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公开(公告)号：KR1020130129742A
公开(公告)日：2013-11-29
申请号：KR1020120053826
申请日：2012-05-21
Applicant: 국방과학연구소
Abstract: The present invention provides a wing unfolding apparatus comprising: a wing part which can be folded and unfolded; and a link assembling part which transfers driving force to the wing part by connecting the wing part to a drive part. The drive part comprises a cylinder; a piston which divides the inner space of the cylinder into first and second chambers; and a fluid inlet part which linearly moves the piston using the difference of power generated by the area difference between the top and bottom surfaces of the head of the piston when pressure is simultaneously applied to the first and second chambers.
Abstract translation: 本发明提供一种机翼展开装置，包括：可折叠和展开的翼部; 以及通过将翼部连接到驱动部而将驱动力传递到翼部的连杆组装部。 驱动部分包括气缸; 活塞，其将所述气缸的内部空间分成第一和第二腔室; 以及流体入口部分，当压力同时施加到第一和第二室时，使用由活塞头部的顶表面和底表面之间的面积差产生的功率的差异线性地移动活塞。
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公开(公告)号：KR100792181B1
公开(公告)日：2008-01-09
申请号：KR1020060100486
申请日：2006-10-16
Applicant: 국방과학연구소
Abstract: A device for attaching/detaching an umbilical to/from a side surface of a rocket is provided to keep a safe umbilical connection condition before launching of the rocket and separate the umbilical without causing damage to the umbilical after launching of the rocket. A device for attaching/detaching an umbilical to/from a side surface of a rocket(10) includes an umbilical gate unit(100) and a separating unit(200). The umbilical gate unit has one side on which a rocket side umbilical(20) is mounted. The umbilical gate unit is mounted on the side surface of the rocket such that the umbilical gate opens the side surface of the rocket when the rocket side umbilical and a launching tube side umbilical(30) are connected with each other, and closes the side surface of the rocket when the rocket side umbilical and the launching tube side umbilical are separated from each other. The separating unit is fixed on a launching tube and opposed to the umbilical gate unit. The separating unit has an inside in which the launching tube side umbilical is mounted. The launching tube side umbilical is connected to or separated from the rocket side umbilical.
Abstract translation: 提供了一种用于将脐带件附接到/从火箭的侧表面分离的装置，用于在发射火箭之前保持安全的脐带连接状态，并在发射火箭之后分离脐带而不会对脐带造成伤害。 用于将脐带件附接到火箭（10）的侧表面的装置包括脐带门单元（100）和分离单元（200）。 脐门单元具有安装有火箭侧脐带（20）的一侧。 脐门单元安装在火箭的侧表面上，使得当火箭侧脐带和发射管侧脐带（30）彼此连接时，脐门打开火箭的侧表面，并且关闭侧表面 当火箭侧脐带和发射管侧脐带彼此分离时。 分离单元固定在发射管上并与脐带门单元相对。 分离单元具有安装发射管侧脐带的内部。 发射管侧脐带与火箭侧脐带连接或分离。
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公开(公告)号：KR101438113B1
公开(公告)日：2014-09-12
申请号：KR1020120053826
申请日：2012-05-21
Applicant: 국방과학연구소
Abstract: 본 발명은 접힘 상태 및 전개 상태로 배치 가능한 날개부 및 상기 날개부와 구동부를 연결하여 상기 날개부에 구동력을 전달하는 링크조립부를 포함하며, 상기 구동부는 실린더와, 상기 실린더 내부 공간을 제1실 및 제2실로 구획하는 피스톤 및 상기 제1실 및 제2실에 동시에 압력을 가하여 피스톤 헤드 상면과 하면의 면적 차이에 의하여 발생하는 힘의 차이에 의해 상기 피스톤을 직선운동시키는 유체유입부를 포함하는 것을 특징으로 하는 날개 전개장치를 제공한다.
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