-
公开(公告)号：KR101338156B1
公开(公告)日：2013-12-06
申请号：KR1020130105471
申请日：2013-09-03
Applicant: 국방과학연구소
Abstract: The present invention provides a portable ejection deice for a guided missile. The present invention includes a first cylindrical surface; a housing including an extended surface extended from one end of the first surface by being curved towards the outside of a cylinder; and a connection ring assembly connecting the portable guided missile and the housing. The connection ring assembly unit includes a body in which a groove in which the extended surface inserted is formed on one end, wherein the one end forms a free end and the other end forms a fixed end by being connected to the housing; a spring applying elasticity to the body by being arranged between a first surface and the connection ring body; and a fixing pin of which one end faces the first surface by passing through the body.
Abstract translation: 本发明提供一种用于导弹的便携式喷射罩。 本发明包括第一圆筒形表面; 壳体，其包括从所述第一表面的一端朝向圆柱体的外侧弯曲的延伸表面; 以及连接便携式导弹和壳体的连接环组件。 连接环组件单元包括其中在一端形成有延伸表面插入的槽的主体，其中一端形成自由端，另一端通过连接到壳体形成固定端; 弹簧通过布置在第一表面和连接环体之间而对身体施加弹性; 以及通过穿过本体而使其一端面向第一表面的固定销。
-
公开(公告)号：KR101408093B1
公开(公告)日：2014-06-17
申请号：KR1020140007831
申请日：2014-01-22
Applicant: 국방과학연구소
Abstract: The present invention relates to a mounting device for a portable guided missile and, more specifically, a mounting device for a portable guided missile, capable of simultaneously perform a function providing management convenience and firing stability while performing roles of a fixing unit and a support unit. The mounting device for a portable guided missile includes a Picatinny rail adaptor mounted on a portable weapon; a ball head connected to the lower end of the Picatinny rail adaptor; and a holder supporting the lower end of the ball head.
Abstract translation: 本发明涉及一种用于便携式导弹的安装装置，更具体地说，涉及一种用于便携式导弹的安装装置，能够同时执行提供管理便利性和起火稳定性的功能，同时执行定影单元和支撑单元的作用 。 用于便携式导弹的安装装置包括安装在便携式武器上的Picatinny轨道适配器; 连接到Picatinny轨道适配器下端的球头; 以及支撑球头下端的支架。
-
Patent Agency Ranking
公开(公告)号：KR101338178B1
公开(公告)日：2013-12-09
申请号：KR1020130092063
申请日：2013-08-02
Applicant: 국방과학연구소
Abstract: The present invention relates to restriction release apparatus of a portable guided missile. Disclosed is the restriction release apparatus including a cooling gas container assembly, which provides gas used for cooling an explorer; a branch block, which distributes the gas to the explorer; and a restriction release device of a portable guided missile, which releases the restriction of the portable guided missile by using the pressure of the gas provided from the branch block.
Abstract translation: 本发明涉及便携式导弹的限制解除装置。 公开了一种包括提供用于冷却探险者的气体的冷却气体容器组件的限制释放装置; 一个分支块，将气体分配给探险者; 以及便携式导弹的限制释放装置，其通过使用从分支块提供的气体的压力来释放便携式导弹的限制。
-
公开(公告)号：KR101338177B1
公开(公告)日：2013-12-09
申请号：KR1020130092062
申请日：2013-08-02
Applicant: 국방과학연구소
Abstract: The present invention relates to an apparatus for adjusting a control fin of a portable guided missile comprising: a control fin having a first through-hole formed in one side, and rotating on the first through-hole; a shaft coupled in a state where one side is received, and arranged inside a guided missile body; a hinge for connecting the control fin and the shaft through the second through-hole of the shaft and the first through-hole; a fixing fin penetrating a first fixing pin receiving hole formed on the hinge in a direction vertical to the axial direction of the hinge and a second fixing pin receiving hole formed on one side of the control fin in a direction different to the first through-hole so as to restrict the rotation of the control fin and the hinge; and an elastic member arranged on the shaft to rotate the control fin.
Abstract translation: 本发明涉及一种用于调节便携式导弹的控制翅片的装置，包括：控制翅片，其具有形成在一侧的第一通孔，并在第一通孔上旋转; 在一侧被接收的状态下联接并布置在导弹体内部的轴; 用于通过所述轴的第二通孔和所述第一通孔连接所述控制翅片和所述轴的铰链; 固定翅片，其穿过形成在所述铰链上的垂直于所述铰链的轴向的方向上的第一固定销接收孔;以及第二固定销容纳孔，其形成在所述控制翅片的与所述第一通孔不同的方向上的一侧 以限制控制翅片和铰链的旋转; 以及设置在所述轴上以使所述控制翅片旋转的弹性构件。
-
公开(公告)号：KR101330213B1
公开(公告)日：2013-11-18
申请号：KR1020130105472
申请日：2013-09-03
Applicant: 국방과학연구소
Abstract: The present invention provides a device for assembling and testing a portable guided missile which includes a platform with a rail extended in the first direction; a portable guide missile which fixes module which fixes the portable guide missile by covering and is driven to be rotated in the second direction parallel to the ground surface and in the third direction perpendicular to the ground surface; a launching tube fixing module which fixes a portable guide missile launching tube and is moved along the rail by being mounted on the platform; a front table which is arranged by being separated from the platform in the first direction; an image tracking unit which collects data by tracking a target on the front table which is acquired by a seeker mounted on the portable guide missile; and a driving unit which drives the portable guide missile fixing module based on the data. [Reference numerals] (AA) Operate a mock target;(BB) Spot the mock target in move and lock on the target;(CC) Track the target and check the eye line information;(DD) Track the target;(EE) Check the performance of a guided missile;(FF) Gimbal;(GG) Give an operation command;(HH) Check the gimbal to be controlled;(II) Target tracking information;(JJ) Additional data
Abstract translation: 本发明提供了一种用于组装和测试便携式导弹的装置，其包括具有沿第一方向延伸的轨道的平台; 便携式导弹，其固定通过覆盖固定便携式导弹的模块，并被驱动沿平行于地面的第二方向和垂直于地面的第三方向旋转; 发射管固定模块，其固定便携式导弹发射管，并通过安装在平台上沿着轨道移动; 前台，其沿第一方向与平台分离; 图像跟踪单元，其通过跟踪由安装在便携式导弹上的探测器获取的前台上的目标来收集数据; 以及基于该数据驱动便携式引导导弹固定模块的驱动单元。 （参考号）（AA）操作模拟目标;（BB）瞄准移动中的模拟目标并锁定目标;（CC）跟踪目标并检查眼线信息;（DD）跟踪目标;（EE） 检查导弹的性能;（FF）Gimbal;（GG）给出操作命令;（HH）检查待控制的万向节;（II）目标跟踪信息;（JJ）附加数据
-
公开(公告)号：KR101356554B1
公开(公告)日：2014-01-29
申请号：KR1020130095894
申请日：2013-08-13
Applicant: 국방과학연구소
Abstract: The present invention relates to a deploying and folding structure of a wing used for controlling a position and a posture of a guided missile during a flight. The guided missile includes a plurality of wings used for controlling the posture and the position of the guided missile during the flight. The deploying and folding structure of the wing of the guided missile includes a hinge which is a rotary axis of the wing by being included on one end of the wing; a spring providing a rotatory force to the wing while the wing is rotated; and a hinge body in which the wing, the spring, and the hinge are assembled. The deploying and folding structure of the wing of the guided missile is characterized by deploying and folding the wing by rotating the same around the hinge once.
Abstract translation: 本发明涉及一种用于在飞行中控制导弹的位置和姿势的机翼的展开和折叠结构。 导弹包括用于控制飞行中导弹的姿势和位置的多个翼。 导弹翼的展开和折叠结构包括一个铰链，它是翼的旋转轴线，它包括在机翼的一端; 弹簧在机翼旋转时向机翼提供旋转力; 以及铰接体，其中机翼，弹簧和铰链组装在其中。 导弹翼的展开和折叠结构的特点是通过围绕铰链旋转一次来展开和折叠机翼。
-
公开(公告)号：KR101345669B1
公开(公告)日：2013-12-30
申请号：KR1020130105469
申请日：2013-09-03
Applicant: 국방과학연구소
Abstract: Provided in the present invention is a device for unfolding and fixing the wings of a portable guided missile installed on the airframes of the portable guided missile to fold or unfold the wing of the guided missile. The device for unfolding and fixing the wings of the portable guided missile comprises: a hinge axis formed intersecting one end part of the wing to be the rotating axis of the wing; a spring coupled to the hinge axis to apply a rotational force in a wing unfolding direction; a fixed pin installed adjacent to the hinge axis in the wing and having one end coupled to a compression spring elastically deformed in a longitudinal direction; and a clevis having a first surface fixed at the airframes and a second surface extended in a direction crossing the first surface, coupled to the hinge axis, providing a sliding path by making the other end of the fixing pin in contact, and forming a recess interlocked with the other end of the fixing pin on one end of the path.
Abstract translation: 在本发明中提供了一种用于展开和固定安装在便携式导弹的机身上的便携式导弹的机翼折叠或展开导弹翼的装置。 用于展开和固定便携式导弹的机翼的装置包括：铰接轴线，其形成为与机翼的一个端部相交以作为机翼的旋转轴线; 耦合到铰链轴线的弹簧以在翼展开方向上施加旋转力; 固定销安装在所述翼中的所述铰链轴线附近，并且其一端联接到沿纵向方向弹性变形的压缩弹簧; 以及具有固定在所述机架上的第一表面的U形夹和在与所述铰链轴线交叉的与所述第一表面交叉的方向上延伸的第二表面，通过使所述固定销的另一端接触而形成滑动路径，并且形成凹部 与路径一端的固定销的另一端互锁。
-
-
-
-
-
-
Search Results
7
records
(took 0.017 seconds)
