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公开(公告)号：KR1020150033065A
公开(公告)日：2015-04-01
申请号：KR1020130112567
申请日：2013-09-23
Applicant: 한국항공우주연구원
CPC classification number: B66C13/40
Abstract: 본발명은레이저거리측정기또는무선통신하는한 쌍의센서등다양한방식을이용하여 x, y, z 삼차원의거리정보를얻을수 있기때문에정밀한위치조절이가능하며, 사용자가거리정보를시각또는음성으로확인하면서크레인작업을할 수있는편의성을제공하는레이저거리측정기를이용한정밀위치조절이가능한크레인및 무선통신을이용한정밀위치조절이가능한크레인에관한것이다.
Abstract translation: 本发明涉及能够使用激光测距仪进行精确位置调整的起重机和能够使用无线通信进行精确位置调整的起重机，其允许通过获得x，y和3的三维距离信息来进行精确位置调整 z通过使用各种方法，例如激光测距仪或一对无线通信的传感器。 本发明在用户视觉上或声学地检查距离信息的同时提供起重机工作的便利。
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公开(公告)号：KR101421947B1
公开(公告)日：2014-07-28
申请号：KR1020130104735
申请日：2013-09-02
Applicant: 한국항공우주연구원
CPC classification number: B64G1/66
Abstract: Disclosed is a device for storing a satellite structure capable of being selectively used according to the shape of satellite structures to be stored. The device for storing a satellite structure comprises an upper plate and multiple brackets for satellite structure fixation. The upper plate is formed of a closed-loop surface with constant thickness and width. A satellite structure is placed on the top of the surface of the upper plate. Multiple upper plate holes for position adjustment are formed at regular intervals along the surface. Each bracket for satellite structure fixation comprises a base having the lower part coming in contact with the upper plate and bracket holes for position adjustment coupled to one among the multiple upper plate holes for position adjustment; a structure fixing wall formed on the top of the base at a constant height and having the front surface fixing the satellite structure toward the center of the upper plate; and a structure supporter formed on the top of the base at the constant height and supporting the rear surface of the structure fixing wall.
Abstract translation: 公开了一种用于存储能够根据要存储的卫星结构的形状选择性地使用的卫星结构的装置。 用于存储卫星结构的装置包括用于卫星结构固定的上板和多个支架。 上板由具有恒定厚度和宽度的闭环表面形成。 卫星结构放置在上板表面的顶部。 用于位置调节的多个上板孔沿着表面以规则的间隔形成。 用于卫星结构固定的每个支架包括具有与上板接触的下部的基座和用于位置调整的支架孔，用于位置调整，该多个上板孔中的一个用于位置调整; 结构固定壁，其形成在所述基座的顶部上，并且具有固定所述卫星结构朝向所述上板的中心的恒定高度; 以及在所述基座的顶部以恒定高度形成并支撑所述结构固定壁的后表面的结构支撑件。
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Patent Agency Ranking
公开(公告)号：KR1020140080708A
公开(公告)日：2014-07-01
申请号：KR1020120146038
申请日：2012-12-14
Applicant: 한국항공우주연구원
CPC classification number: B64G1/66 , B64G1/10 , B64G2700/24
Abstract: The present invention relates to a shock absorber and a strut shock absorber, and more specifically, to a shock absorber and a strut shock absorber having a relatively simpler structure to improves absorption of the vibration or shock of the strut per construction costs and preventing the effect of the vibration of the top mechanisms on the upper and lower parts of the strut from affecting each other by installing a strut with a pipe shape allowing easy transfer of vibration in the center to prevent the vibration from being transferred vertically through the strut.
Abstract translation: 减震器和支柱减震器技术领域本发明涉及减震器和支柱减震器，更具体地说，涉及一种具有相对简单结构的减震器和支柱减震器，以改善每个施工成本的支柱的振动或冲击的吸收并防止效果 通过安装具有允许容易地在中心传递振动的管状支柱的支柱的上部和下部上的顶部机构的振动的振动，以防止振动垂直地通过支柱传递。
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公开(公告)号：KR1020140080704A
公开(公告)日：2014-07-01
申请号：KR1020120146032
申请日：2012-12-14
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a carrying dolly device and, more specifically, to a carrying dolly device capable of accurately adjusting the horizontality of a backing plate when installed. The present invention comprises: a backing plate on which a satellite or parts of the same are placed; a plurality of supports fixed on the backing plate, while having wheels; a gear unit installed on the respective ends of the supports while converting a rotary motion into a linear motion to lift or lower the supports; a ground fixating plate fixed to the gear unit to fixate the supports by coming in contact with the ground when the gear unit is lowered; a rotary handle connected to the gear unit; and a rotation number display for measuring the rotation number of the gear unit.
Abstract translation: 本发明涉及一种携带轻便装置，更具体地，涉及一种能够在安装时能够精确地调节背板的水平度的携带轻便装置。 本发明包括：在其上放置卫星或其一部分的背板; 固定在背板上的多个支撑件，同时具有轮子; 减速器，其安装在所述支撑件的相应端部上，同时将旋转运动转换成直线运动以提升或降低所述支撑件; 固定在所述齿轮单元上的接地固定板，当所述减速器下降时通过与所述地面接触来固定所述支撑件; 连接到减速器的旋转手柄; 以及用于测量减速器的转速的转数显示。
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公开(公告)号：KR1020140071038A
公开(公告)日：2014-06-11
申请号：KR1020120138908
申请日：2012-12-03
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a pallet truck transferring a pallet by using a pair of forks capable of being lifted by being installed on a frame. The fork includes a plurality of mounting units formed on the upper part of an existing fork; a height control unit mounted on the mounting unit; and one or more piston units which is located between the mounting unit and the height control unit and controls the height of the height control unit. The frame includes a control unit on the upper part, wherein the control unit controls the height of the height control unit by controlling the piston.
Abstract translation: 本发明涉及一种通过使用能够通过安装在框架上被提升的一对叉子来转运托盘的托盘车。 叉子包括形成在现有叉子的上部上的多个安装单元; 安装在所述安装单元上的高度控制单元; 以及位于安装单元和高度控制单元之间并控制高度控制单元的高度的一个或多个活塞单元。 框架包括在上部的控制单元，其中控制单元通过控制活塞来控制高度控制单元的高度。
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公开(公告)号：KR101291593B1
公开(公告)日：2013-08-01
申请号：KR1020110091706
申请日：2011-09-09
Applicant: 한국항공우주연구원
Abstract: 본 발명은 전개 및 접힘 시험시 태양 전지판의 좌우 요동 없이 원활하게 가이드 할 수 있고, 그리고 여러 번의 전개 및 접힘 시험이 수행하더라도 균열을 최소화할 수 있는 인인공 위성용 태양 전지판 전개장치를 제공하는 것이 그 기술적 과제이다. 이를 위해, 본 발명의 인공 위성용 태양 전지판 전개장치는 인공 위성 몸체와 태양 전지판을 회동 가능하게 연결시키는 제1 힌지 유닛와, 인공 위성 몸체에 결합되며 중공 형상을 갖는 제1 전개 부재와, 태양 전지판에 결합되며 제1 전개 부재를 수용하여 중첩시킬 수 있도록 채널(channel) 형상을 갖는 제2 전개 부재와, 그리고 제1 및 제2 전개 부재가 서로 접혀짐과 펼쳐짐이 가능하도록 그 사이에 구비되는 제2 힌지 유닛을 포함한다.
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公开(公告)号：KR1020130028278A
公开(公告)日：2013-03-19
申请号：KR1020110091706
申请日：2011-09-09
Applicant: 한국항공우주연구원
CPC classification number: B64G1/443 , B64G2001/224 , H02S30/00
Abstract: PURPOSE: A solar panel unfolding apparatus for a satellite is provided to smoothly fold and unfold solar panels without lateral movement and to minimize cracks even if several folding and unfolding tests are implemented. CONSTITUTION: A solar panel unfolding apparatus for a satellite comprises a first hinge unit, a first unfolding member(200), a second unfolding member(300), and a second hinge unit(400). The first hinge unit rotatably connects a satellite body(10) and a solar panel(20). The second unfolding member is coupled to one side of the satellite body and has a hollow shape. The second unfolding member is coupled to one side of the solar panel corresponding to one side of the satellite body and has a channel shape to overlap the first unfolding member. The second hinge unit is arranged between the first and second members to fold and unfold the first and second members.
Abstract translation: 目的：提供一种用于卫星的太阳能电池板展开装置，以平滑地折叠和展开太阳能电池板而不会横向移动，并且即使实施了几个折叠和展开测试，也可最小化裂纹。 构成：用于卫星的太阳能电池板展开装置包括第一铰链单元，第一展开构件（200），第二展开构件（300）和第二铰链单元（400）。 第一铰链单元可旋转地连接卫星体（10）和太阳能面板（20）。 第二展开构件联接到卫星主体的一侧并且具有中空形状。 第二展开构件联接到对应于卫星体的一侧的太阳能面板的一侧，并且具有与第一展开构件重叠的通道形状。 第二铰链单元布置在第一和第二构件之间以折叠和展开第一和第二构件。
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