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    • 1. 发明授权
    • Fixing device for fixing an actuation device with push-push kinematics
    • 用于固定具有推 - 推运动学的致动装置的固定装置
    • US08998271B2
    • 2015-04-07
    • US13949288
    • 2013-07-24
    • Illinois Tool Works Inc.
    • Christian Beck
    • E05C5/02B60K15/04E05C19/00E05F1/10
    • B60K15/0406B60K15/04E05F1/105E05Y2900/534Y10T292/0863Y10T292/25Y10T403/7007
    • Disclosed is a fixing device for fixing an actuation device with push-push kinematics on a component of a motor vehicle. The fixing device includes a housing with a guiding element and a locking recess on its outer surface, an opening in the component for inserting the actuation device, a guiding element on the component, and a locking projection on the component. The guiding elements of the actuation device and the component corporate such that the actuation device is guided into the opening in a predetermined rotational position, and the locking projection and the locking recess lock with each other upon the actuation device being inserted fully into the opening in the predetermined rotational position, and thus fix the actuation device on the component. The locking can be released again by rotating of the actuation device out of the predetermined rotational position.
    • 公开了一种用于将具有推 - 推运动学的致动装置固定在机动车辆的部件上的固定装置。 定影装置包括具有引导元件的壳体和在其外表面上的锁定凹部,用于插入致动装置的部件中的开口,部件上的引导元件以及部件上的锁定突起。 致动装置和部件公司的引导元件使得致动装置在预定旋转位置被引导到开口中,并且当致动装置完全插入开口中时,锁定突起和锁定凹槽彼此锁定 预定的旋转位置,从而将致动装置固定在部件上。 可以通过使致动装置旋转超出预定旋转位置来再次释放锁定。
    • 8. 发明申请
    • Device and method for the detachable connection of structural parts, in particular in an aircraft
    • 结构部件可拆卸连接的装置和方法,特别是在飞机上
    • US20090223261A1
    • 2009-09-10
    • US12380065
    • 2009-02-23
    • Herbert SteinbeckKonstantin Wagner
    • Herbert SteinbeckKonstantin Wagner
    • E05B65/08
    • F16B5/0084E05B17/0025E05B65/006E05B65/0817E05C3/045F16B2/185Y10S292/55Y10T70/5164Y10T292/0863Y10T292/0886Y10T292/1039Y10T292/1043
    • The invention relates to a device (10) for the detachable connection of structural parts (80, 84) in an aircraft, comprising a clamping lever arrangement (12) associated with a first structural part (80) and a clamping pin (14) associated with a second structural part (84), wherein the clamping lever arrangement (12) comprises an eccentric shaft (20) rotatably mounted about a rotation axis (A) on the first structural part (80), a clamping lever (16) mounted eccentrically and swivellably with respect to the eccentric shaft (20), and a driving bushing (18) rotatably mounted relative to the eccentric shaft (20) about the rotation axis (A) and coupled in a geared manner to the clamping lever (16), wherein the clamping lever arrangement (12) can furthermore be displaced between a release position, a readiness position and a locking position, wherein the clamping lever (16) in the release position releases the clamping pin (14) and wherein the clamping lever (16) in the locking position engages the locking pin (14) in an interlocking positive manner on account of a relative rotation of the eccentric shaft (20) and driving bushing (18) as well as the clamping lever (16).
    • 本发明涉及一种用于飞行器中结构部件(80,84)的可拆卸连接的装置(10),包括与第一结构部件(80)相关联的夹紧杆装置(12)和与之相关联的夹紧销(14) 具有第二结构部件(84),其中所述夹紧杆装置(12)包括绕所述第一结构部件(80)上的旋转轴线(A)可旋转地安装的偏心轴(20),偏心安装的夹紧杆(16) 并且相对于所述偏心轴(20)可旋转地移动;以及驱动衬套(18),所述驱动衬套(18)围绕所述旋转轴线(A)相对于所述偏心轴(20)可旋转地安装并且以齿轮方式联接到所述夹紧杆(16) 其中所述夹紧杆装置(12)还可以在释放位置,准备位置和锁定位置之间移动,其中处于释放位置的夹紧杆(16)释放夹紧销(14),并且其中夹紧杆(16) )在锁定位置 由于偏心轴(20)和驱动套管(18)以及夹紧杆(16)的相对旋转,因此锁定销(14)以互锁的方式进行。
    • 9. 发明授权
    • Binary coded key and tamper resistant latch
    • 二进制编码密钥和防篡改锁存器
    • US07441427B2
    • 2008-10-28
    • US11855796
    • 2007-09-14
    • James H. Vickers
    • James H. Vickers
    • E05B65/06
    • E05C3/042E05B17/0025E05B17/04E05B35/008E05C5/00Y10T70/531Y10T70/5314Y10T70/7593Y10T70/7853Y10T70/7921Y10T70/7932Y10T292/0863Y10T292/0864Y10T292/0887Y10T292/0891
    • A latch has a bushing which has at least one bushing projection or means for preventing insertion of an unauthorized tool to rotate a latch actuator of the latch. Only a key having an outer key recess which can mate with bushing projection on the bushing permits insertion of the key. The cap subassembly of the latch is provided with projections which are of a size and so positioned as to correspond with the internal recesses of the key so as to allow the cap subassembly to enter into the bore of the key and permit a mating engagement of internal recesses on the key and projections on the cap subassembly. Because cap portion rotates freely on top of the cap subassembly which is the part of the cap driven by the key, the arrangement makes it impossible, or at least very difficult, to rotate the shaft and in turn the pawl by means of a tool which rotates the cap portion.
    • 闩锁具有衬套,其具有至少一个衬套突起,用于防止未经授权的工具插入以使锁闩的闩锁致动器旋转。 只有具有能够与衬套上的衬套突起配合的外键凹槽的键允许插入钥匙。 闩锁的盖子组件设置有突起,突出部具有尺寸并且定位成与钥匙的内部凹部对应,以便允许帽子组件进入钥匙的孔中并允许内部的配合接合 钥匙上的凹槽和帽子组件上的突起。 由于盖部分在帽子组件的顶部自由旋转,帽子组件是由钥匙驱动的盖的一部分,所以该装置使得不可能或至少非常困难地使用旋转轴的工具旋转所述棘爪 帽部分。
    • 10. 发明授权
    • Sealable casing having a quarter-turn closing arrangement
    • 密封套具有四分之一圈关闭装置
    • US06789691B2
    • 2004-09-14
    • US10084931
    • 2002-03-01
    • Michel Jean MartinPhilippe Roger Rouix
    • Michel Jean MartinPhilippe Roger Rouix
    • B65D4106
    • B01D29/96B01D35/30B01D2201/4015Y10T292/0863
    • A sealable casing having a quarter-turn closing arrangement including a tubular body defining an orifice at one end having radially projecting arcuate members and clearances formed along an inner periphery thereof. The casing further includes a cap having radially projecting arcuate members and clearances formed along its inner periphery that are complementary to arcuate members and clearances of the tubular body. A hoop member is connected to the cap and includes a plurality of extensions that are biased by at least one resilient member connected to the cap so as to press against the inner Periphery of the tubular body. The extensions are connected to a drive handle mounted underneath a bail of the cap and cooperate with the at least one resilient member.
    • 具有四分之一转闭合装置的可密封壳体包括管状体,其在一端限定孔口,其具有径向突出的弓形构件和沿其内周形成的间隙。 壳体还包括具有沿着其内周形成的径向突出的弓形构件和间隙的盖,其与弓形构件和管状体的间隙互补。 环形构件连接到盖并且包括多个延伸部,其由连接到盖的至少一个弹性构件偏压,以压靠管状体的内周。 延伸部连接到安装在盖的吊环下方的驱动手柄,并与至少一个弹性构件配合。