Group firing system for firework unit
    11.
    发明申请
    Group firing system for firework unit 失效
    烟花组团体射击系统

    公开(公告)号:US20040055493A1

    公开(公告)日:2004-03-25

    申请号:US10658579

    申请日:2003-09-09

    Inventor: Li Yi Li Gang

    CPC classification number: F42B4/24 C06C5/00 C06C5/06

    Abstract: Group firing system for firework unit, wherein it has 1-2 paper fuse tubes, which are assembled with other shot tubes. While both ends of the paper fuse tubes have male socket and female socket, so each firework unit could be connected to a firework group through soft fuse hose which contains a fuse inside. There are two firing systems, i.e. series connection and parallel connection.

    Abstract translation: 烟火单元组发射系统,其中有1-2个纸保险丝管,与其他射出管组装在一起。 虽然纸保险丝管的两端都有阳插座和母插座,但是每个烟花组件都可以通过内部有保险丝的软保险丝软管连接到烟花组。 有两个点火系统,即串联和并联。

    Multiple effect pyrotechnic shell
    12.
    发明授权
    Multiple effect pyrotechnic shell 有权
    多效烟火壳

    公开(公告)号:US06283033B1

    公开(公告)日:2001-09-04

    申请号:US09364594

    申请日:1999-07-30

    CPC classification number: F42B4/24 F42B4/14

    Abstract: A multiple effect pyrotechnic shell (20), having a lift chamber (22), primary break (24), secondary break (26), and a tertiary break (28) has a desired weight distribution to inhibit tumbling. The secondary break weight is less than the primary break weight, and the tertiary break weight is less than both the primary and secondary break weights. Thus, the center of gravity of the shell (20) is positioned below a midpoint of the shell height. A first timing fuse (46) extends from a lift charge (30) into a primary break charge (50A) of the primary break (24), and a primary internal timing fuse (64) extends from the primary break (24) to the secondary break (26). Further, a secondary internal timing fuse (70) extends from the secondary break (26) to the tertiary break (28). Fuse fragments (52) are preferably disbursed within the break hulls (48) to provide filler and add an additional effect to each break (24-28).

    Abstract translation: 具有提升室(22),初级断裂(24),次级断裂(26)和第三断层(28)的多重效果烟火外壳(20)具有所需的重量分布以抑制翻滚。 二次断裂重量小于主断裂重量,三次断裂重量小于初级和次级断裂重量。 因此,壳体(20)的重心位于壳高度的中点之下。 第一正时保险丝(46)从提升电荷(30)延伸到主断裂(24)的初级断开电荷(50A),并且主内部定时熔断器(64)从主断路(24)延伸到 二级休息(26)。 此外,次级内部定时保险丝(70)从次级断裂(26)延伸到第三断裂(28)。 保险丝碎片(52)优选地在断裂壳体(48)内分配以提供填料并且对每个断裂增加附加效果(24-28)。

    Pyrotechnic ignition apparatus
    13.
    发明授权

    公开(公告)号:US5739459A

    公开(公告)日:1998-04-14

    申请号:US543313

    申请日:1995-10-16

    CPC classification number: F41A19/68 F41A19/69 F41A33/04 F42B4/24 F42D1/055

    Abstract: A plurality of magazines each receive an array of pyrotechnic devices. The magazines are latched to a fire control and support assembly which automatically engages the fire control circuit to each device of each magazine. The circuit ignites all devices of all the magazines in a given serial sequence. The system, under control of an operator, when turned off, may be restarted at the beginning of a selected sequence, at the point where the last device was ignited and continue the sequence or at selected different portions of devices. Different size devices can be ignited by one circuit using different magazines all coupled to one unit. Safety features also include delay ignition after startup and sounding an alarm before any device is ignited. A CPU is enabled by a fire command signal and disabled by internal programmed instructions. The CPU is periodically enabled in a device ignition cycle by external timing signals initiated by the CPU when enabled.

    Securing apparatus for modules carried on aircraft, in particular for
flare launching modules
    14.
    发明授权
    Securing apparatus for modules carried on aircraft, in particular for flare launching modules 失效
    用于飞机上承载的模块的固定装置,特别是用于火炬发射模块的模块

    公开(公告)号:US4524670A

    公开(公告)日:1985-06-25

    申请号:US384097

    申请日:1982-06-01

    CPC classification number: F42B4/24 B64D1/08 F42B5/15

    Abstract: Located below an aircraft is a support rod (1) provided with female engagement members (10). Standard missile launcher modules are provided on their flat upper wall with counterpart male engagement members (20). The engagement members (10 and 20) cooperate in the manner of dovetails and for each module location, they are separated from each other according to the same geometric progression along the support rod (1) and the upper wall of the module (2). A device comprising a cam (27) and lever (273) makes it possible to ensure at the same time the translation necessary for locking of the dovetail, as well as the making of contact between the electrical connector members.

    Abstract translation: 位于飞机下方的是具有阴接合构件(10)的支撑杆(1)。 标准的导弹发射器模块在其平坦的上壁上设置有对应的公接合构件(20)。 接合构件(10和20)以燕尾形的方式配合,并且对于每个模块位置,它们沿着支撑杆(1)和模块(2)的上壁沿着相同的几何级联彼此分离。 包括凸轮(27)和杠杆(273)的装置使得可以同时确保锁定燕尾榫所需的平移以及电连接器构件之间的接触。

    PYROTECHNIC LAUNCH UNITS AND SYSTEMS
    19.
    发明公开

    公开(公告)号:US20240353208A1

    公开(公告)日:2024-10-24

    申请号:US18761043

    申请日:2024-07-01

    Abstract: A modular pyrotechnic launch unit includes a launch module, a first module, and a second module. The launch module includes a launch barrel. The first module is coupled in series to the launch module. The first module includes a first ignition state in which the first module ignites a pyrotechnic element that will then pass through the launch barrel. The first module also includes a first pass-through state in which the first module allows a pyrotechnic element ignited by another module to pass through the first module. The second module is coupled in series to the first module. The second module includes a second ignition state in which the second module ignites a pyrotechnic element that will then pass through the first module and through the launch barrel.

    Pyrotechnic launch units and systems

    公开(公告)号:US12044515B2

    公开(公告)日:2024-07-23

    申请号:US18192898

    申请日:2023-03-30

    Abstract: A modular pyrotechnic launch unit includes a launch module, a first module, and a second module. The launch module includes a launch barrel. The first module is coupled in series to the launch module. The first module includes a first ignition state in which the first module ignites a pyrotechnic element that will then pass through the launch barrel. The first module also includes a first pass-through state in which the first module allows a pyrotechnic element ignited by another module to pass through the first module. The second module is coupled in series to the first module. The second module includes a second ignition state in which the second module ignites a pyrotechnic element that will then pass through the first module and through the launch barrel.

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