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1. 发明授权

US07484449B2 Missile ejection system and launching canister thereof 有权
标题翻译：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。

2. 发明授权

US06352993B1 Pyrimidine derivatives and processes for the preparation thereof 失效
标题翻译：嘧啶衍生物及其制备方法
公开(公告)号：US06352993B1
公开(公告)日：2002-03-05
申请号：US09381814
申请日：1999-09-24
申请人： Jong Wook Lee , Bong Yong Lee , Chang Seop Kim , Seung Kyu Lee , Keun Seog Song , Song Jin Lee , Woo Jeon Shim , Man Soon Hwang
发明人： Jong Wook Lee , Bong Yong Lee , Chang Seop Kim , Seung Kyu Lee , Keun Seog Song , Song Jin Lee , Woo Jeon Shim , Man Soon Hwang
IPC分类号： C07D40104
CPC分类号： C07D401/04 , C07D401/14 , C07D417/14
摘要： The present invention relates to novel pyrimidine derivatives of formula (I) or pharmaceutically acceptable salts thereof which possess an excellent anti-secretory activity, pharmaceutical compositions containing the same as an active ingredient, their novel intermediates, and processes for the preparation thereof wherein: when A is piperidin-1-yl or —NH—B, wherein B is C3-C4 alkyl, C3-C4 alkenyl, C3-C7 cycloalkyl, C1-C3 alkoxyethyl, phenylethl which may be substituted or unsubstituted, 3-trifluoromethylphenylmethyl, 1-naphthylmethyl, 4-methylthiazol-2-yl or 4-phenylthiazol-2-yl, R1 is hydrogen or methyl; and R2, R3, R4 and R5 are hydrogen; or when A is a group of formula (II); when R1 is hydroxymethyl or C1-C3 alkoxymethyl, R2, R3, R4, R5 and R6 are hydrogen; and R7 is hydrogen or halogen; or when R1 is hydrogen or methyl, R7 is hydrogen or halogen; and one or two of R2, R3, R4, R5 and R6 is hydroxy, methoxy, or a group of formula (III) wherein Z is C1-C4 alkyl, substituted or unsubstituted C1-C4 alkenyl, cyloalkyl, benzyloxyalkyl, alkoxycarbonylalkyl, morpholinomethyl, piperidinomethyl, 4-substituted-piperazinomethyl, substituted or unsubstituted phenyl, naphthyl, substituted or unsubstituted benzyl, thiophen-2-yl-methyl, 1-substituted-pyrrolidin-2-yl or —CHR8NHR9, wherein R8 is hydrogen, methyl, isopropyl, benzyl, benzyloxymethyl, methylthioethyl, benzyloxycarbonylmethyl, carbamolymethyl, carbamoylethyl, or 1-benzylimidazol-4-ylmethyl and R9 is hydrogen or t-butoxycarbonyl; and the others are hydrogen or methyl.
摘要翻译：本发明涉及具有优异抗分泌活性的式（I）的新颖的嘧啶衍生物或其药学上可接受的盐，其含有与活性成分相同的药物组合物，其新颖的中间体及其制备方法，其中： A是哌啶-1-基或-NH-B，其中B是C 3 -C 4烷基，C 3 -C 4烯基，C 3 -C 7环烷基，C 1 -C 3烷氧基乙基，可以被取代或未取代的苯乙基，3-三氟甲基苯基甲基，萘基甲基，4-甲基噻唑-2-基或4-苯基噻唑-2-基，R 1是氢或甲基; R2，R3，R4和R5是氢; 或当A为式（II）的基团时; 当R 1是羟甲基或C 1 -C 3烷氧基甲基时，R 2，R 3，R 4，R 5和R 6是氢; 并且R 7是氢或卤素; 或当R 1为氢或甲基时，R 7为氢或卤素; R 2，R 3，R 4，R 5和R 6中的一个或两个是羟基，甲氧基或其中Z是C 1 -C 4烷基，取代或未取代的C 1 -C 4烯基，环烷基，苄氧基烷基，烷氧基羰基烷基，吗啉代甲基，哌啶基甲基，4-取代的哌嗪基甲基，取代或未取代的苯基，萘基，取代或未取代的苄基，噻吩-2-基 - 甲基，1-取代的吡咯烷-2-基或-CHR8NHR9，其中R8是氢，甲基，苄基，苄氧基甲基，甲硫基乙基，苄氧基羰基甲基，氨基甲酰基，氨基甲酰基乙基或1-苄基咪唑-4-基甲基，R9为氢或叔丁氧基羰基; 其他的是氢或甲基。

3. 发明授权

US07665395B2 Lateral support device system for canister-launched missile 有权
标题翻译：罐式发射导弹的侧支撑装置系统
公开(公告)号：US07665395B2
公开(公告)日：2010-02-23
申请号：US11343097
申请日：2006-01-30
申请人： Il-Soo Kim , Woo-Jeon Shim , Hak-Yeol Lee
发明人： Il-Soo Kim , Woo-Jeon Shim , Hak-Yeol Lee
IPC分类号： F41F3/04
CPC分类号： F41F3/052
摘要： A lateral support device system of a canister-launched missile of the present invention is provided for eliminating the clearances between missile and the canister in 4 places by 90 degrees interval, and therefore no relative movement occurs between the missile and the canister. Therefore, the missile and the detent is free from shocks and vibrations that occurs during the handling, transportation and operation. In addition, when the missile is fired, those lateral lock become free with a little energy loss.
摘要翻译：提供了本发明的发射筒的侧向支撑装置系统，用于在4个位置间隔90度的间隔消除导弹与罐之间的间隙，因此在导弹和罐之间不发生相对运动。因此，导弹和制动器在处理，运输和运行过程中没有发生冲击和振动。此外，当导弹发射时，这些侧向锁具有一点能量损失的自由。

4. 发明申请

US20060214062A1 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.

5. 发明授权

US5744745A Missile detent and release apparatus 失效
标题翻译：导弹制动和释放装置
公开(公告)号：US5744745A
公开(公告)日：1998-04-28
申请号：US764523
申请日：1996-12-12
申请人： Woo-Jeon Shim , Bon-Soon Koo , Beom-Soo Lim , Kil-Ho Hong
发明人： Woo-Jeon Shim , Bon-Soon Koo , Beom-Soo Lim , Kil-Ho Hong
IPC分类号： F41F3/00 , F41F3/042 , F41F3/052 , F41F3/04
CPC分类号： F41F3/042 , F41F3/052
摘要： A missile detent and release apparatus which is capable of detaining and rapidly releasing a missile in a launch tube when conveying/launching the same, and in particular to an improved missile detent and release apparatus by which the missile is easily detained and rapidly released with only a small amount of force, and by which the missile can be stably detained in the launch tube conveying the missile, which includes a pair of detaining protrusions protruded from one end portion of a missile, a pair of fixing members fixed on an inner surface of a missile launch tube and having a detaining groove into which the detaining protrusion is inserted, with the fixing members being formed in the forwarding direction of the missile, a detaining screw passing through a detaining groove of each fixing member in the forwarding direction of the missile and engaged to a detaining screw hole formed at the center portion of the detaining protrusion for detaining the missile in the forwarding direction of the missile, a releasing rotation member rotatably engaged to the fixing member, and extending in the direction of the center of a missile nozzle, with the releasing rotation member being backwardly moved by a rocketing force of the missile, and a detaining pin for detaining the movement of the detaining screw, with the end portion thereof being fixed to the rotation member.
摘要翻译：一种导弹制动和释放装置，能够在传送/发射发射管时拘留和快速释放导弹，特别是改进的导弹制动和释放装置，导弹容易被拘留并迅速释放少量的力量，导弹可以稳定地扣留在运送导弹的发射管中，该导弹包括一对从导弹的一个端部突出的止动突起，一对固定构件固定在导弹的内表面上一个导弹发射管，并具有一个定位槽，其中锁定突起被插入其中，其中固定构件沿导弹的传送方向形成，一个沿着导弹的传送方向穿过每个固定构件的定位槽的定位螺钉并且接合到形成在扣留突起的中心部分处的扣留螺钉孔，用于在直接转发中扣留导弹导弹的离子，可旋转地接合到固定构件的释放旋转构件，并且在导弹喷嘴的中心方向上延伸，释放旋转构件通过导弹的摆动力向后移动，以及用于扣留锁定螺丝的运动，其端部固定在旋转件上。

6. 发明申请

US20070175323A1 Lateral support device system for canister-launched missile 有权
标题翻译：罐式发射导弹的侧支撑装置系统
公开(公告)号：US20070175323A1
公开(公告)日：2007-08-02
申请号：US11343097
申请日：2006-01-30
申请人： Il-Soo Kim , Woo-Jeon Shim , Hak-Yeol Lee
发明人： Il-Soo Kim , Woo-Jeon Shim , Hak-Yeol Lee
IPC分类号： F41F5/00
CPC分类号： F41F3/052
摘要： A lateral support device system of a canister-launched missile of the present invention is provided for eliminating the clearances between missile and the canister in 4 places by 90 degrees interval, and therefore no relative movement occurs between the missile and the canister. Therefore, the missile and the detent is free from shocks and vibrations that occurs during the handling, transportation and operation. In addition, when the missile is fired, those lateral lock become free with a little energy loss.
摘要翻译：提供了本发明的发射筒的侧向支撑装置系统，用于在4个位置间隔90度的间隔消除导弹与罐之间的间隙，因此在导弹和罐之间不发生相对运动。因此，导弹和制动器在处理，运输和运行过程中没有发生冲击和振动。此外，当导弹发射时，这些侧向锁具有一点能量损失的自由。

7. 发明授权

US5714708A Missile restraining apparatus 失效
标题翻译：导弹限制装置
公开(公告)号：US5714708A
公开(公告)日：1998-02-03
申请号：US720024
申请日：1996-09-27
申请人： Woo-Jeon Shim , Il-Soo Kim , Kil-Ho Hong , Woo-Jin Lee
发明人： Woo-Jeon Shim , Il-Soo Kim , Kil-Ho Hong , Woo-Jin Lee
IPC分类号： F41F3/052 , F41F3/00
CPC分类号： F41F3/052
摘要： An improved missile restraining apparatus capable of effectively protecting a missile from an external impact and quickly releasing a missile restraining state when launching missile, which includes a pair of protrusions having a circular cross-section and formed in the rear portion of a missile, and a pair of brackets fixed to the inner surface of a launch tube and formed so that a pair of restraining grooves corresponding to said protrusions are formed in a predetermined direction, wherein one end of said restraining groove has a circular cross-section, and the other end thereof is shaped to have an elongating axis longer than the diameter of the protrusion in the radial direction and to have the same shorter axis as the restraining groove in the vertical direction.
摘要翻译：一种改进的导弹限制装置，能够有效地保护导弹免受外部冲击，并且在发射导弹时迅速释放导弹限制状态，导弹包括一对具有圆形横截面并形成在导弹后部的突起，以及一对支架固定在发射管的内表面上并且形成为使得一对对应于所述突起的约束槽沿预定方向形成，其中所述限制槽的一端具有圆形横截面，另一端成形为具有比突起在径向方向上的直径长的延伸轴线，并且在垂直方向上具有与限制槽相同的短轴。

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