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    • 62. 发明公开
    • Cavitation device of underwater moving body and underwater moving body having the same
    • 移动水下体的气穴,因此在水中移动体
    • EP2662658A2
    • 2013-11-13
    • EP12182165.6
    • 2012-08-29
    • Agency For Defense Development
    • Jung, Chul MinKim, Chan KiPark, Warn Gyu
    • F42B10/42F42B19/00
    • F42B10/42B63B1/36B63B2001/382F42B19/00Y02T70/121Y02T70/122
    • Disclosed are a cavitation device (140) and an underwater moving body (100)having the same. The underwater moving body (100) includes a body(110); and a cavitation device (140) for generating a cavity which encloses an outer circumferential surface of the body (110), wherein the cavitation device (140) includes: a plurality of flap-up/down members (141) rotatably connected to the body (110), disposed to cover the outer circumferential surface, and disposed in a circumferential direction and a lengthwise direction of the body in a matrix form; and a pressing module(143) for flapping up the flap-up/down members (141) such that the cavity is generated, as the flap-up/down members (141) are being rotated and inclined from the outer circumferential surface. Furthermore, a ventilation module (144) for forming a ventilated cavity may be coupled to the cavitation device (140).
    • 本发明公开了气穴装置(140)和水下移动体(100)具有相同的。 水下移动体(100)包括:主体(110); 和空化设备(140),用于产生在所述主体(110)worin空化设备(140)的外周面包围的腔,包括:瓣上/下部件的多个(141)可旋转地连接到所述主体 (110)设置成覆盖所述外表面的周向,并在圆周方向上并以矩阵形式所述主体的纵向方向设置; 和用于向上扑翼片升/降元件(141)的按压模块(143)检测DASS模具中产生空腔,随着襟翼升/降元件(141)是被旋转并从外周表面倾斜。 进一步,用于形成通风腔中的通风模块(144)可耦合到所述气穴装置(140)。
    • 65. 发明公开
    • Separation device of ejector motor for portable missile
    • Trennvorrichtung eines Auswurfmotorsfüreine tragbare Rakete
    • EP2293007A2
    • 2011-03-09
    • EP10157710.4
    • 2010-03-25
    • Agency For Defense Development
    • Lee, Hyo-NamOh, Jong-YunKim, Seong-Eun
    • F42B15/36
    • F42B15/36
    • Disclosed is a separation device (100) of an ejector motor (130) for a portable missile (1), capable of being separated from a missile (1) without any additional separation devices after ejecting the missile (1). An ejection rocket motor (130) and a separation device are integrally formed. Ejection is performed by a thrust generated while the ejection rocket motor (130) is combusted, and separation is performed by cutting off shearing bolts (113) with using a force generated from a separation cylinder (141) when the combustion of the ejection rocket motor (130) has been completed. This operation and configuration may minimize a weight and a space occupied by a general ejection and separation device (100) in a missile system.
    • 公开了一种用于便携式导弹(1)的喷射器电动机(130)的分离装置(100),能够在弹出导弹(1)之后没有任何额外的分离装置与导弹(1)分离。 一体形成喷射火箭发动机(130)和分离装置。 通过在喷射火箭发动机(130)燃烧时产生的推力来执行喷射,并且当喷射火箭发动机(130)的燃烧时使用从分离气缸(141)产生的力切断剪切螺栓(113)来进行分离, (130)已经完成。 该操作和配置可以使导弹系统中的一般的喷射和分离装置(100)所占的重量和空间最小化。