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   充气容器 的翻译结果: 查询用时:0.143秒
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充气容器
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  “充气容器”译为未确定词的双语例句
     It is proved that the method is accurate and reliable by some cold flow tests and ground static tests,overcoming the data dispersity.
     该测量方法经过多次充气容器冷试和发动机地面静止试验的考核,证实了测出的数据准确可靠,克服了时间测量数据分散度大的缺点。
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     Dynamic Model of a Flow Stabilizator with Stable Gas Pressure
     充气稳压容器的动态数学模型
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     Experimental Investigation of High Velocity Impacts on Gas Filled Pressure Vessels
     充气压力容器高速撞击实验研究
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     The Opulent Container
     奢华的容器
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     BLAST CHAMBER
     爆炸容器
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     ^^Pneumatic overflow valve.
     充气溢流闸门
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The formula for pressure variation by admitting compressed air into a chamber in most literatures are deduced with an assumption of equi-entropy. But this assumption is not correct. A formula based on equi enthalpy is worked out in this paper and checked with experimental results. The conclusion is: The pressure variation calculated with equi-entropy does not fit to experimental results, while that with equi-enthalpy fits well.

本文以等焓为基础,导出了一个气室充气公式,并用实测结果分别校核,得到的结论是:用等熵公式计算所得气压变化与实测曲线吻合得不好,而等焓公式能较好地反映充气容器中气体变化的规律。

Measuring method of opening time and operating synchronism of the reverse nozzle closures of solid rocket motor during thrust termination test was studied.The high anti interference digital recording system,which has μs magnitude time resolution,and multi function analog recording system was used.The method solves the key technique of generation and measurement of the initial pulses and termination pulses,and eliminates,the effects of the explosion wave...

Measuring method of opening time and operating synchronism of the reverse nozzle closures of solid rocket motor during thrust termination test was studied.The high anti interference digital recording system,which has μs magnitude time resolution,and multi function analog recording system was used.The method solves the key technique of generation and measurement of the initial pulses and termination pulses,and eliminates,the effects of the explosion wave and gas ionization from detonation system.It is proved that the method is accurate and reliable by some cold flow tests and ground static tests,overcoming the data dispersity.

研究了固体火箭发动机推力终止试验时,反向喷管堵盖打开时间及同步性测量方法。在测量中配置了抗干扰能力强、时间分辨率为微秒级的数字记录系统和多功能模拟记录系统,解决了时间测量中产生和获取起始脉冲及终止脉冲信号的关键技术,消除了引爆机构产生的冲击波和气体电离的影响。该测量方法经过多次充气容器冷试和发动机地面静止试验的考核,证实了测出的数据准确可靠,克服了时间测量数据分散度大的缺点。

 
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