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    • 1. 发明授权
    • Propellant charge container
    • 推进剂充电容器
    • US4949640A
    • 1990-08-21
    • US710144
    • 1985-03-11
    • Karlheinz Reinelt
    • Karlheinz Reinelt
    • F42B5/38
    • F42B5/38
    • The invention relates to a propellant charge container for receiving loose propellant charge powders. The propellant charge container consists of at least two separate telescopically mounted cylindrical parts which are mutually rotatable relative to each in the peripheral direction. The propellant charge container has a substantially cylindrical shape. The cylindrical container parts forming the container are coupled to each via their mutually overlapping regions. Each of the respective overlapping regions of the parts forming the container have at least one opening, which openings can be mutually aligned to form a filling opening. When these openings are misaligned the filling opening is closed. The overlapping regions of the cylindrical parts have one or more annular corrugations which interengage to form a firm coupling between the cylindrical parts forming the propellant charge container. Both of the end faces of the cylindrical parts forming the container have indentations for permitting a radially and axially play-free loading. The novel propellant charge container of this invention provides for significant manufacturing savings and accelerates the loading process.
    • 本发明涉及用于接收松散推进剂装料粉末的推进剂装料容器。 推进剂装料容器由至少两个单独的可伸缩安装的圆柱形部件组成,其相对于沿周向方向各自相互旋转。 推进剂装料容器具有基本上圆柱形的形状。 形成容器的圆柱形容器部分经由其相互重叠的区域连接到每个。 形成容器的部件的各个重叠区域中的每一个具有至少一个开口,这些开口可以相互对准以形成填充开口。 当这些开口不对准时,填充开口关闭。 圆柱形部分的重叠区域具有一个或多个环形波纹,这些波纹与形成推进剂充电容器的圆柱形部件之间形成牢固的联接。 形成容器的圆柱形部件的两个端面具有用于允许径向和轴向无游隙加载的凹陷。 本发明的新型推进剂装料容器提供显着的制造节省并加速装载过程。
    • 7. 发明授权
    • Liquid propellant
    • 液体推进剂
    • US5047098A
    • 1991-09-10
    • US925520
    • 1986-10-28
    • Wolfram WittKarlheinz Reinelt
    • Wolfram WittKarlheinz Reinelt
    • C06B25/36C06B47/00
    • C06B25/36C06B47/00
    • A liquid propellant for use in a propellant medium combustion chamber of a gun barrel weapon. The liquid propellant is completely decomposed and its combustion velocity is adjusted to the requirements of the weapon and projectile so as to provide a preponderantly oscillation-free plateau-like gas pressure development curve. The liquid propellant consist of a monergolic or nonhypergolic liquid propellant substance which includes up to 40% by weight of additives, preferably in the form of inhibitors. As starting material there are used aliphatic compositions, preferably nitrated alcanes or nitrates of alcanes, for example, isopropylinitrate or nitromethane. As inhibitors for moderating the burning there are used alcohols, such as methylalcohol or isopropylalcohol, which are admixed to the starting material. The inhibitors and/or liquid propellant include additional additives which act as radical binders which preponderantly prevent gas pressure oscillations and effect a plateau-like gas pressure development curve.
    • 用于枪管武器的推进剂介质燃烧室的液体推进剂。 液体推进剂完全分解,其燃烧速度根据武器和射弹的要求进行调节,从而提供无振荡的无平台状气体压力发展曲线。 液体推进剂由单一或非高压液体推进剂物质组成,其包含至多40重量%的添加剂,优选以抑制剂的形式。 作为起始原料,使用脂族组合物,优选硝化的烷烃或丙烷的硝酸盐,例如硝酸异丙酯或硝基甲烷。 作为缓和燃烧的抑制剂,使用与原料混合的醇,如甲醇或异丙醇。 抑制剂和/或液体推进剂包括作为自由基粘合剂的其它添加剂,其主要地防止气体压力振荡并影响平台状气体压力显影曲线。
    • 8. 发明授权
    • Gun barrel weapon with liquid propellant charge
    • 枪炮武器用液体推进剂充电
    • US4574681A
    • 1986-03-11
    • US480686
    • 1983-03-31
    • Edwin GundrumKarlheinz Reinelt
    • Edwin GundrumKarlheinz Reinelt
    • F41A1/04F41F1/06
    • F41A1/04
    • A gun barrel weapon for firing a projectile by means of a liquid propellant medium. The weapon includes a coaxial first member which defines a propellant medium combustion chamber. This first member also functions as a breech or breech block. A second member defining a projectile chamber is disposed between the first member and the gun barrel. The combustion chamber is adapted to hold a liquid propellant medium and includes a neck portion of narrowed cross-section which throttingly communicates with the projectile chamber. The first member also includes a plurality of through-bores which form conduits between the projectile chambers and the combustion chamber.
    • 用于通过液体推进剂介质发射抛射物的枪管武器。 该武器包括一个同轴的第一构件,其限定了推进剂介质燃烧室。 这个第一个成员也用作后膛或后膛。 定义射弹室的第二构件设置在第一构件和枪管之间。 燃烧室适于容纳液体推进剂介质,并且包括与射弹室垂直连通的横截面变窄的颈部。 第一构件还包括在射弹室和燃烧室之间形成导管的多个通孔。