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    • 3. 发明申请
    • DISPOSAL OF MUNITIONS
    • 废物处理
    • WO2014054007A1
    • 2014-04-10
    • PCT/IB2013/059070
    • 2013-10-02
    • CALORDOMUS LIMITED
    • REID, John
    • F42B33/06
    • F42B33/06
    • A method of emptying explosive material (18) from a munition shell (10) is described which comprises the steps of forming an opening at one end (14) of the shell casing, venting the opposite end (16) of the shell, suspending the casing from the opposite end, and heating the shell (10) by passing a high frequency alternating current through an induction coil (20) surrounding the shell casing (12), heat being applied to soften the explosive material (18) sufficiently for the explosive material to drop out of the casing (12) under the action of gravity.
    • 描述了从弹药壳(10)排空炸药(18)的方法,其包括以下步骤:在壳壳的一端(14)处形成开口,将外壳的相对端(16)排出, 并且通过使高频交流电流通过围绕壳壳体(12)的感应线圈(20)来加热壳体(10),加热以充分地将爆炸物质(18)软化以用于爆炸物 材料在重力的作用下脱离壳体(12)。
    • 8. 发明申请
    • CLOSED VESSEL ARRANGEMENT FOR SAFE DESTRUCTION OF ROCKET MOTORS
    • 封闭式船舶装置安全破坏摇篮电机
    • WO2011021969A1
    • 2011-02-24
    • PCT/SE2009/000388
    • 2009-08-21
    • OLCON ENGINEERING ABOHLSON, Johnny
    • OHLSON, Johnny
    • F23G7/00F42B33/06
    • F42D5/045F23G7/003F23G2209/16F42B33/067
    • The present invention relates to a closed vessel arrangement (1) comprising a closed vessel (2) for safe destruction of a rocket motor (3) containing a solid propellant (4) by burning the rocket motor (3) inside the closed vessel (2), which closed vessel (2), is adjustable in size to a rocket motor (3). The invention is characterized in that the closed vessel (2) comprises two communicating chambers (7, 8) coaxially arranged to each other, one outer chamber (8) and one inner chamber (7), which chambers (7, 8) are divided into a plurality of connectable sections (13), which sections (13) are connectable in various numbers for adjusting the size of the vessel (2) to rocket motors (3) of various sizes.
    • 本发明涉及一种密封容器装置(1),其包括用于通过将密封容器(2)内的火箭发动机(3)燃烧而安全地破坏含有固体推进剂(4)的火箭发动机(3)的密闭容器(2) ),其封闭容器(2)的尺寸可以与火箭发动机(3)大小相适应。 本发明的特征在于,密封容器(2)包括彼此同轴布置的两个连通腔(7,8),一个外室(8)和一个内室(7),这些室(7,8)被分开 分成多个可连接部分(13),这些部分(13)可以各种数字连接,用于将容器(2)的尺寸调整为各种尺寸的火箭发动机(3)。