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    • 2. 发明申请
    • PROJECTILE FUZE
    • US20080078299A1
    • 2008-04-03
    • US11857535
    • 2007-09-19
    • Frank KienzlerWolfgang SchillingerWolfgang ZehnderReiner HennigEsther LauferSiegfried Paulini
    • Frank KienzlerWolfgang SchillingerWolfgang ZehnderReiner HennigEsther LauferSiegfried Paulini
    • F42C15/40
    • F42C15/31F42C15/188F42C15/40
    • A projectile fuze (12) having fuze electronics in which the time of flight (T) can be programmed, having a timer/counter which counts up to the programmed time of flight (T)—minus a defined time value (Δt)—and then charges an electrical firing circuit, and having a mechanical safety and arming unit (16) which switches a firing chain to the armed position after a specific time interval. The firing chain has an electrical detonator (24), a fuze needle (20), a piercing detonator (22) and a booster charge (26). The projectile fuze (12) has a pyrotechnic force element (14), which is interconnected with the fuze electronics and mechanically blocks the safety and arming unit (16) until the time of flight (T) minus the predetermined time value (Δt) is reached, after which the electrical firing circuit is charged and the safety and arming unit (16) is unlocked to the armed position by initiation of the force element (14).
    • 具有引信电子装置的射弹引信(12),其中可以对飞行时间(T)进行编程,具有计数到编程的飞行时间(T)的计时器/计数器 - 定义的时间值(Deltat),并且 然后对电击电路充电,并具有机械安全和布防单元(16),其在特定时间间隔之后将击发链路切换到布防位置。 发射链具有电雷管(24),引针(20),穿刺雷管(22)和增压器(26)。 射弹引信(12)具有烟火力元件(14),其与引信电子装置相互连接并机械地阻止安全和布防装置(16),直到飞行时间(T)减去预定时间值(Deltat)为止 到达之后,对该点火电路进行充电,并且通过启动该力元件(14)将安全和布防单元(16)解锁到布防位置。
    • 3. 发明授权
    • Projectile fuze with fuze electronics including a timer/counter
    • 引信电子包括定时器/计数器的射弹引信
    • US07614346B2
    • 2009-11-10
    • US11857535
    • 2007-09-19
    • Frank KienzlerWolfgang SchillingerWolfgang ZehnderReiner HennigEsther LauferSiegfried Paulini
    • Frank KienzlerWolfgang SchillingerWolfgang ZehnderReiner HennigEsther LauferSiegfried Paulini
    • F42C15/34F42C15/24
    • F42C15/31F42C15/188F42C15/40
    • A projectile fuze (12) having fuze electronics in which the time of flight (T) can be programmed, having a timer/counter which counts up to the programmed time of flight (T)—minus a defined time value (Δt)—and then charges an electrical firing circuit, and having a mechanical safety and arming unit (16) which switches a firing chain to the armed position after a specific time interval. The firing chain has an electrical detonator (24), a fuze needle (20), a piercing detonator (22) and a booster charge (26). The projectile fuze (12) has a pyrotechnic force element (14), which is interconnected with the fuze electronics and mechanically blocks the safety and arming unit (16) until the time of flight (T) minus the predetermined time value (Δt) is reached, after which the electrical firing circuit is charged and the safety and arming unit (16) is unlocked to the armed position by initiation of the force element (14).
    • 具有引信电子装置的射弹引信(12),其中可以对飞行时间(T)进行编程,具有计数到编程的飞行时间(T)的计时器/计数器 - 定义的时间值(Deltat),并且 然后对电击电路充电,并具有机械安全和布防单元(16),其在特定时间间隔之后将击发链路切换到布防位置。 发射链具有电雷管(24),引针(20),穿刺雷管(22)和增压器(26)。 射弹引信(12)具有烟火力元件(14),其与引信电子装置相互连接并机械地阻止安全和布防装置(16),直到飞行时间(T)减去预定时间值(Deltat)为止 到达之后,对该点火电路进行充电,并且通过启动该力元件(14)将安全和布防单元(16)解锁到布防位置。
    • 4. 发明授权
    • Safety and arming unit for the fuze of a projectile
    • 射弹引信的安全装备单位
    • US07699003B2
    • 2010-04-20
    • US11858742
    • 2007-09-20
    • Alexander ZinellReiner HennigRolf Kaden
    • Alexander ZinellReiner HennigRolf Kaden
    • F42C15/00
    • F42C15/29F42C15/40
    • A safety and arming unit with a safe separation distance device (14), which acts as a function of a free-flight incident flow and temperature, for the fuze (12) of a projectile (11), which fuze is hermetically sealed from environmental influences, has, as a measurement device for the cooling, as a function of the incident flow, of a conductor through which current passes, in the heating circuit (18) of a resistant heating element (16) which is fitted flat on the fuze casing surface (17), an electronic current measurement apparatus (21) which is connected upstream of an evaluation circuit (22), in order to ram a firing circuit. Two heating elements (16, 16″), which are fed in the same way, are preferably arranged one behind the other in the incident flow direction (15), and, additionally as an environmental temperature sensor, a comparison heating element (16′) which is not influenced by the incident flow (15). This results in a reliable safe separation distance, even for slow projectiles (11), without adversely affecting their aerodynamic behaviour and independently of the environmental atmosphere.
    • 对于引弹(11)的引弹(12),具有安全分离距离装置(14)的安全和布防装置(14)作为自由飞行事件流量和温度的函数,引信与环境密封 具有作为电流通过的导体的入射流的函数的测量装置,在电阻加热元件(16)的加热电路(18)中平坦地配置在引信上 壳体表面(17),连接在评估电路(22)的上游的电子电流测量装置(21),以便击发击发电路。 以相同的方式供给的两个加热元件(16,16“)优选地在入射流动方向(15)上一个接一个地布置,另外作为环境温度传感器,比较加热元件(16' ),不受事件流的影响(15)。 这导致了可靠的安全分离距离,即使对于慢速射弹(11),也不会对其空气动力学行为产生不利影响,而与环境气氛无关。
    • 6. 发明授权
    • Safety and arming unit for a spinning projectile fuze
    • 旋转射弹引信安全装备单位
    • US07661364B2
    • 2010-02-16
    • US11858770
    • 2007-09-20
    • Alexander ZinellReiner HennigAlfred Boos
    • Alexander ZinellReiner HennigAlfred Boos
    • F42C15/22
    • F42C15/40F42C15/26
    • A safety and arming unit (11) which is designed in particular for an electrical fuze circuit (27) does not reliably respond just to lateral loads on one side, but responds only to centrifugal forces produced by the spin during free flight, in that two contact pairs (22-23, 22-23) which are connected electrically in parallel with one another via rings (14, 15) and are arranged diametrically opposite one another on a cross-sectional plane of the fuze (12) are both no longer electrically conductively bridged at the same time by the bolt (17) because, just by virtue of the centrifugal force, both bolts (17) are simultaneously moved radially outwards from their short-circuit safety positions in their blind holes (16), which are oriented transversely with respect to the rotation axis (13).
    • 专门设计用于电气引信电路(27)的安全和布防装置(11)不能仅在一侧的侧向载荷上可靠地作出响应,而只响应自由飞行期间旋转产生的离心力, 通过环(14,15)彼此并联连接并在引信(12)的横截面上沿径向相对布置的接触对(22-23,22-23)不再是 同时通过螺栓(17)导电桥接,因为只要借助离心力,两个螺栓(17)同时从其盲孔(16)中的短路安全位置径向向外移动, 相对于旋转轴线(13)横向定向。
    • 8. 发明申请
    • Safety and Arming Unit for a Spinning Projectile Fuze
    • 旋转喷射器的安全和装备单元
    • US20080210117A1
    • 2008-09-04
    • US11858770
    • 2007-09-20
    • Alexander ZinellReiner HennigAlfred Boos
    • Alexander ZinellReiner HennigAlfred Boos
    • F42C15/22
    • F42C15/40F42C15/26
    • A safety and arming unit (11) which is designed in particular for an electrical fuze circuit (27) does not reliably respond just to lateral loads on one side, but responds only to centrifugal forces produced by the spin during free flight, in that two contact pairs (22-23, 22-23) which are connected electrically in parallel with one another via rings (14, 15) and are arranged diametrically opposite one another on a cross-sectional plane of the fuze (12) are both no longer electrically conductively bridged at the same time by the bolt (17) because, just by virtue of the centrifugal force, both bolts (17) are simultaneously moved radially outwards from their short-circuit safety positions in their blind holes (16), which are oriented transversely with respect to the rotation axis (13).
    • 专门设计用于电气引信电路(27)的安全和布防装置(11)不能仅在一侧的侧向载荷上可靠地作出响应,而只响应自由飞行期间旋转产生的离心力, 通过环(14,15)彼此并联连接并且在引信(12)的横截面上沿径向相对布置的接触对(22-23,22-23)不再是 同时通过螺栓(17)导电桥接,因为只要借助离心力,两个螺栓(17)同时从其盲孔(16)中的短路安全位置径向向外移动, 相对于旋转轴线(13)横向定向。
    • 9. 发明申请
    • Safety and Arming Unit for the Fuze of a Projectile
    • 弹射装置的安全和装备单位
    • US20080210116A1
    • 2008-09-04
    • US11858742
    • 2007-09-20
    • Alexander ZinellReiner HennigRolf Kaden
    • Alexander ZinellReiner HennigRolf Kaden
    • F42C15/00
    • F42C15/29F42C15/40
    • A safety and arming unit with a safe separation distance device (14), which acts as a function of a free-flight incident flow and temperature, for the fuze (12) of a projectile (11), which fuze is hermetically sealed from environmental influences, has, as a measurement device for the cooling, as a function of the incident flow, of a conductor through which current passes, in the heating circuit (18) of a resistant heating element (16) which is fitted flat on the fuze casing surface (17), an electronic current measurement apparatus (21) which is connected upstream of an evaluation circuit (22), in order to ram a firing circuit. Two heating elements (16, 16″), which are fed in the same way, are preferably arranged one behind the other in the incident flow direction (15), and, additionally as an environmental temperature sensor, a comparison heating element (16′) which is not influenced by the incident flow (15). This results in a reliable safe separation distance, even for slow projectiles (11), without adversely affecting their aerodynamic behaviour and independently of the environmental atmosphere.
    • 对于引弹(11)的引弹(12),具有安全分离距离装置(14)的安全和布防装置(14)作为自由飞行事件流量和温度的函数,引信与环境密封 具有作为电流通过的导体的入射流的函数的测量装置,在电阻加热元件(16)的加热电路(18)中平坦地配置在引信上 壳体表面(17),连接在评估电路(22)的上游的电子电流测量装置(21),以便击发击发电路。 以相同的方式进给的两个加热元件(16,16“)优选地在入射流动方向(15)上一个接一个地布置,另外作为环境温度传感器,比较加热元件(16 '),不受事件流的影响(15)。 这导致了可靠的安全分离距离,即使对于慢速射弹(11),也不会对其空气动力学行为产生不利影响,而与环境气氛无关。