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1. 发明专利

JP2006021710A Space structure attitude detection device 审中-公开
标题翻译：空间结构态度检测装置
公开(公告)号：JP2006021710A
公开(公告)日：2006-01-26
申请号：JP2004203340
申请日：2004-07-09
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： OTSUKA MASATAKA , OSHIMA TAKESHI , KONISHI YOSHIHIKO , NAGATSUKA TSUTOMU , TAKEMURA NOBUYASU , ISHII HIDETAKA
IPC分类号： B64G1/24 , B64G3/00 , G01C15/00
摘要： PROBLEM TO BE SOLVED: To directly measure attitude of a space structure for a specific point on the surface of the earth to improve its precision.
SOLUTION: A pilot beam transmission source 1 for transmitting microwaves AM-modulated by a signal wave expected in the space structure 2 and having wavelength of twice or more for the maximum value of difference d in measured distance is used. Pilot beam 4 is transmitted from the pilot beam transmission source 1 installed at the specific point on the earth. Pilot beam detection sensors 3a, 3b on the space structure 2 receive AM-modulated microwaves, sample the signal wave by demodulation, and detect its phase. The difference d in distance is calculated from difference in phase of both of them and the wavelength of the signal wave to detect attitude of the space structure 2 for the specific point on the earth.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：直接测量地球表面上特定点的空间结构的姿态，以提高其精度。解决方案：使用用于发射由空间结构2中预期的信号波AM调制并且以测量距离的最大差值d的波长为两倍或更多的微波的导频波束发射源1。导频波束4从安装在地球上的特定点的导频波束发射源1发射。空间结构2上的导频光束检测传感器3a，3b接收AM调制的微波，通过解调对信号波进行采样，并检测其相位。距离的差d由两者的相位差和信号波的波长来计算，以检测地球上特定点的空间结构2的姿态。版权所有（C）2006，JPO＆NCIPI

2. 发明专利

JP2004013010A REFLECTOR FOR OPTICAL INSTRUMENT LOADED ON SATELLITE 审中-公开
公开(公告)号：JP2004013010A
公开(公告)日：2004-01-15
申请号：JP2002169073
申请日：2002-06-10
申请人： MITSUBISHI ELECTRIC CORP
发明人： ISHII HIDETAKA , OZAKI TAKESHI
IPC分类号： G02B5/08 , G02B7/182
摘要： PROBLEM TO BE SOLVED: To obtain a reflector prepared for an optical instrument to be loaded on a satellite and capable of efficiently discharging heat generated on the mirror surface of the reflector and preventing the thermal distortion of the mirror surface. SOLUTION: In the reflector prepared for the optical instrument to be loaded on the satellite and having a mirror surface body 12 and an optical frame 10 for holding the mirror surface body 12, a heat conduction member 13 which is constituted of bundling high heat conducting fibers 14 and allowed to be flexibly deformed is arranged between the mirror surface body 12 and the optical frame 10 so that one end of the member 13 in the fiber direction is connected to the rear face of the mirror surface body 12 and the other end is connected to the optical frame 10. Both the end parts of the member 13 are stuck to the mirror surface body 12 and the optical frame 10 by high heat conductive adhesives. COPYRIGHT: (C)2004,JPO

3. 发明专利

JP2006320474A MATTRESS 审中-公开
公开(公告)号：JP2006320474A
公开(公告)日：2006-11-30
申请号：JP2005145338
申请日：2005-05-18
申请人： MITSUBISHI ELECTRIC CORP
发明人： USAMI AKIRA , ISHII HIDETAKA , OZAKI TAKESHI
IPC分类号： A61G7/05 , A47C27/10
摘要： PROBLEM TO BE SOLVED: To provide a light mattress which prevents formation or expansion of a bedsore on a patient by reducing selectively and automatically contact pressure applied on the bone projecting part where a bedsore is liable to be formed and on an already formed bedsore without increasing physical burdens of the patient. SOLUTION: The mattress 2 comprises a lamellar elastomer 4 for equalizing pressure applied on a loading body, a sheet 6 arranged on the top face of the elastomer 4, and a control apparatus 12. The sheet 6 has a plurality of cells 8 arranged between the loading body and the elastic body in the shape of a matrix and contain fluid supplied from a compressor 10 via an air pipe 16. Each of the cells 8 has a hole and a valve for taking in and discharging the fluid, and the control apparatus is connected to the valve of each hole via a connecting line so as to control opening and closing of each valve. Each cell 8 of the mattress 2 has a sensor connected to the control apparatus via a connecting line, and the control apparatus 12 directs opening and closing of the valve of each cell 8 in accordance with a signal from each sensor 8. COPYRIGHT: (C)2007,JPO&INPIT

4. 发明专利

JP2005017134A Deformation quantity measuring apparatus 有权
标题翻译：变形量测量装置
公开(公告)号：JP2005017134A
公开(公告)日：2005-01-20
申请号：JP2003183194
申请日：2003-06-26
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： ISHII HIDETAKA , OZAKI TAKESHI
IPC分类号： G01B11/16
摘要： PROBLEM TO BE SOLVED: To obtain a deformation quantity measuring apparatus which can measure the deformation quantity of a material stably with higher accuracy.
SOLUTION: The apparatus is provided with a laser interferometer 9 in a thermostatic humidistatic tank 14 and a test piece housing 12 facing the interferometer 9. The housing 12 is provided with a plane half-mirror 4 and a plane mirror 3 connected by a spring 5 to the half-mirror 4 with their mirror surfaces opposed. After reflecting the displacement of a test piece 1 due to the absorptive deformation on the positional relation of the plane mirror 3 with the half-mirror 4, the interferometer 9 measures the change quantity of interference fringes due to the interference of a reflected light from the plane mirror 3 with that from the half-mirror 4, thus measuring the deformation quantity of the test piece 1.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：获得能够以更高精度稳定地测量材料的变形量的变形量测量装置。解决方案：该设备在恒温恒湿箱14中设置有激光干涉仪9和面向干涉仪9的测试片壳体12.壳体12设置有平面半反射镜4和平面镜3，平面镜3由一个弹簧5到半镜4，镜面相对。在由于对平面镜3与半透半反镜4的位置关系的吸收变形反映测试片1的位移之后，干涉仪9测量由于来自反射镜3的反射光的干涉而引起的干涉条纹的变化量平面镜3与半反射镜4的角度对应，从而测量试件1的变形量。（C）版权所有（C）2005，JPO＆NCIPI

5. 发明专利

JP2003326622A High heat conduction honeycomb sandwich panel and panel loaded with equipment for artificial satellite provided with the sandwich panel 审中-公开
标题翻译：高强度蜂窝电话三面板和装载有用于人造卫星的设备的面板
公开(公告)号：JP2003326622A
公开(公告)日：2003-11-19
申请号：JP2002140572
申请日：2002-05-15
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： ISHII HIDETAKA , OZAKI TAKESHI
IPC分类号： B64G1/66 , B32B3/12
摘要： PROBLEM TO BE SOLVED: To obtain a high conduction honeycomb sandwich panel which is hot lower than 150 W/m/K in thermal conductivity in the surface direction and hot lower than 10 W/m/K in thermal conductivity in the thickness direction, and has a thermal expansion coefficient lower than that of an aluminum alloy honeycomb sandwich panel.
SOLUTION: A honeycomb core 2 and a skin 3 covering the both side surfaces of the honeycomb core 2 are provided. The skin 3 comprises C/C (Carbon/Carbon: carbon fiber reinforcing carbon) filled with a filler (metal or metal ceramic) having thermal conductivity higher than that of the skin 3. The volume ratio of the filler to the skin 3 is 5-10%. The honeycomb core 2 is made of CFRP (Carbon Fiber-Reinforced Plastic) in which the thickness direction coincides with the orientation direction of the carbon fibers.
COPYRIGHT: (C)2004,JPO
摘要翻译：要解决的问题：为了获得在表面方向热导率低于150W / m / K的热传导蜂窝夹层板，并且在厚度方面导热率低于10W / m / K 方向，热膨胀系数低于铝合金蜂窝夹芯板的热膨胀系数。解决方案：提供覆盖蜂窝芯2的两个侧表面的蜂窝芯2和皮肤3。皮肤3包含填充有导热率高于皮肤3的填料（金属或金属陶瓷）的C / C（碳/碳：碳纤维增强碳）。填料与皮肤3的体积比为5 -10％。蜂窝芯2由厚度方向与碳纤维的取向方向一致的CFRP（碳纤维增强塑料）制成。版权所有（C）2004，JPO

6. 发明专利

JP2003081199A Honeycomb sandwiched panel for satellite mounted optical equipment 有权
标题翻译：蜂窝电话用于卫星安装光学设备的三面板
公开(公告)号：JP2003081199A
公开(公告)日：2003-03-19
申请号：JP2001276996
申请日：2001-09-12
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： ISHII HIDETAKA , OZAKI TAKESHI
IPC分类号： B64G1/66 , B64G1/22
摘要： PROBLEM TO BE SOLVED: To solve the problem that troublesome labor is required for fabrication, there is a limit in the point of reduction weight, and the maximum thermal deformation of 5 μm causes the deformation of a reflecting mirror to possibly put a telescope into an unfocused condition and preclude the mounting of optical equipment having high resolution.
SOLUTION: This honeycomb sandwiched panel for satellite mounted optical equipment comprises a honeycomb core and a skin for covering both-side surfaces of the honeycomb core, the honeycomb core and the skin being formed of CFRP. It also has an outside honeycomb core arranged on a portion to which a heavier load is applied than to other portions and an inside honeycomb core lighter than the outside honeycomb core, which is arranged on a portion excluding the outside honeycomb core.
COPYRIGHT: (C)2003,JPO
摘要翻译：要解决的问题为了解决制造中需要麻烦的劳动的问题，减重重点是有限度的，5μm的最大热变形导致反射镜的变形，可能将望远镜放入未聚焦的条件，并排除了具有高分辨率的光学设备的安装。解决方案：这种用于卫星安装光学设备的蜂窝夹板包括蜂窝芯和用于覆盖蜂窝芯的两侧表面，蜂窝芯和皮肤由CFRP形成的皮肤。它还具有布置在比其他部分更重的负荷的部分上的外部蜂窝芯，以及布置在除了外部蜂窝芯之外的部分上的比外部蜂窝芯更轻的内部蜂窝芯。

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