System, in particular hand grenade

    公开(公告)号:US11629945B2

    公开(公告)日:2023-04-18

    申请号:US16924383

    申请日:2020-07-09

    发明人: Graf Helge

    摘要: In order to improve safety, particularly during transportation and/or storage, a system (10) is proposed which at least comprises a housing (13) an explosive (3) held therein which is initiated by a blasting cap (1), wherein a sleeve insert (2, 2′) in the housing (13) makes it possible for the blasting cap (1) to be removed from the explosive (3), in that the blasting cap (1) in the sleeve insert (2, 2′) is height-adjustable, so that the position of the blasting cap (1) relative to the explosive (3) can be changed. The system (10) may include a fuse head (11) which at least comprises a primer cap and possibly a delay line (14). The blasting cap (1) may be an integral part of the fuse head (11) and insulated therewith on the base.

    Time delay systems, methods, and devices

    公开(公告)号:US11598618B1

    公开(公告)日:2023-03-07

    申请号:US17496490

    申请日:2021-10-07

    IPC分类号: F42C15/184 F42C9/10 F42C15/31

    摘要: A damper system for a pyrotechnic time delay may comprise: a firing pin; a moveable housing defining a chamber therein; a fixed piston comprising a piston head disposed in the chamber, a first rod extending from the piston head axially outward of the moveable housing, and a second rod configured to fixedly couple to a housing; a first spring extending axially from the moveable housing to the firing pin; and a second spring extending axially from the moveable housing to the firing pin.

    Integrated thin film explosive micro-detonator

    公开(公告)号:US07497164B1

    公开(公告)日:2009-03-03

    申请号:US11981303

    申请日:2007-10-31

    申请人: Gerald Laib

    发明人: Gerald Laib

    IPC分类号: F42C15/184

    CPC分类号: F42C15/184

    摘要: A method of making a thin film explosive detonator includes forming a substrate layer; depositing a metal layer in situ on the substrate layer; and reacting the metal layer to form a primary explosive layer. The method and apparatus formed thereby integrates fabrication of a micro-detonator in a monolithic MEMS structure using “in-situ” production of the explosive material within the apparatus, in sizes with linear dimensions below about 1 mm. The method is applicable to high-volume low-cost manufacturing of MEMS safety-and-arming devices. The apparatus can be initiated either electrically or mechanically at either a single point or multiple points, using energies of less than about 1 mJ.

    Submunition member with laterally outwardly-movable target detection
device
    4.
    发明授权
    Submunition member with laterally outwardly-movable target detection device 失效
    子弹部件具有横向向外移动的目标检测装置

    公开(公告)号:US4848235A

    公开(公告)日:1989-07-18

    申请号:US227530

    申请日:1988-08-02

    IPC分类号: F42C15/184

    CPC分类号: F42C15/184

    摘要: A rotating submunition member which, subsequent to ejection from a carrier, incorporates a target detection device projecting outwardly beyond the wall contour of the member in an operating position; and a fuze arrangement for a detonator which is disposed interiorly of the wall of the submunition. The submunition member is equipped with a securing or safe-and-arm device in which the detonator is located on a movable mounting or holder, which is displaceable through the intermediary of a spring-elastic power element from the SAFE position of the detonator into its ARMED position, when a flyweight has tensioned the power element and the target detection device is displaced into its operative position projecting beyond the wall contour of the submunition member.

    摘要翻译: 旋转的子弹药构件,其在从载体排出之后,包括在操作位置向外突出超过构件的壁轮廓的目标检测装置; 以及设置在子弹药墙壁内部的雷管的引信安排。 子弹药件配备有固定或安全臂装置,其中雷管位于可移动的安装件或支架上,可移动的安装件或支架通过弹簧力弹性元件的中间位置从雷管的安全位置移动到其中 ARMED位置,当飞重物已经张紧功率元件并且目标检测装置移动到突出超过子弹药构件的壁轮廓的其操作位置时。

    Fuse for a satellite projectile
    5.
    发明授权
    Fuse for a satellite projectile 失效
    卫星射弹保险丝

    公开(公告)号:US4612858A

    公开(公告)日:1986-09-23

    申请号:US651445

    申请日:1984-09-17

    摘要: The invention relates to a fuse for a satellite projectile that is expelled from a carrier projectile. In order to maintain a defined ignition time within narrow tolerances, despite initial blind position of the fuse immediately after the expulsion of the satellite projectile, the firing pin 7 is centrally arranged in the interior of a key-shaped cover 12 which is movably disposed in the interior of a housing 1. The wall 12' of the cover 12 has a plurality of recesses 5' into which there engage a corresponding number of locking pins 5 mounted on sheet metal springs 4. These springs 4 are radially outwardly swingable and are secured to the housing 1. The locking pins 5 prevent an axial movement of the firing pin 7 during the safety inactive-position-period and prevent thereby a radial outward swinging of the detonator support 15 into the ignition position. The lockings pins 5 are capable of being swung outwardly in a radial direction out of the wall of the cover 12 only after the unwinding of a wound band 11, whereby the ignition process can be introduced.

    摘要翻译: 本发明涉及一种从载体抛射体排出的用于卫星射弹的保险丝。 为了在窄公差范围内保持定义的点火时间,尽管在卫星射弹被排出之后立即保险丝的初始盲位,击发销7居中布置在钥匙形盖12的内部,该钥匙形盖12的内部可移动地设置在 外壳1的内部。盖12的壁12'具有多个凹槽5',其中与其相配合的相应数量的锁定销5安装在金属弹簧4上。这些弹簧4径向向外可摆动并固定 锁定销5防止在安全非活动位置期间击发销7的轴向移动,从而防止雷管支撑件15径向向外摆动进入点火位置。 只有在卷绕带11的展开之后,锁定销5能够在径向方向上向外摆动出盖12的壁,由此可以引入点火过程。

    Warhead safety and ribbon chute holder
    6.
    发明授权
    Warhead safety and ribbon chute holder 失效
    弹头安全和带状滑槽架

    公开(公告)号:US4488488A

    公开(公告)日:1984-12-18

    申请号:US452487

    申请日:1982-12-23

    CPC分类号: F42C15/184 F42B10/56

    摘要: A device which serves as a safety mechanism for a warhead to prevent accital detonation thereof. The warhead includes a chute in the form of a ribbon which is folded thereon prior to flight of the warhead to a target. The device serves to releasably secure the ribbon chute to the warhead while also acting as a safety mechanism.

    摘要翻译: 用作弹头的安全机构以防止意外爆炸的装置。 弹头包括带状形式的滑槽,其在将弹头飞行到目标之前折叠在其上。 该装置用于将带状滑槽可释放地固定到弹头,同时还用作安全机构。

    Safety fuse with time and impact action
    8.
    发明授权
    Safety fuse with time and impact action 失效
    安全保险丝与时间和冲击行动

    公开(公告)号:US3630152A

    公开(公告)日:1971-12-28

    申请号:US3630152D

    申请日:1970-05-11

    发明人: ARNELL CLAES G

    摘要: A safety fuse, preferably usable for light grenades and shells having combined time and impact action, comprising a main piston containing elements of the ignition chain, said piston being displaced radially in a bore in the fuse casing by a driving spring, the time of this movement being prolonged by the vacuum created behind the ring-tightened piston, said vacuum being adjustable by leak holes having an arbitrary diameter. The fuse also contains a delay-composition-containing piston that is movable toward a fixed firing pin in a direction at an angle to the main piston. The delay piston has stopping means preventing its movement as long as the main piston has not reached its outward, fully armed position.

    Dual safety grenade fuze
    9.
    发明授权
    Dual safety grenade fuze 失效
    双重安全GREENDE FUZE

    公开(公告)号:US3618522A

    公开(公告)日:1971-11-09

    申请号:US3618522D

    申请日:1969-09-29

    申请人: HAMILTON WATCH CO

    发明人: HENDERSON JOHN E

    摘要: This invention relates to a dual safety time delayed fuze, useful, for example, in conventional grenades, and particularly to a biased barrier between the pyrotechnic delay charge and the fuze ignitor charge. The barrier contains a flash-hole which is normally held out of alignment with the fuze powder train by a barrier latch. Upon ignition of the delayed charge, a heat motor, activated by the burning of the charge, expands against the barrier latch, displacing it, thereby allowing the biasing element to drive the barrier flash-hole into alignment with the delay and the ignitor. The barrier flash-hole may optionally contain a lead charge to insure ignition of the fuze.

    Fuze setback and angular acceleration detent
    10.
    发明授权
    Fuze setback and angular acceleration detent 失效
    FUZE SETBACK AND ANGULAR ACCELERATION DETENT

    公开(公告)号:US3603259A

    公开(公告)日:1971-09-07

    申请号:US3603259D

    申请日:1968-06-26

    申请人: AVCO CORP

    发明人: WEBB GEORGE

    摘要: A safety fuse is shown incorporated in rocket propelled round of ammunition. Two complementary mechanisms act upon a slider to maintain it in a position wherein a primer charge therein is out of register with a firing pin. When the round of ammunition is discharged from a gun, linear and angular acceleration are effective on a locking ball to overcome the action of a spring and disengage the ball to overcome the action of a spring and disengage the ball from a notch in the slider''s guideway. Angular acceleration of the round causes the ball to roll into a laterally extending position in the slider. After discharge from the gun, centrifugal force disengages two plungers from the slider permitting it to travel laterally bringing the primer charge into register with the firing pin.