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1. 发明申请

US20150168563A1 FIBER-OPTIC SENSOR SYSTEM FOR MEASURING RELATIVE DOSE OF THERAPEUTIC PROTON BEAM BY MEASURING CERENKOV RADIATION AND METHOD OF MEASURING USING THE SAME 有权
标题翻译：用于通过测量CERENKOV辐射测量治疗原子束的相对剂量的光纤传感器系统和使用其测量的方法
公开(公告)号：US20150168563A1
公开(公告)日：2015-06-18
申请号：US14415055
申请日：2012-07-23
申请人： Bong Soo Lee , Kyoung Won Jang , Wook Jae Yoo , Sang Hun Shin , Dong Ho Shin
发明人： Bong Soo Lee , Kyoung Won Jang , Wook Jae Yoo , Sang Hun Shin , Dong Ho Shin
IPC分类号： G01T1/02 , G01T1/22
CPC分类号： G01T1/02 , A61N5/1075 , A61N2005/1076 , A61N2005/1087 , G01T1/22
摘要： The present invention relates to a fiber-optic sensor system for measuring the relative dose of a therapeutic proton beam by measuring Cerenkov radiation and a method of measuring using the same, and more particularly to a fiber-optic sensor system for precisely and economically measuring a proton beam by measuring the Cerenkov radiation generated from a fiber-optic sensor and a method of measuring using the same. The present invention comprises a proton beam source, a fiber-optic sensor for measuring the Bragg peak of the proton beam and SOBP, an optical detector for measuring the Cerenkov radiation, and a pair of optical fibers connecting the fiber-optic sensor and the optical detector, wherein the fiber-optic sensor being irradiated with a proton beam, the Cerenkov radiation generated in the optical fibers themselves is delivered through the optical detector to an amplifier system, and the resulting signal is transferred to a computer.
摘要翻译：本发明涉及一种光纤传感器系统，用于通过测量切伦科夫辐射来测量治疗质子束的相对剂量，以及一种使用其测量的方法，更具体地涉及一种用于精确和经济地测量质子束通过测量从光纤传感器产生的切伦科夫辐射和使用其测量的方法。本发明包括质子束源，用于测量质子束的布拉格峰的光纤传感器和SOBP，用于测量切伦科夫辐射的光学检测器和连接光纤传感器和光学器件的一对光纤检测器，其中所述光纤传感器被质子束照射，在光纤本身中产生的切伦科夫辐射通过光学检测器传送到放大器系统，并将所得到的信号传送到计算机。

2. 发明申请

US20100033058A1 Physical/Biochemical Sensor Using Piezoelectric Microcantilever And Manufacturing Method Thereof 有权
标题翻译：使用压电微型悬臂梁的物理/生化传感器及其制造方法
公开(公告)号：US20100033058A1
公开(公告)日：2010-02-11
申请号：US12579660
申请日：2009-10-15
申请人： Jai Chan Lee , Sang Hun Shin
发明人： Jai Chan Lee , Sang Hun Shin
IPC分类号： H01L41/00 , H01B13/00
CPC分类号： G01N29/036 , G01N29/022 , G01N2291/014 , G01N2291/0255 , G01N2291/0256 , G01N2291/0427
摘要： The present invention discloses a physical/biochemical sensor using a multisized piezoelectric microcantilever resonator array which enables to quantitatively and simultaneously analyze a mass loading effect and a surface stress change effect and a manufacturing method thereof. In the physical/biochemical sensor using the multisized piezoelectric microcantilever resonator array, a plurality of piezoelectric micro-cantilever resonators having different sizes is arrayed so as to quantitatively and discriminately analyze a surface stress change as well as a sensor surface mass change induced by an adsorbed sensing-target material occurring in a sensing process. Thus, the mass loading effect and the surface stress change effect can be quantitatively and simultaneously analyzed.
摘要翻译：本发明公开了一种使用能够定量和同时分析质量负荷效应和表面应力变化效应的多尺寸压电微悬臂梁谐振器阵列的物理/生化传感器及其制造方法。在使用多尺寸压电微悬臂梁谐振器阵列的物理/生物化学传感器中，排列具有不同尺寸的多个压电微悬臂谐振器，以便定量和区分地分析表面应力变化以及由吸附引起的传感器表面质量变化感测目标材料发生在感测过程中。因此，可以定量和同时分析质量负荷效应和表面应力变化效应。

3. 发明申请

US20070283800A1 MISSILE LAUNCH AND GUIDANCE APPARATUS 有权
标题翻译： MISSILE发射和指导装置
公开(公告)号：US20070283800A1
公开(公告)日：2007-12-13
申请号：US11618217
申请日：2006-12-29
申请人： Tae-Hak PARK , Sang-Hun SHIN
发明人： Tae-Hak PARK , Sang-Hun SHIN
IPC分类号： F41F3/04
CPC分类号： F41F3/0406 , F42B14/00 , F42B14/02 , F42B14/064
摘要： A missile launch and guidance apparatus of a rail-shoe launching type is disclosed. In a missile adapted to be launched while moving along a rail of a launch tube, a missile launch and guidance apparatus comprises: a bushing inserted into a missile body; a shoe, one end of which is inserted into the bushing, and the other end of which is in contact with the rail; and a spring inserted between the bushing and the shoe so as to provide a separation force to the shoe against the bushing. By separating the shoe from the missile in a lateral direction of the missile launching direction by an elastic force of the spring after launching the missile, the missile launch and guidance apparatus can keep constant the gap between the missile and the launch tube rail irrespective of the behavior of the missile taking place in a launching process, and the drag and weight of the missile launched from the launch tube is reduced to thereby exhibit the maximum flight performance.
摘要翻译：披露了一种轨道式发射型导弹发射导向装置。导弹发射和引导装置在适于沿着发射管轨道发射的导弹中包括：插入导弹体的衬套; 鞋的一端插入衬套中，另一端与导轨接触; 以及插入衬套和鞋之间的弹簧，以便向鞋抵靠衬套提供分离力。通过在发射导弹之后弹簧的弹力使导弹在导弹发射方向的横向上与导弹分离，导弹发射和引导装置可以保持导弹和发射管轨之间的间隙不变，而不管在发射过程中发生的导弹的行为以及从发射管发射的导弹的阻力和重量减小，从而表现出最大的飞行性能。

4. 发明授权

US09322927B2 Fiber-optic sensor system for measuring relative dose of therapeutic proton beam by measuring cerenkov radiation and method of measuring using the same 有权
标题翻译：光纤传感器系统，用于通过测量cerenkov辐射来测量治疗质子束的相对剂量，以及使用其测量的方法
公开(公告)号：US09322927B2
公开(公告)日：2016-04-26
申请号：US14415055
申请日：2012-07-23
申请人： Bong Soo Lee , Kyoung Won Jang , Wook Jae Yoo , Sang Hun Shin , Dong Ho Shin
发明人： Bong Soo Lee , Kyoung Won Jang , Wook Jae Yoo , Sang Hun Shin , Dong Ho Shin
IPC分类号： G01T1/00 , G01T1/02 , G01T1/22 , A61N5/10
CPC分类号： G01T1/02 , A61N5/1075 , A61N2005/1076 , A61N2005/1087 , G01T1/22
摘要： The present invention relates to a fiber-optic sensor system for measuring the relative dose of a therapeutic proton beam by measuring Cerenkov radiation and a method of measuring using the same, and more particularly to a fiber-optic sensor system for precisely and economically measuring a proton beam by measuring the Cerenkov radiation generated from a fiber-optic sensor and a method of measuring using the same. The present invention comprises a proton beam source, a fiber-optic sensor for measuring the Bragg peak of the proton beam and SOBP, an optical detector for measuring the Cerenkov radiation, and a pair of optical fibers connecting the fiber-optic sensor and the optical detector, wherein the fiber-optic sensor being irradiated with a proton beam, the Cerenkov radiation generated in the optical fibers themselves is delivered through the optical detector to an amplifier system, and the resulting signal is transferred to a computer.
摘要翻译：本发明涉及一种光纤传感器系统，用于通过测量切伦科夫辐射来测量治疗质子束的相对剂量，以及一种使用其测量的方法，更具体地涉及一种用于精确和经济地测量质子束通过测量从光纤传感器产生的切伦科夫辐射和使用其测量的方法。本发明包括质子束源，用于测量质子束的布拉格峰的光纤传感器和SOBP，用于测量切伦科夫辐射的光学检测器和连接光纤传感器和光学器件的一对光纤检测器，其中所述光纤传感器被质子束照射，在光纤本身中产生的切伦科夫辐射通过光学检测器传送到放大器系统，并将所得到的信号传送到计算机。

5. 发明授权

US08304703B2 Apparatus for deploying wing and apparatus for launching flight having the same 有权
标题翻译：用于部署机翼的装置和用于发射具有相同的飞行的装置
公开(公告)号：US08304703B2
公开(公告)日：2012-11-06
申请号：US12757191
申请日：2010-04-09
申请人： Heon Suk Hong , Sang Hun Shin , Woo Yong Lee
发明人： Heon Suk Hong , Sang Hun Shin , Woo Yong Lee
IPC分类号： F42B15/01
CPC分类号： F42B10/14 , F42B10/18
摘要： Disclosed are a wing deployment apparatus and an apparatus for launching a flying object having the same, the wing deployment apparatus including wings configured to be in a folded state and a deployed state, a driving unit connected to the wings, and configured to drive the wings to be switched from the folded state to the deployed state or vice versa, and a damper cooperative with the operation of the driving unit, and configured to damp a driving force of the driving unit from the start of the wings being moved to the completion of the movement of the wings.
摘要翻译：公开了一种翼展开装置和用于发射具有该飞行物体的飞行物体的装置，所述翼展开装置包括构造成处于折叠状态和展开状态的翼部，连接到翼部的驱动单元，并且构造成驱动翼从折叠状态切换到展开状态，反之亦然，以及与所述驱动单元的操作相协调的风门，并且构造成阻止所述驱动单元的驱动力从所述翼的开始移动到完成机翼的运动。

6. 发明授权

US07647856B2 Missile launch and guidance apparatus 有权
标题翻译：导弹发射和引导装置
公开(公告)号：US07647856B2
公开(公告)日：2010-01-19
申请号：US11618217
申请日：2006-12-29
申请人： Tae-Hak Park , Sang-Hun Shin
发明人： Tae-Hak Park , Sang-Hun Shin
IPC分类号： F41F3/052
CPC分类号： F41F3/0406 , F42B14/00 , F42B14/02 , F42B14/064
摘要： A missile launch and guidance apparatus of a rail-shoe launching type is disclosed. In a missile adapted to be launched while moving along a rail of a launch tube, a missile launch and guidance apparatus comprises: a bushing inserted into a missile body; a shoe, one end of which is inserted into the bushing, and the other end of which is in contact with the rail; and a spring inserted between the bushing and the shoe so as to provide a separation force to the shoe against the bushing. By separating the shoe from the missile in a lateral direction of the missile launching direction by an elastic force of the spring after launching the missile, the missile launch and guidance apparatus can keep constant the gap between the missile and the launch tube rail irrespective of the behavior of the missile taking place in a launching process, and the drag and weight of the missile launched from the launch tube is reduced to thereby exhibit the maximum flight performance.
摘要翻译：披露了一种轨道式发射型导弹发射导向装置。导弹发射和引导装置在适于沿着发射管轨道发射的导弹中包括：插入导弹体的衬套; 鞋的一端插入衬套中，另一端与导轨接触; 以及插入衬套和鞋之间的弹簧，以便向鞋抵靠衬套提供分离力。通过在发射导弹之后弹簧的弹力使导弹在导弹发射方向的横向上与导弹分离，导弹发射和引导装置可以保持导弹和发射管轨之间的间隙不变，而不管在发射过程中发生的导弹的行为以及从发射管发射的导弹的阻力和重量减小，从而表现出最大的飞行性能。

7. 发明授权

US08169124B2 Physical/biochemical sensor using piezoelectric microcantilever and manufacturing method thereof 有权
标题翻译：使用压电微悬臂梁的物理/生化传感器及其制造方法
公开(公告)号：US08169124B2
公开(公告)日：2012-05-01
申请号：US12579660
申请日：2009-10-15
申请人： Jai Chan Lee , Sang Hun Shin
发明人： Jai Chan Lee , Sang Hun Shin
IPC分类号： H01L41/08
CPC分类号： G01N29/036 , G01N29/022 , G01N2291/014 , G01N2291/0255 , G01N2291/0256 , G01N2291/0427
摘要： The present invention discloses a physical/biochemical sensor using a multisized piezoelectric microcantilever resonator array which enables to quantitatively and simultaneously analyze a mass loading effect and a surface stress change effect and a manufacturing method thereof. In the physical/biochemical sensor using the multisized piezoelectric microcantilever resonator array, a plurality of piezoelectric micro-cantilever resonators having different sizes is arrayed so as to quantitatively and discriminately analyze a surface stress change as well as a sensor surface mass change induced by an adsorbed sensing-target material occurring in a sensing process. Thus, the mass loading effect and the surface stress change effect can be quantitatively and simultaneously analyzed.
摘要翻译：本发明公开了一种使用能够定量和同时分析质量负荷效应和表面应力变化效应的多尺寸压电微悬臂梁谐振器阵列的物理/生化传感器及其制造方法。在使用多尺寸压电微悬臂梁谐振器阵列的物理/生物化学传感器中，排列具有不同尺寸的多个压电微悬臂谐振器，以便定量和区分地分析表面应力变化以及由吸附引起的传感器表面质量变化感测目标材料发生在感测过程中。因此，可以定量和同时分析质量负荷效应和表面应力变化效应。

8. 发明授权

US08525089B2 Wing device and flight vehicle having the same 有权
标题翻译：翼装置和飞行器具有相同的
公开(公告)号：US08525089B2
公开(公告)日：2013-09-03
申请号：US13084434
申请日：2011-04-11
申请人： Sang-Hun Shin , Hae-Yong Jeong
发明人： Sang-Hun Shin , Hae-Yong Jeong
IPC分类号： F42B15/01 , B64C3/56
CPC分类号： F42B10/16
摘要： Disclosed are a wing device for a flight vehicle and a flight vehicle having the same, the wing device including a fixing shaft disposed in a lengthwise direction of a main body of the flight vehicle, a wing rotatably mounted to the fixing shaft so as to be deployed from a state of being laid on an outer circumferential surface of the main body to an erected state, and slidable along the fixing shaft, a fixing groove formed to face the wing in a sliding direction of the wing, and a spring unit configured to apply a first elastic force in an outer circumferential direction of the main body for deployment of the wing, and apply a second elastic force in a lengthwise direction of the main body for inserting the wing into the fixing groove, whereby the wing can be fixed after deployment so as to enhance stability of the flight vehicle.
摘要翻译：公开了一种用于飞行器车辆的翼装置和具有该翼装置的飞行器，所述翼装置包括沿着飞行车辆的主体的长度方向设置的固定轴，可旋转地安装到固定轴的翼，从主体的外周面放置到竖立状态的状态，沿着固定轴滑动，形成为沿机翼的滑动方向与机翼相对的固定槽，弹簧单元构成为在主体的外周方向上施加第一弹性力以展开机翼，并且在主体的长度方向上施加第二弹性力，以将翼插入固定槽中，由此翼可以固定在固定槽之后部署，以提高飞行器的稳定性。

9. 发明申请

US20100314490A1 APPARATUS FOR DEPLOYING WING AND APPARATUS FOR LAUNCHING FLIGHT HAVING THE SAME 有权
标题翻译：配备发射飞机的装置和装置
公开(公告)号：US20100314490A1
公开(公告)日：2010-12-16
申请号：US12757191
申请日：2010-04-09
申请人： Heon Suk HONG , Sang Hun SHIN , Woo Yong LEE
发明人： Heon Suk HONG , Sang Hun SHIN , Woo Yong LEE
IPC分类号： B64C3/56 , B64F1/04
CPC分类号： F42B10/14 , F42B10/18
摘要： Disclosed are a wing deployment apparatus and an apparatus for launching a flying object having the same, the wing deployment apparatus including wings configured to be in a folded state and a deployed state, a driving unit connected to the wings, and configured to drive the wings to be switched from the folded state to the deployed state or vice versa, and a damper cooperative with the operation of the driving unit, and configured to damp a driving force of the driving unit from the start of the wings being moved to the completion of the movement of the wings.
摘要翻译：公开了一种翼展开装置和用于发射具有该飞行物体的飞行物体的装置，所述翼展开装置包括构造成处于折叠状态和展开状态的翼部，连接到翼部的驱动单元，并且构造成驱动翼从折叠状态切换到展开状态，反之亦然，以及与所述驱动单元的操作相协调的风门，并且构造成阻止所述驱动单元的驱动力从所述翼的开始移动到完成机翼的运动。

10. 发明授权

US08415597B2 Wing assembly and apparatus for launching flying object using the same 有权
标题翻译：翼组件和使用其的飞行物体的发射装置
公开(公告)号：US08415597B2
公开(公告)日：2013-04-09
申请号：US12779346
申请日：2010-05-13
申请人： Sang Hun Shin , Heon Suk Hong , Woo Yong Lee
发明人： Sang Hun Shin , Heon Suk Hong , Woo Yong Lee
IPC分类号： F42B10/00
CPC分类号： F42B10/14
摘要： Disclosed are a wing assembly including a wing movably accommodated in a launch tube, and a buffer unit detachably mounted to the wing to come in contact with the launch tube and configured to be separated from the wing after the wing comes out of an inner space of the launch tube, and an apparatus for launching a flying object having the same.
摘要翻译：公开了一种机翼组件，其包括可移动地容纳在发射管中的机翼，以及缓冲单元，其可拆卸地安装到机翼以与发射管接触并且构造成在机翼从机翼从内部空间出来之后与机翼分离发射管，以及用于发射具有该飞行物体的飞行物体的装置。

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