此外，还选取若干个控制参数，研究其对气动效率和气动功率的影响。
In addition, a number of control parameters are selected to study their impact on aerodynamic efficiency and pneumatic power.
比例、伺服液压技术，低功率气动控制阀，填料密封生产。
Ratio, servo hydraulic pressure technology, low power pneumatic control valve, production of stuffing.
得伟18伏整理钉枪-气动性能-功率的无绳方便。
DeWalt 18 Volt Finishing Nailer - Performance of pneumatic - convenience of cordless power.
给出了离心压缩机气动参数和结构参数与声功率级之间的内在关系。
The intrinsic relation between the pneumatic parameter, structural parameter and acoustic power level for centrifugal compressor is given.
用这种办法，气动执行机构地呈现极年夜地兴味，他们供给别的高功率输出关于低地外衣。
In this way, pneumatic actuators appear to be of great interest, They provide moreover high power output with regard to their low coat.
结合长叶片级S_2流面设计问题的计算结果对大功率汽轮机长叶片气动设计进行了初步的探讨。
Some discussion about aerodynamic design of last stage blade of large steam turbine has been given basing on the result of S_2 design calculation.
为了提高燃气涡轮起动机的功率，了解燃气涡轮设计点的气动参数以及内部流场结构。
It is important to understand aerodynamic parameters of design-point of gas turbine in order to improve the power of gas-starter.
扩散段、拐角以及风扇段的气动减阻在一定程度上减少了风机的功率。
Dropping the pressure loss of diffuser, corner, and fan section can help to reduce the power of the fan.
对不同的空气动声的声功率和效率作了相互比较。
The sound power and efficiencies of these different aerodynamic sound have been compared with each other.
本文详细讨论了现代大功率汽轮机排汽缸的流动特点对其气动性能的要求及对机组的各种影响。
The flow characters and the requirement for aerodynamic performance of modern large steam turbine exhaust hood, and their several effects on the steam turbine are discussed in detail.
气动肌肉是一种具有重量轻、功率—重量比高的新型气动柔性执行器。
Pneumatic muscle is a lightweight, flexible pneumatic actuator with high power weight ratio.
将适当功率的大扭矩特种电动机与气动风炮上的旋转式冲击装置相匹配而产生出的一种有着强冲击扭力的电动工具――电动风炮。
One great-torque motor with proper power is made to match with the rotary churn unit in pneumatic drill to form the electric pneumatic drill as one kind of powerful electrically driven tool.
气动特性实验表明在风洞气流速度比加油机最小飞行速度低16%的条件下，冲压涡轮输出功率即可满足加油需要。
It was found that the output power of ram air turbine can satisfy the flight refuel needs on conditions that the air speed of wind tunnel is 16% lower than the minimal flight speed of aircraft tanker.
气动特性实验表明在风洞气流速度比加油机最小飞行速度低16%的条件下，冲压涡轮输出功率即可满足加油需要。
It was found that the output power of ram air turbine can satisfy the flight refuel needs on conditions that the air speed of wind tunnel is 16% lower than the minimal flight speed of aircraft tanker.
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