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1. 发明申请

WO2009147660A2 KEY, LOCK AND LOCKING MECHANISM 审中-公开
标题翻译：钥匙，锁定和锁定机构
公开(公告)号：WO2009147660A2
公开(公告)日：2009-12-10
申请号：PCT/IL2009000540
申请日：2009-06-01
申请人： HAVIV ASHER , TORGEMAN ERIC
发明人： HAVIV ASHER , TORGEMAN ERIC
IPC分类号： E05B35/00 , E05B19/08 , E05B27/00
CPC分类号： E05B35/003 , E05B19/0058 , E05B27/0017 , E05B27/0042 , Y10T29/49826 , Y10T70/7559 , Y10T70/7802 , Y10T70/7819 , Y10T70/7825 , Y10T70/7842 , Y10T70/7859 , Y10T70/7864 , Y10T70/787 , Y10T70/7881
摘要： A key blank comprises a shaft and a head connected to the shaft, the shaft including first and second surface that are oppositely facing, wherein the surfaces are configured to include combination elements to operate a lock and a pair of coaxial operating elements, wherein one element of the pair is operative from the first surface of the shaft and the other element of the pair is operative from the second surface of the shaft, and wherein at least one of the operative elements is a resilient element mounted inside a bore provided in the shaft, wherein the resilient element is operative to exert a compressive force on a pin mechanism of the lock in response to the operative engagement and thereby release the pin mechanism from a lock position, without requiring any pressure on the coaxial element on the other side.
摘要翻译：钥匙坯件包括轴和连接到所述轴的头部，所述轴包括相对面对的第一和第二表面，其中所述表面构造成包括组合元件以操作锁和一对同轴操作元件，其中一个元件所述一对的所述第一表面从所述轴的第一表面起作用，并且所述一对的另一个元件从所述轴的第二表面操作，并且其中所述操作元件中的至少一个是安装在设置在所述轴中的孔内的弹性元件其中所述弹性元件可操作以响应于所述操作接合而施加在所述锁的销机构上的压缩力，从而将所述销机构从锁定位置释放，而不需要在所述另一侧上的所述同轴元件上的任何压力。

2. 发明申请

WO02055382A2 LOCK SYSTEM FOR AIRCRAFT COCKPIT DOOR 审中-公开
标题翻译：航空器门锁系统
公开(公告)号：WO02055382A2
公开(公告)日：2002-07-18
申请号：PCT/IL0200049
申请日：2002-01-16
申请人： A L S AVIAT LOCKING SYSTEMS LT , HAVIV ASHER
发明人： HAVIV ASHER
IPC分类号： B64C1/14 , B64D45/00 , B64C
CPC分类号： B64C1/1469 , B64C2001/009 , B64D45/0015
摘要： The present invention is a lock system particularly suited to the requirements of restricting access to an aircraft cockpit, although the invention may equally be applied to a range of other applications. Disclosed is a lock system including a door mounted locking bolt that may be actuated by a handle on the cockpit side of the door and by a key on the cabin side of the door. The key actuator may be disabled from the cockpit side of the door. The bolt is configured to engage a doorframe mounted bolt-receiver the bolt and the bolt-receiver thereby interlocking in a way that holds the bolt in the bolt-receiver in the advent of attempted forced entry to the cockpit, such as by a terrorist. The doorplane elements are further configured so as to automatically release the bolt and allow the door to open freely in the case of a sudden differential is cockpit and cabin air pressure. The automatic release may also be activated a manual switch or by a system override.
摘要翻译：本发明是特别适合于限制对飞行器驾驶舱的通道的要求的锁定系统，尽管本发明可以同样适用于一系列其他应用。公开了一种锁系统，其包括门安装的锁定螺栓，其可以由门的驾驶舱侧上的手柄和门的舱室侧上的钥匙致动。钥匙执行器可以从门的驾驶舱侧禁用。螺栓被构造成接合门框安装的螺栓 - 接收器，螺栓和螺栓 - 接收器因此在将试图强制进入驾驶舱（例如恐怖分子）的情况下将螺栓保持在螺栓接收器中的方式互锁。门面元件还被构造成在驾驶舱和客舱空气压力突然差异的情况下自动释放螺栓并允许门自由地打开。也可以通过手动开关或系统覆盖来激活自动释放。

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