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公开(公告)号：KR101517301B1
公开(公告)日：2015-05-04
申请号：KR1020130142315
申请日：2013-11-21
Applicant: 한국항공우주연구원
CPC classification number: B64G7/00 , B64G2007/005 , G01B11/26
Abstract: 본발명은열진공챔버내 시험대상물의각도를조절하기위한각도조절장치및 방법에관한것으로, 상기장치는상기시험대상물이탑재되는시험대상물탑재부와; 상기시험대상물의각도를측정하는각도센서와; 상기각도센서로부터획득한시험대상물의각도를기설정값과비교한후 각도조절을위한제어신호를전송하는제어부와; 상기제어부로부터제어신호를수신하여상기시험대상물탑재부를상하방향으로이동시키는각도조절부를포함하는것을특징으로한다.
Abstract translation: 本发明涉及一种用于调节热真空室中接触物体的角度的装置及其方法。 所述装置包括：测试对象加载单元，其中加载测试对象; 测量被测物的角度的角度传感器; 控制单元，其将从所述角度传感器获得的测试对象的角度与预定义的值进行比较，并且传送控制信号以调整角度; 以及角度调节单元，其接收来自所述控制单元的控制信号以使所述测试对象加载单元上下移动。 本发明的目的是提供一种用于调节热真空室中接触物体的角度的装置和方法，以在热真空测试期间测量，控制和保持测试对象的角度。
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公开(公告)号：KR101514571B1
公开(公告)日：2015-04-23
申请号：KR1020130148879
申请日：2013-12-03
Applicant: 한국항공우주연구원
Abstract: 본발명은열전대라우터및 이를이용한온도측정시스템에관한것이다. 본발명의열전대라우터는열전대를수용하기위한다수의하부삽입홈이구비된하부몸체; 및상기하부몸체와힌지결합되며, 열전대를수용하기위한다수의상부삽입홈이구비된상부몸체를포함하는것을특징으로한다.
Abstract translation: 本发明涉及一种热电偶路由器和使用该热电偶路由器的温度计系统。 根据本发明，热电偶路由器包括：具有多个下部插入槽以接收热电偶的下部主体; 并且与下体铰接的上体具有多个上插入槽以接收热电偶。
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83.发明授权위트니스 플레이트용 핀셋 및 위트니스 플레이트용 가위형 핀셋 有权WITNESS PLATE和SCISSORS TWEEZERS FOR TWITZERS TYPE TWEEZERS FOR WITNESS PLATE
公开(公告)号：KR101480245B1
公开(公告)日：2015-01-13
申请号：KR1020130106852
申请日：2013-09-05
Applicant: 한국항공우주연구원
Abstract: 본 발명은 위트니스 플레이트용 핀셋 및 위트니스 플레이트용 가위형 핀셋에 관한 것으로, 더욱 상세하게는 받침대를 설치하여 종래의 끝이 날카로운 핀셋에 비해 오염측정 내지 세척시 안정적으로 파지할 수 있는 위트니스 플레이트용 핀셋 및 위트니스 플레이트용 가위형 핀셋에 관한 것이다.
Abstract translation: 本发明涉及用于见证板的镊子和用于见证板的剪刀式镊子。 更具体地说，与具有尖端的传统镊子相比，用于见证板的镊子和用于见证板的剪刀式镊子可以通过在污染测量或洗涤的情况下安装支撑板来稳定地抓握。 根据本发明的用于目击板的镊子包括：第一支撑件; 第二支撑件，其在所述第一支撑件中延伸并且具有带有所述第一支撑件的弹性结构; 以及形成在第一支撑件和第二支撑件的端部上的第一支架和第二支架，并且放置证人板。
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公开(公告)号：KR1020140077431A
公开(公告)日：2014-06-24
申请号：KR1020120146246
申请日：2012-12-14
Applicant: 한국항공우주연구원
CPC classification number: B64G7/00 , B64G2007/005 , G01M99/00
Abstract: The present invention relates to a vacuum pump for a high-altitude test and a chamber for a high-altitude test using the same and, more specifically, to a vacuum pump for a high-altitude test which controls an altitude rising rate inside a chamber for a high-altitude test by comprising an inverter to control the number of rotations of a motor in the vacuum pump; and to a chamber for a high-altitude test using the same. The vacuum pump for a high-altitude test controls an altitude rising rate inside a chamber, and comprises an inverter for controlling the number of revolutions of a motor. A chamber for a high-altitude test using the vacuum pump is controlled by the vacuum pump which uses the inverter to control the number of revolutions of a motor in order to control an altitude rising rate in the chamber.
Abstract translation: 本发明涉及一种用于高空测试的真空泵和使用该真空泵的高空测试室，更具体地说，涉及一种控制室内高度上升速率的高空测试用真空泵 用于通过包括用于控制真空泵中的电动机的转数的逆变器来进行高空测试; 并使用该舱室进行高空测试。 用于高空测试的真空泵控制室内的高度上升速率，并且包括用于控制电动机的转数的逆变器。 使用真空泵进行高空试验的室由真空泵控制，该真空泵使用逆变器来控制电动机的转数，以便控制室中的高度上升速率。
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公开(公告)号：KR1020140028851A
公开(公告)日：2014-03-10
申请号：KR1020120096081
申请日：2012-08-31
Applicant: 한국항공우주연구원
CPC classification number: B64G7/00
Abstract: The present invention relates to a device for transferring radiant heat and, more specifically, a device for transferring radiant heat capable of improving reliability of an experiment result and maximizing convenience of a user. The device for transferring radiant heat is economical as the device is simplified. The device for transferring radiant heat includes a plate-shaped radiant heat radiation unit (100) including a space unit inside; a fluid path (200) installed in the space unit of the plate-shaped radiant heat (100); and a radiant heat change unit (300) formed as a radiation factor change matter changing a radiation factor is coated on the outer surface of the radiant heat radiation unit (100).
Abstract translation: 本发明涉及一种用于传递辐射热的装置，更具体地说，涉及一种用于传递辐射热的装置，其能够提高实验结果的可靠性并最大化用户的便利性。 用于传递辐射热的装置是经济的，因为装置被简化。 用于传递辐射热的装置包括内部包括空间单元的板状辐射热辐射单元（100） 安装在板状辐射热（100）的空间单元中的流体路径（200）; 在辐射热辐射单元（100）的外表面上涂布形成为辐射因子改变物质的辐射换热单元（300）。
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Patent Agency Ranking
公开(公告)号：KR1020140014586A
公开(公告)日：2014-02-06
申请号：KR1020120080961
申请日：2012-07-25
Applicant: 한국항공우주연구원
Abstract: The present invention relates to a cryogenic thermal environment test device using direct injection of liquid nitrogen and more specifically, to a cryogenic thermal environment test device using direct injection of liquid nitrogen which is capable of providing a cryogenic environment of temperatures lower than -100 degrees Celsius which is a necessary condition for testing a structure used in space, and which is capable of efficiently controlling the flux of liquid nitrogen using a pressure modulating valve, influx modulating valve and a control unit. [Reference numerals] (AA) Control unit
Abstract translation: 本发明涉及使用直接喷射液氮的低温热环境测试装置，更具体地说，涉及一种使用直接喷射液氮的低温热环境测试装置，其能够提供低于-100摄氏度的低温环境 这是用于测试在空间中使用的结构的必要条件，并且其能够使用压力调节阀，流入调节阀和控制单元来有效地控制液氮的通量。 （附图标记）（AA）控制单元
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公开(公告)号：KR101306017B1
公开(公告)日：2013-09-12
申请号：KR1020110142370
申请日：2011-12-26
Applicant: 한국항공우주연구원
Abstract: 본 발명은 포트 플레이트를 설치하거나 탈거할 때 작업 인력을 최소화하고 작업을 용이하게 할 수 있는 포트 플레이트 착탈용 지그를 제공하는 것이 그 기술적 과제이다. 이를 위해, 본 발명의 포트 플레이트 착탈용 지그는 챔버의 외면 중 포트의 주변에 구비되어 상기 포트의 위치에 포트 플레이트를 지지시키는 지지 유닛을 포함한다. 지지 유닛은 챔버에 구비되는 한 쌍의 평행 지지대와, 그리고 한 쌍의 평행 지지대에 가로 질러 구비되며 포트 플레이트를 지지하는 가로 지지대를 포함한다.
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公开(公告)号：KR1020130074340A
公开(公告)日：2013-07-04
申请号：KR1020110142370
申请日：2011-12-26
Applicant: 한국항공우주연구원
CPC classification number: B25B11/02 , B64G2007/005
Abstract: PURPOSE: A jig for attaching and detaching a port plate is provided to reduce a work load because a worker does not need to lift up a port plate when the port plate is installed. CONSTITUTION: A jig for attaching and detaching a port plate comprises a support unit (100). The support unit is formed around the port of a chamber and supports a port plate (20) to the port of the chamber. The support unit comprises a pair of parallel supports (110) and horizontal supports (120). The parallel supports are formed in the chamber. The horizontal supports cross the parallel supports and support the port plate.
Abstract translation: 目的：提供用于连接和拆卸端口板的夹具，以减少工作负载，因为工作人员在安装端口板时不需要抬起端口板。 构成：用于安装和拆卸端口板的夹具包括支撑单元（100）。 支撑单元形成在室的端口周围并且支撑到腔室的端口的端口板（20）。 支撑单元包括一对平行支撑件（110）和水平支撑件（120）。 平行支撑件形成在腔室中。 水平支架穿过平行支撑并支撑端口板。
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公开(公告)号：KR1020130047966A
公开(公告)日：2013-05-09
申请号：KR1020110112819
申请日：2011-11-01
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A blower device for high-temperature or cryogenic gas is provided to accurately simulate a space environmental test of a satellite on the ground by circulating the high-temperature or cryogenic gas into a shroud. CONSTITUTION: A blower device for high-temperature or cryogenic gas comprises a blower case(101), a blower(110), a heat exchanger(130), and an airtight member(150). The blower is embedded in the blower case and supplies the high-temperature or cryogenic gas. The heat exchanger circulates heat exchange mediums to the internal space of the blower case to prevent the heating of a blower motor due to the gas supplied by the blower. The airtight member seals a driving shaft of the blower so that the driving shaft of the blower cannot come in contact with the gas supplied by the blower.
Abstract translation: 目的：提供用于高温或低温气体的鼓风装置，以通过将高温或低温气体循环到护罩中来准确模拟地面上卫星的空间环境试验。 构成：用于高温或低温气体的鼓风装置包括鼓风机壳体（101），鼓风机（110），热交换器（130）和气密构件（150）。 鼓风机嵌入鼓风机壳体中，并提供高温或低温气体。 热交换器将热交换介质循环到鼓风机壳体的内部空间，以防止由鼓风机提供的气体导致鼓风机马达的加热。 气密部件密封鼓风机的驱动轴，使得鼓风机的驱动轴不能与由鼓风机供应的气体接触。
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公开(公告)号：KR101260193B1
公开(公告)日：2013-05-06
申请号：KR1020110136140
申请日：2011-12-16
Applicant: 한국항공우주연구원
IPC: G01M3/20
Abstract: PURPOSE: A device and a method for sensing a leakage are provided to sense leakages generated in several spots of a target object simultaneously by sensing the leakages by using infrared rays. CONSTITUTION: A device(1) for sensing a leakage comprises a supply unit(10) and a sensing unit(20). The supply unit supplies a sensitizer to the inside of a target object. The sensing unit senses the existence of a leakage of the sensitizer from the target object by using infrared rays. The supply unit supplies the sensitizer to the inside of the target object after heating.
Abstract translation: 目的：提供用于感测泄漏的装置和方法，以通过使用红外线感测泄漏来同时感测目标物体的若干点中产生的泄漏。 构成：用于感测泄漏的装置（1）包括供应单元（10）和感测单元（20）。 供应单元向目标物体的内部提供敏化剂。 感测单元通过使用红外线来感测敏化剂从目标物体泄漏的存在。 供电单元在加热后将敏化剂供应到目标物体的内部。
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