静叶片的英文

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"静叶片"怎么读用"静叶片"造句

英文翻译手机版

fixed-blade
stationary blades/ blading
stationary vane
stator blade

"静"英文翻译 still; calm; motionless
"叶片"英文翻译 blade vane; blade; paddle; l ...
"可转静叶片" 英文翻译 : variable stator vane
"静叶" 英文翻译 : stationary guide blade
"可调静叶片操纵杆系" 英文翻译 : variable stator linkage
"静叶点" 英文翻译 : rest point
"静叶环" 英文翻译 : fixed blade ring
"静叶列" 英文翻译 : stationary blade row
"变距静叶" 英文翻译 : variable stator vane
"环形静叶栅" 英文翻译 : annual static cascade
"静叶持环" 英文翻译 : stationary blade carrier
"静叶根槽" 英文翻译 : stationary blade groove
"静叶环套" 英文翻译 : stator blade carrier ring
"静叶栅损失" 英文翻译 : stator cascade loss
"可转静叶" 英文翻译 : variable stator blade
"叶片" 英文翻译 : 1.[植物学] (leaf) blade2.[机械工程] vane; blade; paddle; limb 涡轮叶片 turbine blade
"静叶持环、静叶的测量与调整" 英文翻译 : measurement and adjustment of static carrier ring and static blade
"百叶片" 英文翻译 : louver; louvre blade
"背叶片" 英文翻译 : back vane
"泵叶片" 英文翻译 : pumblade
"长叶片" 英文翻译 : a linear leaf; long blade
"导叶片" 英文翻译 : guide blade; guide vane
"动叶片" 英文翻译 : bucket; feathering blade; moving blades/ blading; moving vane; rotor blades
"短叶片" 英文翻译 : short blade
"多叶片" 英文翻译 : multiple-blade

例句与用法

In order to eliminate the brittle fracture of the stator blade , using the orthogonal experiment , the brittle problem of the stator blade was studied
为了消除静叶片的脆性断裂，采用正交试验对脆性问题进行了研究。
The steam path of the steam turbine through which steam flows consists of nozzles , and the moving blade , fixed blade and other auxiliary equipment
汽轮机的通流部分即蒸汽流过并做功的部分，其中包括喷嘴，隔板以及动、静叶片以及相应的汽封装置。
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。