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公开(公告)号：KR101369564B1
公开(公告)日：2014-03-06
申请号：KR1020120152805
申请日：2012-12-26
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a rotational reaction force measuring device and a rotational reaction force measuring method and, more specifically, to a rotational reaction force measuring device and a rotational reaction force measuring method capable of accurately measuring rotational reaction force by crossing first and second elastic units at a right angle to disperse deformation concentrated on one direction.
Abstract translation: 旋转反作用力测量装置和旋转反作用力测量方法技术领域本发明涉及旋转反作用力测量装置和旋转反作用力测量方法，更具体地说，涉及一种旋转反作用力测量装置和旋转反作用力测量方法，该方法能够通过将第一和第二弹性 以直角分散变形的单元在一个方向上集中。
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公开(公告)号：KR101369545B1
公开(公告)日：2014-03-06
申请号：KR1020120146040
申请日：2012-12-14
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a sensor fixing device for vibration test using a ductile metal, and more specifically, to a sensor fixing device for vibration test using a flexible metal which is applied to uneven and various shapes of mounting surfaces and achieves cost savings and convenience of the test by having bocks which is to attach a sensor for vibration test and which is composed of ductile metals.
Abstract translation: 本发明涉及一种使用延性金属进行振动试验的传感器固定装置，更具体地说，涉及一种应用于不均匀和各种形状的安装表面的柔性金属进行振动试验的传感器固定装置，并且实现了成本节约和方便 的测试通过具有附接传感器用于振动测试并且由延性金属组成的块。
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公开(公告)号：KR101332060B1
公开(公告)日：2013-11-22
申请号：KR1020120080965
申请日：2012-07-25
Applicant: 한국항공우주연구원
CPC classification number: G01M7/027
Abstract: The present invention relates to a position controlling device for testing the vibration of a satellite comprising a pneumatic pump supplying air to the body of a vibration testing device in a position controlling device for parallel arranging of the body of the vibration testing device; a pressure controlling valve controlling the pressure of air supplied to the pneumatic pump; and a position and pressure controlling device receiving the current position of the body of the vibration testing device for indicating pressure value according to the current position before configuring the required pressure to a target pressure for positioning the body of the vibration testing device at the center before controlling the target pressure to be supplied to the body of the vibration testing device through controlling the pressure controlling valve. [Reference numerals] (10) Body of a vibration testing device
Abstract translation: 本发明涉及一种用于测试卫星的振动的位置控制装置，该位置控制装置包括在位置控制装置中向振动测试装置的主体供应空气的气动泵，用于平行布置振动测试装置的主体; 控制供给气动泵的空气的压力的压力控制阀; 以及位置和压力控制装置，其接收所述振动试验装置的本体的当前位置，用于在将所述压力构成所述压力之前根据当前位置指示压力值到用于将所述振动试验装置的主体定位在中心的目标压力 通过控制压力控制阀来控制提供给振动试验装置的主体的目标压力。 （附图标记）（10）振动试验装置的主体
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公开(公告)号：KR101299050B1
公开(公告)日：2013-08-21
申请号：KR1020110147242
申请日：2011-12-30
Applicant: 한국항공우주연구원
Abstract: 본 발명은 로켓 또는 항공기에 설치되는 전자제품의 엔진 소음으로 인한 피로 시험용 진행파 음향 튜브에 관한 것으로, 더욱 상세하게는 엔진 소음으로 인한 음향 진행파의 구현을 위해 진행파의 반사를 최소화화고, 진행파의 고주파 대역을 만족시켜 시험의 신뢰도를 높이는 피로 시험용 진행파 음향 튜브에 관한 것이다.
본 발명의 피로 시험용 고 에너지 음향 튜브는 하류단에서의 소음 리플랙션을 최소화 하여 엔진 소음과 같은 진행파의 구현에 충실하며, 에어스피커와 전자스피커를 혼용하여 고주파 영역의 소음 시험도 만족시켜 피로 시험의 신뢰도를 높일 수 있는 효과가 있다.-
Patent Agency Ranking
公开(公告)号：KR1020130068778A
公开(公告)日：2013-06-26
申请号：KR1020110136141
申请日：2011-12-16
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A height aligning device of an exciter bearing is provided to measure the height by directly fixing the device to the bearing, thereby obtaining an accurate result by minimizing errors generated by a measuring point. CONSTITUTION: A height aligning device of an exciter bearing comprises a bearing joining unit(10), a first measurement frame(20), a second measurement frame(30), a first length measuring unit(40), and a second length measuring unit(50). The bearing joining unit is joined to the exciter bearing. The first measuring frame is extended from one side of the bearing joining unit. The second measuring frame is extended from the other side of the bearing joining unit. The first length measuring unit is joined to the first measuring frame and measures a distance between the first measuring frame and a surface plate(200). The length measuring device is joined to the second measuring frame and measures a distance between the second measuring frame and the surface plate.
Abstract translation: 目的：提供一种激励器轴承的高度对齐装置，通过将装置直接固定在轴承上来测量高度，从而通过最小化测量点产生的误差来获得准确的结果。 构成：励磁机轴承的高度对准装置包括轴承接合单元（10），第一测量框架（20），第二测量框架（30），第一长度测量单元（40）和第二长度测量单元 （50）。 轴承接合单元连接到励磁机轴承。 第一测量框架从轴承接合单元的一侧延伸。 第二测量框架从轴承接合单元的另一侧延伸。 第一长度测量单元连接到第一测量框架并测量第一测量框架和表面板（200）之间的距离。 长度测量装置连接到第二测量框架并测量第二测量框架和表面板之间的距离。
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公开(公告)号：KR1020130067782A
公开(公告)日：2013-06-25
申请号：KR1020110134690
申请日：2011-12-14
Applicant: 한국항공우주연구원
CPC classification number: G01N3/303 , G01M7/08 , G01N2203/04
Abstract: PURPOSE: A release device of an impact testing device is provided to stably fix and support a falling object, thereby freely determining the weight of the falling object. CONSTITUTION: A release device(10) of an impact testing device comprises a gripper unit, an electromagnet, and a moving unit. The gripper is formed to be gathered or seized around a gripper axis and composed of: a gripper upper part with a magnetic reaction body; and a gripper lower part where a supporting unit supporting the underside of a falling object(20) is formed. The electric magnet pulls or pushes the magnetic reaction body by generating a magnetic force according to a power supply, thereby controlling the gripper unit from being gathered or seized. The moving unit moves the gripper unit in a vertical direction.
Abstract translation: 目的：提供冲击测试装置的释放装置，以稳定地固定和支撑坠落物体，从而自由地确定坠落物体的重量。 构成：碰撞测试装置的释放装置（10）包括夹持器单元，电磁体和移动单元。 夹持器形成为围绕夹持器轴线收集或抓住，并由以下部件组成：具有磁性反作用体的夹持器上部; 以及形成有支撑下落物体（20）的下侧的支撑单元的夹持器下部。 电磁体通过根据电源产生磁力来拉动或推动磁性体，由此控制夹持器单元的收集或卡住。 移动单元沿着垂直方向移动夹持单元。
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公开(公告)号：KR101082755B1
公开(公告)日：2011-11-10
申请号：KR1020090122622
申请日：2009-12-10
Applicant: 한국항공우주연구원
Abstract: 본발명은인공위성용광학렌즈의초정밀위치정렬장치에관한것으로, 보다상세하게는인공위성에사용되는광학렌즈의위치를 5축방향으로정밀하게정렬하여상기광학렌즈의위치를제어하기위한인공위성용광학렌즈의초정밀위치정렬장치에관한것이다. 본발명에따른인공위성용광학렌즈의초정밀위치정렬장치에의하면, X축방향으로각각이동하는제 1 X축스테이지및 제 2 X축스테이지와 Y축방향으로각각이동하는제 1 Y축스테이지및 제 2 Y축스테이지의위치정렬에의하여 X축, Y축및, Z축의 3축방향의병진운동(translation) 뿐만아니라 X축중심의회전운동(elevation)과 Y축중심의회전운동(azimuth)에대하여미세하고정밀한위치정렬을제어할수 있는현저한효과가있다.
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公开(公告)号：KR1020110065924A
公开(公告)日：2011-06-16
申请号：KR1020090122622
申请日：2009-12-10
Applicant: 한국항공우주연구원
Abstract: PURPOSE: An apparatus for aligning the position of a satellite optical lens is provided to control the alignment of the position with respect to the translation, the elevation, and the azimuth of an object and a telescopic sight. CONSTITUTION: A fixing frame(10) forms the Z-axis linear guide(12) on the upper side. The Z-axis stage(20) is mounted to be moved in the Z-axis direction along the Z-axis linear guide. A first X-axis stage(30) is mounted on the Z-axis stage to be moved in the X-axis direction along a first X-axis linear guide. A second X-axis stage(40) is mounted on the Z-axis stage to be moved in the Z-axis direction along a second X-axis linear guide. A first Y-axis stage(50) is mounted to be moved along the Y-axis direction along a first Y-axis linear guide(32). A second Y-axis stage(60) is mounted to be moved along the Y-axis direction along a second Y-axis linear guide(42).
Abstract translation: 目的：提供一种用于对准卫星光学透镜的位置的装置，以控制位置相对于物体和望远镜的平移，仰角和方位的对准。 构成：固定架（10）在上侧形成Z轴直线导轨（12）。 安装Z轴台（20）沿着Z轴线性导轨沿Z轴方向移动。 第一X轴平台（30）安装在Z轴平台上沿着第一X轴直线导轨沿X轴方向移动。 第二X轴平台（40）安装在Z轴台上沿着第二X轴直线导轨沿Z轴方向移动。 第一Y轴平台（50）安装成沿着Y轴方向沿着第一Y轴线性导轨（32）移动。 安装第二Y轴平台（60）沿着Y轴方向沿第二Y轴线性导轨（42）移动。
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公开(公告)号：KR101028493B1
公开(公告)日：2011-04-11
申请号：KR1020090110991
申请日：2009-11-17
Applicant: 한국항공우주연구원
CPC classification number: H02S20/30
Abstract: PURPOSE: A solar cell panel fixing device is provided to accurately position a solar cell panel on a satellite by including a fixing device which is vertically and horizontally controlled on the lower side of the solar cell panel. CONSTITUTION: A lower fixing unit(200) comprises a panel support unit, a vertical control unit, and a fixing unit. The panel support unit is connected to a solar cell panel(B). The panel support unit is integrated with a combination frame connected to the solar cell panel. The vertical control unit vertically moves the panel support unit. A pulling unit(100) pulls the solar cell panel to combine the solar cell panel with a satellite(S).
Abstract translation: 目的：提供一种太阳能电池板固定装置，通过在太阳能电池板的下侧包括垂直和水平控制的固定装置来将太阳能电池板精确地定位在卫星上。 构成：下固定单元（200）包括面板支撑单元，垂直控制单元和定影单元。 面板支撑单元连接到太阳能电池板（B）。 面板支撑单元与连接到太阳能电池板的组合框架集成。 垂直控制单元垂直移动面板支撑单元。 拉动单元（100）拉动太阳能电池面板以将太阳能电池面板与卫星（S）组合。
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