排序方式: 共有41条查询结果,搜索用时 15 毫秒
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研制了一种小角度超声纵波特种斜探头,用于台阶形金属/非金属异形复合构件粘接界面的检测,选择了探头材质,计算了入射倾角,建立了伤方法及判伤标准,并在对比试块及实际产品上进行了检测,证明了该探头及方法适用于该特定形状产品的探伤,并对类似异种形面产品的探伤有参考意义。 相似文献
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介绍了卫星推进系统气体流量探头设计中的几个问题,该探头适用微波量气体流量的测量,采用了差压式孔板流量计的原理,设计轻巧,使用方便,能够进行远距离无失真传输,方便了现场测试。 相似文献
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J. G. Trotignon J. L. Michau D. Lagoutte M. Chabassière G. Chalumeau F. Colin P. M. E. Décréau J. Geiswiller P. Gille R. Grard T. Hachemi M. Hamelin A. Eriksson H. Laakso J. P. Lebreton C. Mazelle O. Randriamboarison W. Schmidt A. Smit U. Telljohann P. Zamora 《Space Science Reviews》2007,128(1-4):713-728
The main objective of the Mutual Impedance Probe (MIP), part of the Rosetta Plasma Consortium (RPC), is to measure the electron
density and temperature of Comet 67P/Churyumov-Gerasimenko’s coma, in particular inside the contact surface. Furthermore,
MIP will determine the bulk velocity of the ionised outflowing atmosphere, define the spectral distribution of natural plasma
waves, and monitor dust and gas activities around the nucleus. The MIP instrumentation consists of an electronics board for
signal processing in the 7 kHz to 3.5 MHz range and a sensor unit of two receiving and two transmitting electrodes mounted
on a 1-m long bar. In addition, the Langmuir probe of the RPC/LAP instrument that is at about 4 m from the MIP sensor can
be used as a transmitter (in place of the MIP ones) and MIP as a receiver in order to have access to the density and temperature
of plasmas at higher Debye lengths than those for which the MIP is originally designed. 相似文献
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理解发展新社会阶层中的优秀分子入党这一问题,对大学生来讲有两方面的难点:一是如何理解拥有大量财产的人入党的问题;二是如何理解存在剥削行为的人入党的问题。笔从这两方面入手,进行必要的探讨和研究。 相似文献
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疲劳寿命受到材料内部缺陷的制约,可以通过电位法试验获得微缺口试样的疲劳裂纹扩展规律,进而分析缺陷对材料疲劳寿命的影响。在试验前,需要预先研究试验的主要影响因素。利用COMSOL有限元软件,研究了电流输入点位置和电势差测点位置对试验精度和试验复现性的影响,计算得到不同裂纹前缘形状对应的电位法校核曲线。结果表明:(1)电流输入点位置位于试样平行于裂纹面的上下表面时,可以保证试验的复现性。(2)当测点位于裂纹面的垂直对称面上,且测点距离裂纹面垂直距离为0.06~0.1倍试样宽度时,可以同时满足测试精度和复现性。(3)当裂纹宽度和裂纹深度的比值3时,可以不考虑裂纹前缘形状对校核曲线的影响,当裂纹宽度和裂纹深度的比值≤3时,裂纹前缘形状对校核曲线的影响较大。 相似文献
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G.E. Dorrington 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Various balloon systems intended as scientific platforms to float in the atmosphere of Venus at altitudes between about 35 and 65 km are briefly reviewed. Previous predictions of the altitude oscillations of balloons filled with helium gas and water vapor are largely confirmed through numerical simulation and analysis. The need for refined thermal modelling is emphasised. Several novel technical concepts are introduced. It is concluded that phase change balloons would be more suitable than non-condensing super pressure gas balloons when repeated altitude excursions are a mission requirement. 相似文献
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