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    • 3. 发明授权
    • Conductive energy weapon ammunition
    • 导弹能量武器弹药
    • US08733251B1
    • 2014-05-27
    • US13735933
    • 2013-01-07
    • Steven AbboudChi-Myin Chang
    • Steven AbboudChi-Myin Chang
    • F41B15/04F41B11/06H05C1/00F41H13/00
    • F42B5/02F41H13/0012F41H13/0025F41H13/0031F42B5/025F42B5/03F42B5/067F42B5/08F42B5/145F42B5/16F42B5/26F42B5/285F42B5/307F42B5/313F42B12/46
    • Ammunition for a conductive energy weapon. A receptacle includes a cavity accessible through each of a first opening in a first face of the receptacle, a second opening in the first face of the receptacle, a third opening in a second face of the receptacle and a fourth opening in a third face of the receptacle. A propellant unit is included within the cavity proximate the second opening and a projectile is included within the cavity proximate the second opening. A housing is coupled to at least the second face and the third face of the receptacle and is further configured to couple to the conductive energy weapon. The propellant unit releases a propellant into the cavity, in a direction substantially opposite the projectile's direction of flight, in response to a trigger pull of the conductive energy weapon, and the cavity directs the propellant in the projectile's direction of flight.
    • 导弹能武器弹药。 容器包括通过容器的第一面中的第一开口中的每一个可容纳的腔,在容器的第一面中的第二开口,在容器的第二面中的第三开口和第三面中的第四开口 容器 推进剂单元包括在靠近第二开口的腔内,并且射弹被包括在靠近第二开口的腔内。 壳体至少耦合到容器的第二面和第三面,并且还被配置成耦合到导电能量武器。 推进剂单元响应于导电能量武器的触发拉动,沿与弹丸的飞行方向大致相反的方向将推进剂释放到空腔中,并且空腔将推进剂引导到射弹的飞行方向。