导流叶片的英文

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"导流叶片"怎么读用"导流叶片"造句

英文翻译手机版

breather vane
corner-vane
countervane
guide baffle
guide rib
suction vane

"叶片"英文翻译 blade vane; blade; paddle; l ...
"导流叶片齿轮" 英文翻译 : suction vane gear
"反转导流叶片" 英文翻译 : contra vane
"风扇导流叶片" 英文翻译 : stator vane
"刚性导流叶片" 英文翻译 : rigid guide vane
"固定导流叶片" 英文翻译 : fixed guide vane
"进口导流叶片" 英文翻译 : inlet guide blade
"进气导流叶片" 英文翻译 : inlet guide vane
"逆向导流叶片" 英文翻译 : contra-vane
"排气导流叶片" 英文翻译 : exhaust stator blade
"入口导流叶片" 英文翻译 : inlet guide vance; inlet guide vane
"转动导流叶片" 英文翻译 : rotating guide vane
"可转动的导流叶片" 英文翻译 : rotating guide vane
"通气口导流叶片" 英文翻译 : breather vane
"导流叶" 英文翻译 : contra vane
"导流叶片通气控制阀" 英文翻译 : breather vane
"空气进口导流叶片装置" 英文翻译 : air inlet guide vane assembly
"导流叶轮" 英文翻译 : guide vane assembly; impeller inducer; inducer
"前导流叶" 英文翻译 : pre-turning vane
"前导流叶器" 英文翻译 : front inertia
"分流叶片" 英文翻译 : divided flow blade; split blade; splitter blade; splitter vanes
"双流叶片泵" 英文翻译 : zweiflutige flügelzellen-pumpe dual flow vane pump
"旋流叶片" 英文翻译 : intervane; swirl vane; swirler vane
"整流叶片" 英文翻译 : straightened blade; straightener blade; straightening vanes
"轴流叶片" 英文翻译 : axial flow blading

例句与用法

Straightening vanes can be used where long straight ways are not possible .
在不可能安装较长的直管段情况下，可以来用导流叶片。
Air inlet guide vane assembly
空气进口导流叶片装置
Consider a row of guide vanes in a compressible internal flow as shown below
如下图所示，考虑可压缩内部流中的一排导流叶片。
Results show that restaggering ogv is more effective to reduce disturbance in integrated pylon case but with less effective in separated pylon case
分离式吊架情况下，对减小扰动的作用不明显；一体化式吊架情况下，通过适当调整出口导流叶片安装角可以有效地降低转子后的压力扰动，改善流场。
Unsteady numerical simulations and experiments were carried out to investigate the method of restaggering ogv to shield influence of pylons on a low - speed compressor , including separated pylon and separated pylon cases
摘要针对调整出口导流叶片来减小吊架对压气机流场影响的方法，采用非定常数值模拟和实验方法，对分离式和一体化式吊架进行了研究。
The dynamo runs at rull speed to drive main shaft , then the main shaft makes the emulsifying wings in emulsification grove rotate , which absorbs the liquid in its brand groove into ring groove through guide vanes on upper and lower sides of the groove . the vanes spins circularly at high speed with the main shatf as center , and the blade and emulsificaton groove cut and crush it continuously . after that . it gers squeezed by the vanes highspeed centrifugal rotation . at last , it finishes isotropt emulsification tratment within extremely short time after continuous circulating mixing
由电动机全速运转带动主轴，经主轴转动乳化框槽内之乳化翼片，使其将桶槽内之液体经框槽上、下两侧之导流叶片吸入环状框槽内，经以主轴为中心高速圆周旋转叶片；连续使乳化翼端刀面与乳化框间极小之间系高频率之强力切割剪断、粉碎，再借叶片高速离心旋转排挤，持续循环混合，以极短之时间即可完成均质乳化之处理。
To meet the needs for wider surge margin of the turbofan engine , a new model was developed to predict the characteristics of the fan / high pressure compressor and turbine in this thesis . several ways , including , variable inlet guide vanes of the fan , variable guide vanes of the high pressure compressor , the variable inlet area ratio of the mixer and the nozzle areas , were presented to enlarge the surge margin of the turbofan engine . meanwhile , a method of combined variable geometries for optimizing controls of inlet guide vanes of the fan , guide vanes and the first two stators of high pressure compressor , area ratio of mixer and noz zle areas was established
为了满足下一代作战飞机对推进系统的性能和稳定性要求，本文建立了压缩系统特性和涡轮特性的新模型，并分别采用改变涡扇发动机风扇进口导流叶片、压气机导流叶片和前两级静叶片、混合室进口处内、外涵面积比和尾喷管面积，研究了其对发动机性能和稳定性的影响，进而得出了涡扇发动机变几何扩稳的方法，为发动机变几何扩稳研究打下理论基础。
By using harika algorithm , the characteristic of a high - pressure compressor is calculated at different installation angle of the inlet guide vane and the stator vanes ; the characteristics of a high - pressure turbine and a low - pressure turbine are simulated at different installation angles of the guide vane based on ainley method
本文用harika算法计算了导流叶片和静子叶片安装角度可调的变几何高压压气机特性；用ainley法计算了涡轮导向器面积可调的高压涡轮和低压涡轮的特性。