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    • 1. 发明授权
    • Ski binding
    • SKI BINDING
    • US5213358A
    • 1993-05-25
    • US806294
    • 1991-12-13
    • Wolfgang Badura
    • Wolfgang Badura
    • A63C9/08A63C9/088
    • A63C9/0802A63C9/088
    • An automatically detachable ski binding includes spaced apart and interconnected toe and heel portions mounted on a ski for holding a ski boot in place thereon. The ski binding includes a mechanical shoe clamping and release system and an electronic controller, the heel portion of the binding including a pivotable clamp with which a spring and a probe engage. The binding is designed in such a manner that the point of application of the probe on the clamp lies between the point of application of the spring on the clamp and the transverse axis about which the clamp pivots, and that the distance between the point of application of the probe and that of the spring and/or the prestress of the spring are selected in such a manner that in the point of application of the probe would specify the relationship, are the same between the desired release values of the vertical and the horizontal torque such that the two different torque values effect the same linear shifting movement of the probe.
    • 可自动拆卸的滑雪板装置包括安装在滑雪板上的间隔开和相互连接的趾部和脚跟部分,用于将滑雪靴固定在其上。 滑雪板装置包括机械鞋夹紧和释放系统以及电子控制器,所述装订的所述后跟部分包括可枢转的夹具,弹簧和探针通过所述可枢转的夹具接合。 装订装置的设计方式是使夹具上的探针的施加点位于夹具上弹簧的施加点和夹紧器枢转的横向轴线之间,并且施加点之间的距离 探针的弹簧和/或弹簧的预应力的选择方式是这样一种方式,使得在探头的应用点将指定关系时,垂直和水平的期望释放值之间是相同的 扭矩使得两个不同的扭矩值影响探头的相同的线性移动运动。
    • 3. 发明授权
    • Device for producing a decoy cloud, in particular an infrared decoy cloud
    • 用于制造诱饵云的装置,特别是红外诱饵云
    • US4621579A
    • 1986-11-11
    • US743949
    • 1985-06-12
    • Wolfgang BaduraGerhard GrauAxel WideraKurt Adamek
    • Wolfgang BaduraGerhard GrauAxel WideraKurt Adamek
    • F42B4/24F42B5/15F42B13/44
    • F42B5/15F42B4/24
    • Device for producing a series of consecutive decoy clouds, in particular infrared decoy clouds which move progressively away from the actual target, in which several projectiles (A, B, C, D, E, F, G) are arranged within a thin walled discharge tube (1), each projectile is practically of identical construction and has a separate ignition disintegrator unit (10) for disintegrating it and for igniting and scattering the combustible charge (18) to form a decoy cloud, a separate ejection chamber (27) provided with a propellant charge cartridge (28) is provided on each projectile, each propellant charge cartridge (28) can be ignited via a separate electrically actuated ignition lead (5) by means of a command controlled ignition distributor unit (69) and each projectile has a separate percussion fuse (47) for the ignition disintegrator unit (10) which can be actuated by releasing its safety device (360 mechanically, its safety device (36) only being released after ignition of the propellant charge cartridge (28) with opening of the ejection chamber (27) and after the projectile has left the discharge tube (1) and due to the acceleration of the projectile.
    • 用于产生一系列连续诱饵云的设备,特别是在实际目标中逐渐移动的红外诱饵云,其中多个抛射体(A,B,C,D,E,F,G)布置在薄壁放电 管(1),每个射弹实际上具有相同的结构,并且具有用于分解它并且用于点燃和散射可燃炸药(18)以形成诱饵云的单独的点火解体器单元(10),提供单独的喷射室(27) 在每个抛射体上设置有推进剂充电盒(28),每个推进剂充电盒(28)可以通过指令控制的点火分配器单元(69)经由单独的电致动点火引线(5)点火,并且每个抛射体具有 用于点火解体器单元(10)的单独的冲击式保险丝(47),其可以通过释放其安全装置(360机械地启动,其安全装置(36))仅在推进剂c点燃之后被释放 具有喷射室(27)的开口并且在射弹离开放电管(1)并且由于射弹加速之后的喷射墨盒(28)。
    • 4. 发明授权
    • Incendiary warhead
    • 燃烧弹头
    • US4173931A
    • 1979-11-13
    • US879599
    • 1978-02-21
    • Alois SchiesslGeorg PraehauserWolfgang BaduraWolfgang Trede
    • Alois SchiesslGeorg PraehauserWolfgang BaduraWolfgang Trede
    • F42B10/12F42B10/14F42B12/44F42B12/58F42B13/44
    • F42B10/12F42B10/14F42B12/44F42B12/58
    • An incendiary warhead comprises a destructible body carrying a plurality of stacked incendiaries. Each incendiary comprises a housing containing a compressed three-part icendiary filling. The filling comprises a flame substance for forming an intense flame, a thermit unit for forming a red-hot slag, and a combustion transfer substance which projects into both the flame substance and the thermit substance to be ignited by the former and ignite the latter. A tail unit is mounted at a top end of the housing to control the rate of descent of the incendiary. The tail comprises a hook, a pair of chains connected to the hook, and a vane connected to the free end of each chain. An anchor point extends from a bottom end of the housing and is in the shape of an arrowhead having barbed side edges.
    • 燃烧弹头包括携带多个堆叠燃烧器的可破坏物体。 每个燃烧器包括一个包含压缩三部分燃料填充物的壳体。 填充物包括用于形成强烈火焰的火焰物质,用于形成红热炉渣的热化器单元,以及将火焰物质和物质物质投射到被燃烧器点燃并点燃火焰物质的燃烧转移物质。 尾座装在机壳的顶端,以控制燃烧器的下降速度。 尾部包括钩,连接到钩的一对链和连接到每个链的自由端的叶片。 锚定点从壳体的底端延伸并且具有带倒刺侧边缘的箭头的形状。
    • 5. 发明授权
    • Missile with detachable drag chute
    • 导弹与可拆卸的滑槽
    • US5370057A
    • 1994-12-06
    • US181912
    • 1994-01-18
    • Wolfgang BaduraChristian Falter
    • Wolfgang BaduraChristian Falter
    • F42B10/56F42B12/62F42B15/10
    • F42B10/56F42B12/625
    • A missile includes, as viewed successively in flight direction, a booster, a folded drag chute in a parachute housing, a cruise engine and a warhead. The booster is detachable from the drag chute before the opening of the drag chute and the drag chute is detachable from the cruise engine upon the activation of said cruise engine. The drag chute is accommodated in a parachute housing that is closed toward the booster and is open toward the cruise engine to which the booster is connected via a positive locking releasable due to axial tensile force. A separating charge for detaching the booster from the parachute housing is arranged between the booster and the base of the parachute housing at the booster side. The booster is connected to the parachute housing via a mechanical parachute release mechanism for releasing the drag chute from the parachute housing with a delay in comparison to the ignition of the separating charge.
    • 导弹在飞行方向上连续观察,包括升降机,降落伞壳体中的折叠式滑槽,巡航发动机和弹头。 在启动所述巡航发动机之前,所述增压器可以在所述拖曳滑槽打开之前与所述拖曳滑槽分离,并且所述拖曳滑槽可从所述巡航发动机上拆卸。 拖曳滑槽被容纳在降落伞壳体中,该降落伞壳体朝向助推器关闭,并且通过由于轴向拉力可释放的正向锁定而朝向升降机连接到的巡航发动机打开。 用于将增压器从降落伞壳体上分离的分离装置设置在助力器与助力器侧的降落伞壳体的底座之间。 增压器经由机械降落伞释放机构连接到降落伞壳体,用于与降落伞壳体的点火相比延迟地从降落伞壳体释放拖曳滑槽。
    • 6. 发明授权
    • Projectile for a defensive projecting device
    • 防弹投射装置的射弹
    • US5272981A
    • 1993-12-28
    • US907043
    • 1992-07-01
    • Wolfgang BaduraFritz Greindl
    • Wolfgang BaduraFritz Greindl
    • F42B5/155F42B12/68F42C7/12F42B12/48
    • F42C7/12F42B12/68F42B5/155
    • A projectile to be fired by a electric ignition defensive projector attached to an object to be defended has a propellant charge and an active charge and ignition devices for igniting the propellant and active charges. The active charge-ignition device is a mechanical ignition device including a firing pin and a firing pin spring. The mechanical ignition device is tensioned and released by a grappling line which is connected to the projector or a part of a projectile which remains in the projector, and is likewise connected to the firing pin. After the projectile has been fired and when it has travelled through a range of fire that corresponds to the length of the grappling line, then the firing pin spring is tensioned by the now taut grappling line and the firing pin is subsequently released which then ignite the active charge of the projector via a percussion cap and a pyrotechnical igniter train.
    • 被安装在待防御物体上的电动点火防护投影机发射的射弹具有推进剂装药和用于点燃推进剂和主动充电的主动充电和点火装置。 有源充电点火装置是包括击发销和撞针弹簧的机械点火装置。 机械点火装置被连接到投影仪的抓斗线张紧和释放,或者投影机中保留的投射器的一部分,并且同样地连接到击发销。 在射弹被射击之后,当它经过对应于抓斗线的长度的一系列火焰行进时,射击弹簧被现在紧紧抓紧的线张紧,并且击发销随后被点燃, 通过打击乐帽和烟火点火器列车对投影机进行主动充电。
    • 7. 发明授权
    • Contact head
    • 接触头
    • US4370929A
    • 1983-02-01
    • US175024
    • 1980-08-04
    • Wolfgang SteinickeWolfgang BaduraAlois SchiesslWerner WeinzierlHartmut Krone
    • Wolfgang SteinickeWolfgang BaduraAlois SchiesslWerner WeinzierlHartmut Krone
    • F42B5/08F42C19/12F42B9/08
    • F42C19/12F42B5/08
    • A contact head for a projectile which is capable of being fired from an electrically actuable launcher comprises a solid metal core formed on one side with a recess for constituting a propellent charge chamber in which are located a propellent charge and a primer capsule. The recess is closed by a base plate having breakage points for the egress of gases generated by ignition of the charge. The part of the core surrounding the recess is formed with first and second sets of bores spaced equiangularly about the axis of the core for receiving connecting screws for connecting the, contact head to a projectile and for receiving fixing screws for fixing the base plate to the core, respectively. An elastic protective member coaxially surrounds the head and is preferably subdivided into three rings, e.g. of rubber, which carry two metallic contact rings connected to the primer capsule by firing circuit wires. The use of a solid metal core as opposed to plastics members used in the prior art provides better control of the flight of the projectile and enables the contact head to withstand more rigorous conditions.
    • 用于能够从可电致动的发射器发射的射弹的接触头包括形成在一侧的实心金属芯,其具有用于构成推进剂充电室的凹部,其中位于推进剂装料和底漆胶囊中。 该凹槽由具有用于通过点燃点火产生的气体出口的断裂点的基板封闭。 围绕凹部的芯部的一部分形成有围绕芯的轴线等角度地隔开的第一和第二组孔,用于接收连接螺钉,用于将接触头连接到抛射体并用于接收用于将基板固定到 核心。 弹性保护构件同轴地围绕头部,并且优选地分为三个环,例如, 的橡胶,其通过点火电路线承载连接到底漆胶囊的两个金属接触环。 与现有技术中使用的塑料构件相反的实心金属芯的使用提供了对射弹飞行的更好的控制,并使得接触头能够承受更严格的条件。