专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明专利

JP2003341600A Apparatus assembly of satellite apparatus panel and apparatus removal device for satellite apparatus panel 有权
标题翻译：卫星装置面板装置组装及卫星装置面板装置拆卸装置
公开(公告)号：JP2003341600A
公开(公告)日：2003-12-03
申请号：JP2002149739
申请日：2002-05-23
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： MORINAGA HIROTSUGU , OZAKI TAKESHI , KABASHIMA SHIGENORI
IPC分类号： B64G1/66 , B64G1/50
摘要： PROBLEM TO BE SOLVED: To provide an apparatus assembly having an adhesive layer formed by an adhesive only and having excellent heat radiation performance, and to provide an apparatus removal device for removing the apparatus without damaging the apparatus and panel even if the adhesive layer is formed by the adhesive only.
SOLUTION: The adhesive layer 4 is formed by an adhesive made by adding powder of filler having higher thermal conductivity than an adhesive as base material. The device includes a plate-like bed part 5a, leg parts 5b for supporting the bed part 5a provided on the lower side of both sides of the bed part 5a, a through hole 5c provided in a part of the bed part 5a opposite to a part for disposing the apparatus 3, a female screw part 5d provided in a part of the apparatus 3 opposite to the through hole 5c, a male screw rod 5e inserted in the through hole and the female screw parts 5c, 5d to be fastened, thereby jacking up the apparatus 3, and a scraper (an adhesive scraping tool) 5f.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供一种具有仅由粘合剂形成并且具有优异的散热性能的粘合剂层的装置组件，并且提供一种用于除去装置而不损坏装置和面板的装置去除装置，即使粘合剂层仅由粘合剂形成。解决方案：粘合剂层4由通过添加具有比作为基材的粘合剂更高的导热性的填料的粉末制成的粘合剂形成。该装置包括板状床部5a，用于支撑设置在床部5a的两侧的下侧的床部5a的腿部5b，设置在与床部5a相对的床部5a的一部分的通孔5c 用于设置设备3的部分，设置在与通孔5c相对的设备3的一部分中的阴螺纹部分5d，插入通孔中的外螺纹杆5e和待紧固的阴螺纹部分5c，5d，从而顶起装置3，以及刮刀（粘合剂刮削工具）5f。版权所有（C）2004，JPO

2. 发明专利

JP2003276700A Apparatus and method for thermal vacuum test of satellite 审中-公开
标题翻译：卫星热真空试验装置及方法
公开(公告)号：JP2003276700A
公开(公告)日：2003-10-02
申请号：JP2002088482
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , HAHN STEVEN , OZAKI TAKESHI
IPC分类号： B64G7/00
摘要： PROBLEM TO BE SOLVED: To shorten the time required for a thermal vacuum test by changing the attitude of a satellite as a test object without exposing a high vacuum vessel to the atmosphere during the thermal vacuum test of the satellite.
SOLUTION: A thermal vacuum test apparatus is provided with a holding mechanism comprising a temperature-adjustable and rotatable ring-like member, and a driving device. The thermal vacuum test can be correctly carried out in a short time while changing the attitude of the satellite without opening/ closing the high vacuum vessel.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：通过在卫星的热真空测试期间改变作为测试对象的卫星的姿态而不将高真空容器暴露在大气中，缩短热真空测试所需的时间。解决方案：热真空测试装置设置有包括温度可调和可旋转的环状构件的保持机构和驱动装置。在不打开/关闭高真空容器的同时改变卫星的姿态，可以在短时间内正确地进行热真空测试。版权所有（C）2004，JPO

3. 发明专利

JP2003347687A Circuit board and phased-array antenna 审中-公开
标题翻译：电路板和平面阵列天线
公开(公告)号：JP2003347687A
公开(公告)日：2003-12-05
申请号：JP2002154564
申请日：2002-05-28
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： MORINAGA HIROTSUGU , OZAKI TAKESHI , KABASHIMA SHIGENORI
IPC分类号： H05K1/02 , H01Q21/06
摘要： PROBLEM TO BE SOLVED: To uniformly radiate heat from all heat generating devices if a circuit board is mounted with a plurality of the heat generating devices.
SOLUTION: The circuit board 12 comprises a base having heat radiating property and a circuit portion 13 formed on the base. On the circuit board 12, for example, four heat generating devices 11, substantially identical in heat release value, are arranged in the circuit portion 13 in the direction of A. The coefficient of thermal conductivity of the base in the direction of B orthogonal to the direction of A is made larger than the coefficient of thermal conductivity of the base in the direction of A. Thus, heat generated by the heat generating devices 11 is substantially all conducted in the direction of B, and it is not conducted in the direction of A.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：如果电路板安装有多个发热装置，则从所有发热装置均匀地散发热量。解决方案：电路板12包括具有散热性能的基座和形成在基座上的电路部分13。在电路板12上，例如，四个热释放值大致相同的发热装置11沿着A方向排列在电路部分13中。基板的B方向的导热系数正交于使A的方向大于基体在A方向的导热系数。因此，由发热装置11产生的热量基本上全部沿B方向传导，并且不沿方向（C）2004，JPO

4. 发明专利

JP2003283241A Microstrip antenna 审中-公开
标题翻译： MICROSTRIP天线
公开(公告)号：JP2003283241A
公开(公告)日：2003-10-03
申请号：JP2002088477
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , OZAKI TAKESHI
IPC分类号： B01J13/00 , H01Q1/02 , H01Q1/38 , H01Q1/40 , H01Q13/08
摘要： PROBLEM TO BE SOLVED: To provide a microstrip antenna capable of being installed e.g. on the other structure and having good portability, although it has hitherto required strength and rigidity as an independent simple body structure of an antenna. SOLUTION: The microstrip antenna having good portability is provided with a flexible dielectric substrate having a predetermined elongation after rupture and dielectric loss tangent, a radiating element provided on one surface of the substrate, a ground conductor provided on the other surface of the substrate, and a feeding section for supplying radio waves to the radiating element. COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供能够安装的微带天线，例如，在另一结构上并且具有良好的便携性，尽管迄今为止，迄今为止需要强度和刚性作为天线的独立的简单体结构。解决方案：具有良好便携性的微带天线设置有在断裂和介电损耗角正切之后具有预定伸长率的柔性电介质基板，设置在基板的一个表面上的辐射元件，设置在基板的另一个表面上的接地导体基板和用于向辐射元件提供无线电波的馈电部分。版权所有（C）2004，JPO

5. 发明专利

JP2003276698A Artificial satellite 审中-公开
标题翻译：卫星
公开(公告)号：JP2003276698A
公开(公告)日：2003-10-02
申请号：JP2002088480
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , HAHN STEVEN , TAKADA SHIRO , TAKANO MASAHIRO
IPC分类号： B64G1/66 , H01Q1/28 , H01Q19/13
摘要： PROBLEM TO BE SOLVED: To ensure the directivity accuracy of antennas while maintaining the positional relationship of a plurality of antennas and radio wave radiators mounted on an artificial satellite structure.
SOLUTION: The directivity accuracy of antennas is ensured while maintaining the positional relationship of the antennas and radio wave radiators by providing an earth-directing surface panel including a carbon fiber reinforced composite material as a component material, a satellite structure, a mechanism to flexibly couple the earth-directing surface panel with the satellite structure, at least one antenna reflector, an antenna supporting structure including a carbon fiber reinforced composite material as a component material to couple the earth-directing surface panel with the antenna reflector, and an apparatus to control the directing direction of the earth-directing surface panel.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：确保天线的方向性精度，同时保持安装在人造卫星结构上的多个天线和无线电波辐射体的位置关系。解决方案：通过提供包括碳纤维增强复合材料作为组分材料的导向表面板，卫星结构，机构，确保天线的方向性精度，同时保持天线和无线电波辐射体的位置关系至少一个天线反射器，包括碳纤维增强复合材料的天线支撑结构，作为用于将导引表面面板与天线反射器耦合的组件材料的天线支撑结构，以及用于控制导向面板的引导方向的装置。版权所有（C）2004，JPO

6. 发明专利

JP2004019990A Sandwich panel with heat pipe 审中-公开
公开(公告)号：JP2004019990A
公开(公告)日：2004-01-22
申请号：JP2002173240
申请日：2002-06-13
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： MORINAGA HIROTSUGU , OZAKI TAKESHI , KABASHIMA SHIGENORI
IPC分类号： B64G1/50 , B32B27/36 , F28D15/02
CPC分类号： F28D15/02
摘要： PROBLEM TO BE SOLVED: To improve a heat radiation property and strength in a sandwich panel with a heat pipe. SOLUTION: A heat conductive member 15 composed of a composite material such as carbon-fiber reinforced resin or carbon-fiber reinforced carbon is joined to both the whole side faces 14d of the heat pipe 14. A cross sectional shape of the heat conductive member 15 is a right triangle, the upper face 24 of the heat conductive member 15 is joined to an upper skin 16, and a side face 25 of the heat conductive member 15 is joined to the side face 14d of the heat pipe 14. COPYRIGHT: (C)2004,JPO

7. 发明专利

JP2003291899A Artificial satellite structure 审中-公开
标题翻译：人造卫星结构
公开(公告)号：JP2003291899A
公开(公告)日：2003-10-15
申请号：JP2002099021
申请日：2002-04-01
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： TAKANO MASAHIRO , TAKADA SHIRO , KABASHIMA SHIGENORI , HAHN STEVEN
IPC分类号： B64G1/22 , B64G1/40
摘要： PROBLEM TO BE SOLVED: To provide an artificial satellite structure having a module configuration in which a payload assembly and a bus assembly are independent from each other to avoid cost increase due to complex design, and capable of mounting enough number of electronic devices on the payload assembly while maintaining the size and the strength at the same level as a conventional structure.
SOLUTION: The artificial satellite structure comprises a payload assembly 1 which is formed in the shape of a box by a payload assembly panel 3, and a bus assembly 2 which is formed at a lower end of the payload assembly 1 by a bus assembly panel 4. Four tubular type cylinders 5 are arranged in a square in the bus assembly 2, and inside each cylinder 5, fuel tanks 6 on which fuel is dividedly loaded are arranged and fixed to the cylinder by a plurality of tank support points 8 on the circumference.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：提供一种具有模块构造的人造卫星结构，其中有效载荷组件和总线组件彼此独立，以避免由于复杂设计而导致的成本增加，并且能够安装足够数量的电子设备在有效载荷组件上，同时将尺寸和强度保持在与常规结构相同的水平。解决方案：人造卫星结构包括通过有效载荷组件面板3形成为箱形的有效载荷组件1和总线组件2，总线组件2通过总线形成在有效载荷组件1的下端组合面板4.四个管状缸体5布置在总线组件2的正方形中，并且在每个气缸5内部，燃料被分开装载的燃料箱6通过多个罐支撑点8布置并固定到气缸在圆周上。版权所有（C）2004，JPO

8. 发明专利

JP2003276696A Heat pipe panel for satellite 审中-公开
标题翻译：卫星热管板
公开(公告)号：JP2003276696A
公开(公告)日：2003-10-02
申请号：JP2002088479
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , HAHN STEVEN , OZAKI TAKESHI
IPC分类号： B64G1/50 , F28D15/02
摘要： PROBLEM TO BE SOLVED: To mount appliances on both sides of a heat pipe panel, to dispose the panel inside a satellite, and, in particular, to mount a large number of TWTAs.
SOLUTION: Appliances are mounted on both sides of the heat panel, the panel is disposed inside the satellite, and, in particular, a large number of TWTAs are mounted by providing a heat pipe group comprising a skin with appliances mounted thereon, a honeycomb core in contact with the skin, and heat pipes in contact with the skin and embedded in the honeycomb core, a second heat pipe group comprising heat pipes in contact with the heat pipe group, orthogonal thereto, and embedded in the honeycomb core, a third heat pipe group comprising heat pipes in contact with the second heat pipe group, orthogonal thereto, and embedded in the honeycomb core, and a radiator having the skin on which the appliances in contact with the third heat pipe group and connected to the second heat pipe group.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：为了将设备安装在热管板的两侧，将面板放在卫星内，特别是安装大量的TWTA。
解决方案：将电器安装在散热板的两侧，面板设置在卫星内，特别是通过提供包括安装在其上的电器的皮肤的热管组来安装大量的TWTA，与皮肤接触的蜂窝芯和与皮肤接触并嵌入在蜂窝芯中的热管，第二热管组，包括与热管组接触的热管，与其垂直并嵌入在蜂窝芯中，第三热管组，其包括与第二热管组接触的热管，与其正交并嵌入在蜂窝芯中;以及散热器，其具有与第三热管组接触的器具并与第二热管组相连的散热器热管组。版权所有（C）2004，JPO

9. 发明专利

JP2003278826A Sandwich panel and artificial satellite structure having the same 审中-公开
标题翻译：三星面板和人造卫星结构
公开(公告)号：JP2003278826A
公开(公告)日：2003-10-02
申请号：JP2002088478
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , OZAKI TAKESHI
IPC分类号： B64G1/38 , F16F15/02
摘要： PROBLEM TO BE SOLVED: To make lightweight and simple a heavy and complicated satellite structure to withstand a vibration load upon launching.
SOLUTION: A sandwich panel having a light and simple structure has a vibration control system using both a sensor and an actuator in a characteristic frequency of 15 Hz to 35 Hz. A durability to vibration upon launching is improved and the sandwich panel is used for the satellite structure so that the satellite structure can be made lightweight and simple.
COPYRIGHT: (C)2004,JPO

10. 发明专利

JP2003276699A Artificial satellite 审中-公开
标题翻译：卫星
公开(公告)号：JP2003276699A
公开(公告)日：2003-10-02
申请号：JP2002088481
申请日：2002-03-27
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： KABASHIMA SHIGENORI , OZAKI TAKESHI , NOMURA TAKATSUGU
IPC分类号： B64G1/66 , B64G1/22 , H01Q1/28 , H01Q15/20
摘要： PROBLEM TO BE SOLVED: To mount a large antenna reflector on an artificial satellite.
SOLUTION: In the artificial satellite having a payload unit with a payload appliance mounted thereon, a bath unit with appliances to maintain the functions of the satellite mounted thereon, and a center cylinder to support the entire satellite, the payload unit and the bath unit are independent from each other, and the width between north and south sides of the payload unit is set to be smaller than the width between the north and south sides of the bath unit. An antenna holding structure is provided on the center cylinder at a boundary part between the payload unit and the bath unit. A large antenna reflector can be mounted, and the antenna orientation can be stably maintained.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：将大型天线反射器安装在人造卫星上。解决方案：在具有安装在其上的有效载荷装置的有效载荷单元的人造卫星中，具有用于保持安装在其上的卫星的功能的装置的浴室单元和用于支撑整个卫星的中心气缸，有效载荷单元和浴单元彼此独立，有效载荷单元的南北侧之间的宽度被设定为小于浴室单元的南北侧之间的宽度。天线保持结构设置在有效载荷单元和浴单元之间的边界部分的中心圆柱体上。可以安装大型天线反射器，并且可以稳定地保持天线方位。版权所有（C）2004，JPO

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式