偏压到伸出位置。

    Locking wedge for a motor vechicle door lock or the like, and motor
vehicle door lock with said locking wedge
    9.
    发明授权
    Locking wedge for a motor vechicle door lock or the like, and motor vehicle door lock with said locking wedge 失效
    用于电动车门锁或类似物的锁定楔,以及具有所述锁定楔的机动车门锁

    公开(公告)号:US6068309A

    公开(公告)日:2000-05-30

    申请号:US147580

    申请日:1999-01-26

    IPC分类号: B60J5/00 E05B15/02 E05B85/04

    摘要: The subject of the invention is a key collar for a motor vehicle door lock or the like including a key collar support plate fixedly attached on a support sheet, and a collar element supported on the collar support plate which, in operation, engages a lock catch of the motor vehicle door lock or the like. Optionally, the key collar includes an elastomer arrangement which allows the collar element to move a limited distance relative to the collar support plate in the plane of the collar support plate thereby better meeting the different requirements of normal use conditions and during a vehicle crash. In operation, the collar element of a preferred embodiment is supported on the collar support plate on two spaced bearing points, one bearing point with a trailing bridge in a manner that collar element can be swivelled around an axis which is perpendicular to collar support plate, and another bearing point with a leading bridge which can be displaced in corresponding arc-shaped crank.

    摘要翻译: PCT No.PCT / DE97 / 01256 Sec。 371日期1999年1月26日 102(e)日期1999年1月26日PCT提交1997年6月19日PCT公布。 公开号WO98 / 04797 日本1998年2月5日本发明的主题是用于机动车门锁等的钥匙圈,其包括固定在支撑片上的钥匙圈支撑板,以及支撑在套环支撑板上的套环元件, 接合机动车门锁等的锁扣。 可选地,钥匙圈包括弹性体装置,其允许套环元件在套环支撑板的平面中相对于套环支撑板移动有限的距离,从而更好地满足正常使用条件和车辆碰撞期间的不同要求。 在操作中,优选实施例的轴环元件在两个间隔的支承点上支撑在轴环支撑板上,一个轴承点具有后桥,该轴承座可以围绕垂直于轴环支撑板的轴线旋转, 另一个带有可在相应的弧形曲柄中移位的引导桥的支承点。

    Method for load limiting in drive systems for aircraft high lift systems
    10.
    发明授权
    Method for load limiting in drive systems for aircraft high lift systems 失效
    用于飞机高升力系统的驱动系统中的负载限制方法

    公开(公告)号:US08074937B2

    公开(公告)日:2011-12-13

    申请号:US10579420

    申请日:2004-11-12

    IPC分类号: B64C13/16

    CPC分类号: B64D45/0005 B64D2045/001

    摘要: The invention relates to a device for load limitation in a aircraft high lift system, said system comprising individual segments of landing flap systems and slat flap systems, and a drive unit. The inventive device for load limitation comprises a control unit that is connected to position sensors and is embodied in such a way as to process signals from the position sensors and to generate a signal for limiting the supplied drive power. The invention also relates to a method for load limitation. According to said method, signals from at least two position sensors are measured; at least one reference variable is calculated form the measured signals; each reference variable is compared with a corresponding threshold value pre-determined from a maximum authorized load; and a control signal is generated for limiting the drive power, when at least one of the reference variables reaches or exceeds the threshold value.

    摘要翻译: 本发明涉及一种用于飞机高升降系统中的负载限制的装置,所述系统包括着陆挡板系统和板条翼片系统的单独部分以及驱动单元。 本发明的用于负载限制的装置包括连接到位置传感器的控制单元,并且以这样的方式实现,以便处理来自位置传感器的信号并产生用于限制所提供的驱动功率的信号。 本发明还涉及一种用于负载限制的方法。 根据所述方法,测量来自至少两个位置传感器的信号; 从测量信号计算出至少一个参考变量; 将每个参考变量与从最大授权负载预先确定的对应阈值进行比较; 并且当至少一个参考变量达到或超过阈值时,产生用于限制驱动功率的控制信号。