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1. 发明专利

JP2012183593A Electromagnetic hand, and robot system using the same 有权
标题翻译：电磁手柄和使用它的机器人系统
公开(公告)号：JP2012183593A
公开(公告)日：2012-09-27
申请号：JP2011046444
申请日：2011-03-03
申请人： Kawasaki Heavy Ind Ltd , 川崎重工業株式会社
发明人： AKAMATSU MASAHIKO , ENOMOTO MASAYUKI , YAMAMOTO TAKESHI , MIURA KATSUYA , TAKEMOTO YUTAKA
IPC分类号： B25J15/06 , B25J13/08
摘要： PROBLEM TO BE SOLVED: To pick workpieces stored in bulk state within a casing one by one without interruption and interference.SOLUTION: The robot system 10 includes a robot 12 picking the plurality of columnar or cylindrical workpieces W stored in bulk state within the casing C. The robot 12 includes an electromagnetic hand 18. The electromagnetic hand 18 includes: a main electromagnetic attraction part 20 electromagnetically attracting a circumferential face Wp or an end face We of the workpiece W by a first electromagnetic attraction face 20a; and an auxiliary electromagnetic attraction part 22 electromagnetically attracting the circumferential face Wp of the workpiece W by both second and third electromagnetic attraction faces 22a, 22b which are arranged at a tip 24 to form an obtuse angle or electromagnetically attracting the end face We of the workpiece W by either one of the second and third electromagnetic attraction faces 22a, 22b. The robot 12 picks each of the plurality of workpieces W in bulk state in the plurality of different electromagnetic attraction forms.
摘要翻译：要解决的问题：一个接一个地在壳体内以体积状态存储的工件不受中断和干扰。机器人系统10包括机器人12，其拾取在壳体C内以体积状态存储的多个柱状或圆柱形工件W.机器人12包括电磁手18.电磁手18包括：主电磁吸引第二部分20通过第一电磁吸引面20a电磁吸引工件W的周面Wp或端面We; 以及辅助电磁吸引部22，通过布置在尖端24处的第二和第三电磁吸引面22a，22b电磁吸引工件W的周面Wp，以形成钝角或电磁吸引工件的端面We W通过第二和第三电磁吸引面22a，22b中的任意一个。机器人12以多种不同的电磁吸引方式在批量状态下拾取多个工件W中的每一个。版权所有（C）2012，JPO＆INPIT

2. 发明专利

JP2012137380A Sampling device for combustion gas from combustor for gas turbine engines 有权
标题翻译：用于燃气涡轮机发动机燃烧气体的采样装置
公开(公告)号：JP2012137380A
公开(公告)日：2012-07-19
申请号：JP2010289725
申请日：2010-12-27
申请人： Japan Aerospace Exploration Agency , Kawasaki Heavy Ind Ltd , 川崎重工業株式会社 , 独立行政法人宇宙航空研究開発機構
发明人： KOBAYASHI MASAYOSHI , YAMADA HIDESHI , SHIMODAIRA KAZUO , YAMAMOTO TAKESHI , YAMAGUCHI KENTA
IPC分类号： G01N1/22 , G01M15/10 , G01N1/28
摘要： PROBLEM TO BE SOLVED: To provide a sampling device that can endure environment of high temperature and high pressure.SOLUTION: In a device 2 for sampling combustion gas G discharged from a combustor 12 for gas turbine engines, an inlet unit 11 has a gas inlet passage GP for letting in the combustion gas G discharged from the combustor 12 and a cooling passage CP for letting cooling water C for cooling the gas inlet passage GP flow; a drive mechanism K causes the inlet unit 11 to rotate around its axial part 30; a supporting unit 34 has a gas communicating path 77 and cooling water communicating paths 81 and 83 respectively communicating with the gas inlet passage GP and the cooling passage CP of the inlet unit 11, and the axial part 30 is rotatably linked to it; to the supporting unit 34, a gas outlet pipe 98 for letting the combustion gas G out, a cooling water inlet pipe 78 for letting in the cooling water C from outside and a cooling water outlet pipe 96 for letting the cooling water C out are connected.
摘要翻译：要解决的问题：提供可承受高温高压环境的取样装置。解决方案：在用于对从燃气涡轮发动机的燃烧器12排出的燃烧气体G进行采样的装置2中，入口单元11具有用于使从燃烧器12排出的燃烧气体G中的冷却通道用于使用于冷却气体入口通道GP的冷却水C的流量; 驱动机构K使入口单元11围绕其轴向部分30旋转; 支撑单元34具有分别与进气通道GP和入口单元11的冷却通道CP连通的气体连通路径77和冷却水连通路径81和83，并且轴向部分30可旋转地连接到其上; 连接到支撑单元34，连接用于使燃烧气体G输出的气体出口管98，用于从外部排出冷却水C的冷却水入口管78和用于使冷却水C出出的冷却水出口管96 。版权所有（C）2012，JPO＆INPIT

3. 发明专利

JPH07125699A FAILURE DIAGNOSING METHOD FOR HELICOPTER 失效
公开(公告)号：JPH07125699A
公开(公告)日：1995-05-16
申请号：JP29390293
申请日：1993-10-29
申请人： JAPAN TECH RES & DEV INST , KAWASAKI HEAVY IND LTD
发明人： NIWA YOSHIYUKI , AEBA MASAYUKI , BANDO SHUNICHI , YAMAMOTO TAKESHI , ASO MITSUHIRO , KAWAGUCHI HITOSHI
IPC分类号： G01M99/00 , B64D45/00 , G01H13/00 , G01M19/00
摘要： PURPOSE:To provide a highly safe failure diagnosing method which makes an excitation device periodically excite an airframe during flight, and detects the resultant vibration of the air frame through an analysis device to judge a failure for making stable diagnosis possible to dispense with overhaul. CONSTITUTION:The vibration characteristics of an airframe 7 can be shown as an amplitude enlarging rate, which is about constant independently of flight conditions. Thus it is proper for the diagnosis of failure to base on the amplitude enlarging rate. The measurement of the amplitude enlarging rate is carried out in such 3 way as an actuator 8 serving as an exciting device is arranged on one of coupling links 6 between a support member 5 and the air frame 7, and excited by a signal issued from a control computer 9 serving as an analysis device. Frequency in this case is different from the frequency of air exciting force, and the frequency in which the amplitude enlarging rate varys greatly is selected. The exciting force and a signal issued from an acceleration sensor 10 are mutually compared, and the amplitude enlarging rate can therefore be obtained. Since the amplitude enlarging rate at a normal time is entirely different from that at she time of failure, the failure can be easily diagnosed.

4. 发明专利

JPS529286A METHOD OF REDUCING A TRANSVERSAL STRENGTH OF A HULL 失效
公开(公告)号：JPS529286A
公开(公告)日：1977-01-24
申请号：JP8487075
申请日：1975-07-09
申请人： KAWASAKI HEAVY IND LTD
发明人： YAMAMOTO TAKESHI
IPC分类号： B63B3/00
摘要： PURPOSE:To reduce an external load acting on a transversal strength member in a hold.

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