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公开(公告)号：US20080157542A1
公开(公告)日：2008-07-03
申请号：US10595417
申请日：2004-09-27
CPC分类号： E05C9/06 , E05B47/0012 , E05B2047/0024 , E05B2047/0068 , E05C9/16 , Y10T70/5208 , Y10T70/5226 , Y10T70/527 , Y10T292/0834 , Y10T292/084 , Y10T292/0964 , Y10T292/1016 , Y10T292/57
摘要： A security lock arrangement (10) includes a carrier (40) to be mounted on a wing member. At least one latch bolt (28-34) is displaceably arranged relative to the carrier (40) between a retracted, unlocked position and an extended, locked position. An urging means (60) acts on the at least one latch bolt (28-34) for urging the latch bolt (28-34) to its extended, locked position. A drive means is mounted on the carrier (40) for driving the at least one latch bolt (28-34) at least into its retracted position against the action of the urging means (60). A displacement mechanism is interposed between the drive means and the at least one latch bolt (28-34), the displacement mechanism comprising a cam member (64) rotatably driven by the drive means, the cam member (64) acting on a follower of the at least one latch bolt (28-34), the cam member (64) having a maximum throw when the at least one latch bolt (28-34) is proximate its retracted position.
摘要翻译： 安全锁装置（10）包括安装在机翼构件上的托架（40）。 至少一个闩锁螺栓（28-34）在缩回的解锁位置和延伸的锁定位置之间相对于托架（40）可移位地布置。 推动装置（60）作用在至少一个闩锁螺栓（28-34）上，用于将闩锁螺栓（28-34）推动到其延伸的锁定位置。 驱动装置安装在载体（40）上，用于抵抗推动装置（60）的作用至少将其中的至少一个闩锁螺栓（28-34）驱动到其缩回位置。 位移机构设置在驱动装置和至少一个闩锁螺栓（28-34）之间，移动机构包括由驱动装置旋转驱动的凸轮构件（64），凸轮构件（64）作用在驱动装置 所述至少一个闩锁螺栓（28-34），当所述至少一个闩锁螺栓（28-34）靠近其缩回位置时，所述凸轮构件（64）具有最大投射。
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公开(公告)号：US07591157B2
公开(公告)日：2009-09-22
申请号：US10595417
申请日：2004-09-27
IPC分类号： E05B63/14
CPC分类号： E05C9/06 , E05B47/0012 , E05B2047/0024 , E05B2047/0068 , E05C9/16 , Y10T70/5208 , Y10T70/5226 , Y10T70/527 , Y10T292/0834 , Y10T292/084 , Y10T292/0964 , Y10T292/1016 , Y10T292/57
摘要： A security lock arrangement (10) includes a carrier (40) to be mounted on a wing member. At least one latch bolt (28-34) is displaceably arranged relative to the carrier (40) between a retracted, unlocked position and an extended, locked position. An urging means (60) acts on the at least one latch bolt (28-34) for urging the latch bolt (28-34) to its extended, locked position. A drive means is mounted on the carrier (40) for driving the at least one latch bolt (28-34) at least into its retracted position against the action of the urging means (60). A displacement mechanism is interposed between the drive means and the at least one latch bolt (28-34), the displacement mechanism comprising a cam member (64) rotatably driven by the drive means, the cam member (64) acting on a follower of the at least one latch bolt (28-34), the cam member (64) having a maximum throw when the at least one latch bolt (28-34) is proximate its retracted position.
摘要翻译： 安全锁装置（10）包括安装在机翼构件上的托架（40）。 至少一个闩锁螺栓（28-34）在缩回的解锁位置和延伸的锁定位置之间相对于托架（40）可置换地布置。 推动装置（60）作用在至少一个闩锁螺栓（28-34）上，用于将闩锁螺栓（28-34）推动到其延伸的锁定位置。 驱动装置安装在载体（40）上，用于克服施力装置（60）的作用至少将其中的至少一个闩锁螺栓（28-34）驱动到其缩回位置。 位移机构设置在驱动装置和至少一个闩锁螺栓（28-34）之间，移动机构包括由驱动装置可旋转地驱动的凸轮构件（64），凸轮构件（64）作用在驱动装置 所述至少一个闩锁螺栓（28-34），当所述至少一个闩锁螺栓（28-34）接近其缩回位置时，所述凸轮构件（64）具有最大投射。
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