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公开(公告)号：KR1020150065497A
公开(公告)日：2015-06-15
申请号：KR1020130150895
申请日：2013-12-05
Applicant: 국방과학연구소
CPC classification number: H02N2/0055 , H01L41/053 , H01L41/0973 , H02N2/0015 , H02N2/04
Abstract: 본발명은, 서로반대측에형성되는제1 및제2 면을구비하며일방향으로연장되고휘어짐이가능하도록형성되는탄성플레이트, 및상기제1 및제2 면에각각적어도하나장착되고상기탄성플레이트를중심으로대칭적으로배치되며전압이인가되면기계적변형이발생하는압전소자를포함하고, 상기압전소자는, 상기탄성플레이트의굽힘을유발시키도록상기제1 및제2 면중 어느한 면에배치되는압전소자에전압이인가되면팽창또는수축되는것을특징으로하는굽힘구조체를제공한다.
Abstract translation: 提供弯曲结构。 弯曲结构包括弹性板，其具有彼此面对的第一和第二表面，沿一个方向延伸并且可以弯曲，并且安装到第一和第二基板中的至少一个的压电装置是对称的 并且在施加电压时机械地变形。 当压电装置施加到布置在第一和第二表面之一上的压电装置时，压电装置膨胀或收缩。
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公开(公告)号：KR1020130142496A
公开(公告)日：2013-12-30
申请号：KR1020120065758
申请日：2012-06-19
Applicant: 국방과학연구소
Abstract: The present invention includes a first body and a second body in which are mutually rotated. A separation device for separating the first body and the second body is separated from a separation structure. Furthermore, the first body and the second body are separated for themselves if the first body and the second body are opened at a predetermined angle. Thus, a separate separation device relative to the separation device is not necessary and the separation structure can stably supply power while the separation structure is mounted on a main body.
Abstract translation: 本发明包括相互旋转的第一主体和第二主体。 用于分离第一主体和第二主体的分离装置与分离结构分离。 此外，如果第一主体和第二主体以预定角度打开，则第一主体和第二主体自身分离。 因此，不需要相对于分离装置的单独的分离装置，并且分离结构可以在分离结构安装在主体上时稳定地供电。
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公开(公告)号：KR101265090B1
公开(公告)日：2013-05-16
申请号：KR1020110107739
申请日：2011-10-20
Applicant: 국방과학연구소
Abstract: 본발명은비행체의캡 분리장치및 이를구비하는비행체에관한것으로, 비행체의캡 분리장치는, 비행체의선단부에장착되어측정장치가배치되는공간을형성하며상기비행체의중심축을기준으로양방향으로분리되는제1 및제2 캡과, 상기제1 및제2 캡과각각결합하는제1 및제2 연결구조물과, 상기제1 및제2 연결구조물을서로체결하며, 기폭에의하여절개되는폭발볼트, 및기폭에의하여피스톤을이동시키도록형성되며, 상기피스톤이제1 및제2 연결구조물중 적어도하나를푸시하도록배치되는파이로푸셔를포함한다. 이에의하여본 발명은비행도중적정시점에서비행체와충돌없이캡을안전하게분리시키는캡 분리장치를제공한다.
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公开(公告)号：KR1020130043528A
公开(公告)日：2013-04-30
申请号：KR1020110107739
申请日：2011-10-20
Applicant: 국방과학연구소
Abstract: PURPOSE: A cap separating device and a flight vehicle with the same are provided to reduce separating force and to minimize the collision to the flight vehicle because a cap is forcibly separated by a pyro-pusher. CONSTITUTION: A cap separating device(200) comprises first and second caps, first and second connection structures(231,232), an explosive bolt, and a pyro-pusher(250). The first and second caps are mounted in the front end of the flight vehicle and form a space where a measuring device is arranged. The first and second caps are bidirectionally separated on a central axis of the flight vehicle. The first and second connection structures are coupled to the first and second caps. The explosive bolt couples the first and second connection structure and is cut by explosion. The pyro-pusher moves a piston(252) and makes the piston push at least one of the first and second connection structures.
Abstract translation: 目的：提供一种帽分离装置和具有该盖分离装置的飞行器，以减少分离力并使与飞行器车辆的碰撞最小化，因为盖子被热击器强行分开。 构成：盖分离装置（200）包括第一和第二盖，第一和第二连接结构（231,232），爆炸螺栓和热推器（250）。 第一和第二盖安装在飞行器车辆的前端，形成测量装置的空间。 第一和第二盖在飞行器的中心轴上双向分离。 第一和第二连接结构联接到第一和第二盖。 爆炸螺栓连接第一和第二连接结构，并被爆炸切断。 热推杆移动活塞（252）并使活塞推动第一和第二连接结构中的至少一个。
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公开(公告)号：KR1020120037806A
公开(公告)日：2012-04-20
申请号：KR1020100099484
申请日：2010-10-12
Applicant: 국방과학연구소
Abstract: PURPOSE: A deploying device, a missile comprising the same and a blade deploying method are provided to reduce the weight and drag of a missile flying since if the deploying of a blade is completed, a deploying device is separated from the blade. CONSTITUTION: A deploying device comprises a housing(23), first and second cylinders(41,42), a fixing pin(30), first and second flow paths(27,28), a rotating shaft(32), and a drive shaft(25). The housing is detachably formed on one side of fuselage. If pneumatic pressure is provided through the pressure port (26) of the first cylinder, a fixing pin reciprocates along the inner circumference of the first cylinder. Pneumatic pressure passes through the first flow path when the fixing pin rises. If the pneumatic pressure is supplied through the first flow pipe, the second cylinder reciprocates along the inner peripheral surface of the first flow pipe by a piston shaft(43).
Abstract translation: 目的：提供一种部署装置，包括相同的刀片展开方法的导弹，以减少导弹飞行的重量和拖动，因为如果叶片的部署完成，部署装置与叶片分离。 构造：展开装置包括壳体（23），第一和第二气缸（41,42），固定销（30），第一和第二流动路径（27,28），旋转轴（32）和驱动 轴（25）。 外壳可拆卸地形成在机身的一侧。 如果通过第一气缸的压力端口（26）提供气压，则固定销沿着第一气缸的内圆周往复运动。 当固定销上升时，气动压力通过第一流路。 如果通过第一流管供给气压，则第二气缸通过活塞轴（43）沿第一流管的内周面往复运动。
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Patent Agency Ranking
公开(公告)号：KR1020180107963A
公开(公告)日：2018-10-04
申请号：KR1020170036963
申请日：2017-03-23
Applicant: 국방과학연구소
Abstract: LVDT 센서를이용한매니퓰레이터가개시된다. LVDT 센서를이용한매니퓰레이터는, LVDT 센서를이용한매니퓰레이터로서, 플랫폼; 상기플랫폼의하부에병렬로형성되는액추에이터; 상기액추에이터사이사이에형성되는 LVDT 센서; 및상기매니퓰레이터의제어변수목표값과상기 LVDT 센서로부터획득된상기매니퓰레이터의자세정보를고려하여제어신호를생성하는제어신호생성부;를포함하며, 상기 LVDT 센서의일단은상기플랫폼의하부에고정되며, 상기 LVDT 센서의타단은볼 조인트가형성된다.
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公开(公告)号：KR101513097B1
公开(公告)日：2015-04-17
申请号：KR1020130156662
申请日：2013-12-16
Applicant: 국방과학연구소
CPC classification number: H02N2/001 , F03G7/04 , H01L41/053 , H02N2/005
Abstract: 본발명은주몸체, 상기주몸체를기준으로회전가능하게장착되는회전체, 상기주몸체와상기회전체를연결하는구동장치를포함하고, 상기구동장치는, 공간을구비하고변형가능하도록형성되는링크유닛, 상기공간사이에배치되고, 상기링크유닛의형상이변형되도록길이의변형이가능한압전작동기, 일단은상기링크유닛에장착되고타단은상기회전체에연결되어, 상기링크유닛의변형에의하여상기회전체를회전시키는연결바를포함하는회전운동장치를제공한다.
Abstract translation: 提供一种旋转运动装置，包括：主体; 安装成可相对于主体旋转的转子; 以及连接主体和转子的驱动单元。 驱动单元包括：具有空间并形成为可变形的连杆单元; 布置在所述空间中的压电致动器，并且具有使所述连杆单元变形的可变长度; 以及连接杆，其一端安装在所述连杆单元上，另一端连接到所述转子，并且通过所述连杆单元的变形使所述转子旋转。 旋转运动装置能够产生足够的角度，尽管轴向变形小。
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公开(公告)号：KR101366774B1
公开(公告)日：2014-02-21
申请号：KR1020120065758
申请日：2012-06-19
Applicant: 국방과학연구소
Abstract: 본 발명은 서로 회동하는 제1 및 제1 바디를 포함하고, 상기 제1 및 제2 바디를 분리하는 분리장치는 분리구조물과 함께 분리된다. 또한 상기 제 1 및 제2 바디는 기 설정된 각도 이상으로 벌어지면 상기 제1 및 제2 바디가 스스로 분리된다.
따라서, 상기 분리장치에 대한 별도의 분리장치를 장착하지 아니하여도 되며, 상기 분리구조물이 상기 본체에 장착되어 있는 동안 안정적으로 전원을 공급할 수 있다.-
公开(公告)号：KR100758855B1
公开(公告)日：2007-09-19
申请号：KR1020060050079
申请日：2006-06-02
Applicant: 국방과학연구소
Abstract: A device for opening a powder type induction ballistic article is provided to utilize the explosion pressure of the powder, so instantly developing a moving body at a precise timing. A device for opening a powder type induction ballistic article comprises a pressure generating unit, and a pressure transmission unit. The pressure generating unit is installed between a moving body and a mounting material(30) to generate the explosion pressure. The pressure transmission unit is connected with the pressure generating unit to operate the power due to the explosion pressure to the mounting material, and to develop the moving body due to the reaction force with the mounting material. The pressure transmission unit is positioned to generate a pair of reaction forces which is the same size and the opposite direction of the mounting material at the upper and lower sides if the explosion pressure due to the pressure generating unit is generated, to develop the upper and lower dividing moving bodies simultaneously.
Abstract translation: 提供一种用于打开粉末型感应弹道制品的装置，以利用粉末的爆炸压力，从而在精确的时间瞬间显影移动体。 用于打开粉末型感应弹道制品的装置包括压力产生单元和压力传递单元。 压力发生单元安装在移动体和安装材料（30）之间以产生爆炸压力。 压力传递单元与压力发生单元连接，由于对安装材料的爆炸压力而操作动力，并且由于与安装材料的反作用力而使运动体显影。 压力传递单元被定位成产生一对反作用力，如果产生由压力发生单元引起的爆炸压力，则产生与上部和下侧相同的尺寸和相反的安装材料的方向，以形成上部和下部 同时下划分移动体。
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公开(公告)号：KR101921415B1
公开(公告)日：2018-11-22
申请号：KR1020170036963
申请日：2017-03-23
Applicant: 국방과학연구소
Abstract: LVDT 센서를이용한매니퓰레이터가개시된다. LVDT 센서를이용한매니퓰레이터는, LVDT 센서를이용한매니퓰레이터로서, 플랫폼; 상기플랫폼의하부에병렬로형성되는액추에이터; 상기액추에이터사이사이에형성되는 LVDT 센서; 및상기매니퓰레이터의제어변수목표값과상기 LVDT 센서로부터획득된상기매니퓰레이터의자세정보를고려하여제어신호를생성하는제어신호생성부;를포함하며, 상기 LVDT 센서의일단은상기플랫폼의하부에고정되며, 상기 LVDT 센서의타단은볼 조인트가형성된다.
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