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    Missile ejection system and launching canister thereof
    3.
    发明授权
    Missile ejection system and launching canister thereof 有权
    导弹弹射系统及其发射罐

    公开(公告)号：US07484449B2

    公开(公告)日：2009-02-03

    申请号：US11169022

    申请日：2005-06-28

    申请人： Woo-Jeon Shim ,  Il-Soo Kim ,  Seung-Jong Oh ,  Jae-Hoon Ha ,  Ji-Chul Kim

    发明人： Woo-Jeon Shim ,  Il-Soo Kim ,  Seung-Jong Oh ,  Jae-Hoon Ha ,  Ji-Chul Kim

    IPC分类号： F41F3/04 ,  F41F3/042 ,  F41F3/045

    CPC分类号： F41F3/0413 ,  F41F3/00 ,  F41F3/042 ,  F41F3/073 ,  F42B5/045 ,  F42B14/064

    摘要： The present invention discloses a missile ejection system and a canister thereof. The missile ejection system comprises: comprising: a canister formed as a cylindrical shell, a partition wall protruding from an inner wall of the canister so as to divide the canister into a first chamber for housing a missile therewithin and a second chamber, and having at least one hole therethrough for allowing the flowing of gas through the partition wall, a gas generator secured to the partition wall in the second chamber so that a gas outlet thereof faces in an opposite direction from the first chamber, and an obturator including a sealing plate formed with a concave surface toward a fore-end of the missile for enclosing a tail end of the missile, and a radially extending skirt plate extended from the circumference of the sealing plate to the inner wall of the canister and inclined toward the fore-end of the missile for covering the space between the missile and the inner canister, wherein the missile is propelled by the pressure of the gas discharged out of the gas generator from the second chamber to the first chamber through the hole, being pressurized by the flown-in gas in the first chamber, pushing upon the obturator. Thereby, the system is able to effectively release a missile from a canister by a gas generator without using a missile propulsion engine, thereby fundamentally preventing the damage of ground equipments or peripheral missiles.

    摘要翻译： 本发明公开了一种导弹喷射系统及其罐。 导弹喷射系统包括：包括：形成为圆柱形壳体的罐，从罐的内壁突出的分隔壁，以便将罐分成用于容纳其中的导弹和第二室的第一室，并且具有 通过其中的至少一个孔，用于允许气体流过分隔壁;气体发生器，固定到第二腔室中的分隔壁，使得其气体出口面向与第一腔室相反的方向;以及闭孔器，包括密封板 形成有朝向导弹前端的凹形表面，用于封闭导弹的尾端，以及径向延伸的裙板，其从密封板的圆周延伸到罐的内壁，并朝向前端倾斜 的导弹，用于覆盖导弹和内部罐之间的空间，其中导弹由从气体发生器fr排出的气体的压力推进 通过该孔将第二腔室的第二腔室移动到第一腔室，由第一腔室中的流入气体加压，推压闭塞器。 因此，该系统能够在不使用导弹推进发动机的情况下通过气体发生器有效地从罐排出导弹，从而从根本上防止了地面设备或周边导弹的损坏。

    Missile ejection system and launching canister thereof
    5.
    发明申请
    Missile ejection system and launching canister thereof 有权

    公开(公告)号：US20060214062A1

    公开(公告)日：2006-09-28

    申请号：US11169022

    申请日：2005-06-28

    申请人： Woo-Jeon Shim ,  Il-Soo Kim ,  Seung-Jong Oh ,  Jae-Hoon Ha ,  Ji-Chul Kim

    发明人： Woo-Jeon Shim ,  Il-Soo Kim ,  Seung-Jong Oh ,  Jae-Hoon Ha ,  Ji-Chul Kim

    IPC分类号： B64C1/22 ,  B64D1/08 ,  B64D9/00

    CPC分类号： F41F3/0413 ,  F41F3/00 ,  F41F3/042 ,  F41F3/073 ,  F42B5/045 ,  F42B14/064

    摘要： The present invention discloses a missile ejection system and a canister thereof. The missile ejection system comprises: comprising: a canister formed as a cylindrical shell, a partition wall protruding from an inner wall of the canister so as to divide the canister into a first chamber for housing a missile therewithin and a second chamber, and having at least one hole therethrough for allowing the flowing of gas through the partition wall, a gas generator secured to the partition wall in the second chamber so that a gas outlet thereof faces in an opposite direction from the first chamber, and an obturator including a sealing plate formed with a concave surface toward a fore-end of the missile for enclosing a tail end of the missile, and a radially extending skirt plate extended from the circumference of the sealing plate to the inner wall of the canister and inclined toward the fore-end of the missile for covering the space between the missile and the inner canister, wherein the missile is propelled by the pressure of the gas discharged out of the gas generator from the second chamber to the first chamber through the hole, being pressurized by the flown-in gas in the first chamber, pushing upon the obturator. Thereby, the system is able to effectively release a missile from a canister by a gas generator without using a missile propulsion engine, thereby fundamentally preventing the damage of ground equipments or peripheral missiles.