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公开(公告)号：KR1020040040698A
公开(公告)日：2004-05-13
申请号：KR1020020068897
申请日：2002-11-07
Applicant: 한국항공우주연구원
IPC: G01K7/02
Abstract: PURPOSE: A method for measuring the operational temperature of a heater circuit is provided to simply and easily measure the operational temperature of a heater circuit equipped with a low-temperature thermostat. CONSTITUTION: An ambient temperature of a low-temperature thermostat is lowered by using evaporation heat of a dry ice(6). Thus, power is supplied to a heater(2) so that the temperature of the heater(2) is increased. If the temperature of the heater(2) exceeds the temperature of the thermostat(3), power applied to the heater(2) is shielded so that the heater(2) is again cooled. In order to lower the temperature of a test sample, the dry ice(6) is positioned adjacent to the test sample by gripping the dry ice(6) using a gripper(7) made from plastic.
Abstract translation: 目的：提供一种用于测量加热器电路的工作温度的方法，以简单且容易地测量配备有低温恒温器的加热器电路的工作温度。 构成：使用干冰的蒸发热（6）降低低温恒温器的环境温度。 因此，向加热器（2）供电，使得加热器（2）的温度升高。 如果加热器（2）的温度超过恒温器（3）的温度，则屏蔽加热器（2）的功率，从而再次冷却加热器（2）。 为了降低测试样品的温度，使用由塑料制成的夹具（7）夹住干冰（6）将干冰（6）定位在测试样品附近。
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公开(公告)号：KR1020030050315A
公开(公告)日：2003-06-25
申请号：KR1020010080728
申请日：2001-12-18
Applicant: 한국항공우주연구원
IPC: B64G7/00
Abstract: PURPOSE: A sample support of a thermal vacuum chamber is provided to reduce a testing time by quickly adjusting the temperature of a base plate of a satellite component. CONSTITUTION: An upper plate(1) of a sample support is located inside a thermal vacuum chamber. A satellite structure putting a satellite component and a thermal filler are combined through a fixing bolt by forming many fixing holes(2) in the upper plate. A sample support(20) is formed in the lower part of the upper plate. The sample support comprises a thermal exchanging pipe(9) having an inlet(3) and an outlet. Thereby, the reliable environment test is possible by realizing the same value as an actual contact heat transfer.
Abstract translation: 目的：提供热真空室的样品支架，通过快速调节卫星部件底板的温度来减少测试时间。 构成：样品支架的上板（1）位于热真空室内。 通过在上板中形成许多固定孔（2），通过固定螺栓将放置卫星部件和热填料的卫星结构组合在一起。 样品支撑件（20）形成在上板的下部。 样品支架包括具有入口（3）和出口的热交换管（9）。 因此，通过实现与实际接触热传递相同的值，可靠的环境测试是可能的。
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公开(公告)号：KR100341006B1
公开(公告)日：2002-06-20
申请号：KR1019990064653
申请日：1999-12-29
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: 본발명은우주환경시험장치인열진공챔버에서우주환경시험시시험물을원하는온도에빨리도달하게하여주는시험보조장치(Fixture)에관한것으로열진공챔버내부에서열교환장치인슈라우드(Shroud)와시험물간의열교환시열전도를유발시켜열전달을향상시킴으로써시험시간을단축시키도록하는슈라우드접촉을이용한열진공챔버용시험보조장치에관한것이다. 고진공환경하에서는대류에의한열전달은소멸되고복사에의한열전달이지배하게되는데, 이경우극저온영역에서의복사열전달은매우미약하여우주환경을모사하는열진공시험시원하는온도에도달하는데장시간이필요하게된다. 따라서슈라우드의곡면과접촉되는시험물지지대와보조날개를대칭되도록형성하여슈라유드와시험물간에전도에의한열전달을많이유발시켜시험시간을단축하고액체질소소비량의감소, 작업자의근무시간단축및 고가장비의수명을연장하는것이다.
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Patent Agency Ranking
公开(公告)号：KR1020020042109A
公开(公告)日：2002-06-05
申请号：KR1020000071869
申请日：2000-11-30
Applicant: 한국항공우주연구원
IPC: F28D15/02
CPC classification number: F28D15/0233 , F28D15/0275
Abstract: PURPOSE: A method for arranging heat pipe with identical shape using line contact is provided to form uniform distribution of temperature by efficiently dispersing concentrated heat load. CONSTITUTION: Heat pipes(10) contacts with each other on lines to form regular polygons such as hexagons and quadrangles to exchange heat. The heat pipes layered upon another to contact with each other on lines. The heat pipes are manufactured by same process as the shape thereof is identical. The weight of needed heat pipes is reduced in comparison with usual method when the heat pipes are to be densely used so as to be applied to a communication satellite.
Abstract translation: 目的：提供一种使用线接触排列具有相同形状的热管的方法，通过有效地分散集中热负荷来形成均匀的温度分布。 构成：热管（10）在线上彼此接触以形成正六边形和四边形的常规多边形以交换热量。 层叠在另一个上的热管在线上彼此接触。 热管通过与其形状相同的相同工艺制造。 当热管被密集使用以便应用于通信卫星时，与常规方法相比，所需热管的重量减少。
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公开(公告)号：KR100315552B1
公开(公告)日：2001-12-20
申请号：KR1019990020849
申请日：1999-06-05
Applicant: 한국항공우주연구원
IPC: B64G1/66
Abstract: 본발명은우주환경시험장치인열진공챔버에서, 우주환경시험시시험물질표면에서발생된출기물(outgassing)을흡착하는흡착식오염방지판에관한것으로, 오염방지판을냉각시키는데필요한극저온냉매의소모량을절감시키도록하는흡착식오염방지판의극저온냉매소비절감장치에관한것이다. 이러한본 발명은흡착식오염방지판또는슈라우드(Shroud)의 LN2 공급구리관에전자개폐밸브를설치하고오염방지구리판의온도이외에구리관출구쪽 온도에따라밸브를개폐하게하고, 구리관의출구쪽 구리판또는슈라우드보다높은위치에상 분리기형태의가스탱크를설치하므로써이루어지는것이다.
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公开(公告)号：KR1020010064451A
公开(公告)日：2001-07-09
申请号：KR1019990064653
申请日：1999-12-29
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: PURPOSE: A fixture for a heat vacuum chamber using shroud contact is provided to rapidly reach the wanted temperature of a test object by improving the efficiency of heat transfer, and reduce consumpted amount of liquid nitrogen and work time. CONSTITUTION: A fixture for a heat vacuum chamber using shroud contact includes test object rests(1,2) having a curved surface equal to a shroud(8) and directly contacted with the shroud for inducing radiation, auxiliary blades(3,4) connected with the test object rests and oppositely formed to be coupled with the curved surface of the shroud by using thin metal, so that the temperature of a test object(9) promptly reaches desired temperature.
Abstract translation: 目的：提供使用护罩接触的热真空室的固定装置，通过提高传热效率快速达到被测物体的所需温度，并减少液氮消耗量和工作时间。 构成：用于使用护罩接触的热真空室的固定装置包括具有等于护罩（8）的弯曲表面并与护罩直接接触以引起辐射的测试对象静止件（1,2），辅助叶片（3,4）连接 测试对象静止并相反地形成为通过使用薄金属与护罩的弯曲表面联接，使得测试对象（9）的温度迅速达到期望的温度。
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公开(公告)号：KR100267024B1
公开(公告)日：2000-10-02
申请号：KR1019980018076
申请日：1998-05-20
Applicant: 한국항공우주연구원
IPC: B64G7/00
Abstract: PURPOSE: A thermal vacuum chamber is provided to perform a thermal vacuum test of components more efficiently and conducting a thermal equilibrium test by removing a sample holder. CONSTITUTION: A contact rod(11) longitudinally contacted inside a shroud is established and a lower part of the contact rod is formed to enlarge a contact face with respect to the shroud. On upper part of the contact rod, a holder(12) is fixed and a heat pipe(13) is installed on a bottom of the holder. In case of arranging a sample holder(10) in the shroud, an aluminum foil is covered and the sample holder is put thereon. Method of fixing the sample holder to the shroud with a bolt stably secures heat conductivity. When heat conductivity occurs through the contact rod in the shroud, the heat pipe is used for keeping a temperature change rapidly and uniformly of the holder. For easy replacement of the heat pipe with a copper bar, the heat pipe is fitted to a fixing metal piece(14) and fixed to the holder with a nut.
Abstract translation: 目的：提供热真空室，以更有效地进行部件的热真空测试，并通过移除样品架进行热平衡测试。 构成：建立纵向接触护罩内的接触杆（11），接触杆的下部形成为相对于护罩扩大接触面。 在接触杆的上部，保持器（12）固定，并且热管（13）安装在保持器的底部。 在将样品架（10）布置在护罩中的情况下，覆盖铝箔并将样品保持器放置在其上。 用螺栓将样品架固定在护罩上的方法可以稳定地保证导热性。 当通过护罩中的接触杆发生热传导时，热管用于保持保持器的温度变化迅速且均匀。 为了方便用铜棒更换热管，热管安装在固定金属片（14）上，并用螺母固定在支架上。
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公开(公告)号：KR100141612B1
公开(公告)日：1998-07-15
申请号：KR1019940040798
申请日：1994-12-31
Applicant: 한국항공우주연구원
IPC: B64G7/00
CPC classification number: B64G2007/005
Abstract: 본 발명은 우주환경을 모사하여 위성체의 신뢰성을 시험하는 열진공 챔버에 있어서, 열진공 챔버의 외부에서 위성체에 관련된 각종 작업을 용이하게 하고 위성체를 안전하게 열진공 챔버의 내부로 이송시킬 수 있도록 하는테이블 리프트를 이용한 열진공 챔버용 위성작업대에 관한 것으로 본 발명은 우주 환경을 시험하는 도어 분리식 열진공 챔버에 있어서, 개방된도어와 챔버 사이에 설치되고도어의 위성체지지대를 하부에서 지지시키며 도어 닫음시 접철되어가며 위성체를 챔버 내부로 이송시키는테이블 리프트로 이루어지는 것이다.
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