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1. 发明公开

EP2293007A2 Separation device of ejector motor for portable missile 有权
标题翻译： Trennvorrichtung eines Auswurfmotorsfüreine tragbare Rakete
公开(公告)号：EP2293007A2
公开(公告)日：2011-03-09
申请号：EP10157710.4
申请日：2010-03-25
申请人： Agency For Defense Development
发明人： Lee, Hyo-Nam , Oh, Jong-Yun , Kim, Seong-Eun
IPC分类号： F42B15/36
CPC分类号： F42B15/36
摘要： 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.
摘要翻译：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。

2. 发明授权

EP2293007B1 Separation device of ejector motor for portable missile 有权
标题翻译：对于便携式导弹喷射器电机分离装置
公开(公告)号：EP2293007B1
公开(公告)日：2013-06-26
申请号：EP10157710.4
申请日：2010-03-25
申请人： Agency For Defense Development
发明人： Lee, Hyo-Nam , Oh, Jong-Yun , Kim, Seong-Eun
IPC分类号： F42B15/36
CPC分类号： F42B15/36

3. 发明公开

EP2293007A3 Separation device of ejector motor for portable missile 有权
标题翻译：对于便携式导弹喷射器电机分离装置
公开(公告)号：EP2293007A3
公开(公告)日：2012-07-04
申请号：EP10157710.4
申请日：2010-03-25
申请人： Agency For Defense Development
发明人： Lee, Hyo-Nam , Oh, Jong-Yun , Kim, Seong-Eun
IPC分类号： F42B15/36
CPC分类号： F42B15/36
摘要： 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.

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