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    • 12. 发明授权
    • Medical instrument
    • 医疗仪器
    • US07517354B2
    • 2009-04-14
    • US10872846
    • 2004-06-21
    • Dieter Lang
    • Dieter Lang
    • A61B17/28
    • A61B17/29A61B10/06A61B17/1608A61B2017/2939
    • The invention relates to a medical instrument having a hollow shaft (2) and, positioned on its proximal end, a handle (3) consisting of at least two gripping members (3a, 3b) and, on its distal end, a tool consisting of at least two jaw members (5a, 5b). The instrument's jaw members (5a, 5b) are stationed at a lateral angle to the longitudinal axis of the shaft (2) so that at least one jaw member (5a) of the tool (5) can be moved for opening and closing by means of a gripping member (3b) of the handle (3) that can be rotated with respect to the at least one other jaw member (5b) of the tool (5) and the at least one movable jaw member (5a) and the corresponding gripping member (3b) of the handle (3) serving to move the jaw member (5a) are connected to one another by a compression-tension element (8) positioned in the hollow shaft (2). To ensure that power is transmitted precisely and without free play to the tool, it is proposed with the invention that the compression-tension element (8) and the respective jaw member (5a) of the tool (5) are connected to one another by a transmission lever (7).
    • 本发明涉及一种具有中空轴(2)的医疗器械,并且在其近端处设置有由至少两个夹持构件(3a,3b)组成的手柄(3),并且在其远端上包括由 至少两个钳口构件(5a,5b)。 仪器的钳口构件(5a,5b)以与轴(2)的纵向轴线成横向的角度安置,使得工具(5)的至少一个钳口构件(5a)可以通过装置移动以打开和关闭 手柄(3)的夹持构件(3b)可相对于工具(5)的至少一个其它钳口构件(5b)旋转,并且至少一个可移动钳口构件(5a)和相应的 用于移动钳口构件(5a)的手柄(3)的夹持构件(3b)通过位于空心轴(2)中的压缩张力元件(8)彼此连接。 为了确保功率精确地传递并且没有自由地传播到工具,本发明提出了压缩张力元件(8)和工具(5)的相应的钳口构件(5a)通过 传动杆(7)。
    • 20. 发明申请
    • Device for monitoring tiltable flaps on aircraft wings
    • 用于监控飞机机翼上的倾斜襟翼的装置
    • US20060145028A1
    • 2006-07-06
    • US11316084
    • 2005-12-21
    • Martin RichterDieter Lang
    • Martin RichterDieter Lang
    • B64C9/16
    • B64D45/0005B64D2045/001
    • In a device for monitoring tiltable flaps on aircraft wings it is proposed that rotary sensors in the rotary axis of the flap be associated with each actuating element, and a sensor rotation by way of a spring band be connected to the actuating element, as a coupler for angle transmission, at a distance to the rotary axis. The spring band is stiff in the direction of rotation, while in lateral direction, for the purpose of compensating for a transverse movements of the actuating elements, said spring band is soft. For each flap the signals of the rotary sensors, as decentralised monitoring devices to locate errors, are transmitted to an evaluation unit.
    • 在用于监测飞机机翼上的可倾斜襟翼的装置中,提出在翼片的旋转轴线上的旋转传感器与每个致动元件相关联,并且通过弹簧带将传感器旋转连接到致动元件,作为耦合器 用于角度传输,距离旋转轴。 弹簧带在旋转方向上是刚性的,而在横向方向上,为了补偿致动元件的横向运动,弹簧带是柔软的。 对于每个挡板,旋转传感器的信号作为分散监视装置来定位错误,被传送到评估单元。