涡轮部件的英文

• turbine bulk

• "涡轮"英文翻译    turbine; worm wheel
• "部件"英文翻译    component; unit; parts; asse ...
• "齿轮部件" 英文翻译 :    geared parts
• "三轮部" 英文翻译 :    miwabe
• "齿轮部分" 英文翻译 :    gear parts
• "大三轮部" 英文翻译 :    omiwabe
• "部件" 英文翻译 :    component; unit; parts; assembly; subsystem; secundina (pl. secundinae)
• "涡轮" 英文翻译 :    [机械工程] turbine; worm wheel◇涡轮泵 [航空] turbopump; roturbo; 涡轮发动机 turbine engine; 涡轮风扇发动机 fanjet; 涡轮机 turbomachine; turbomachinery; 涡轮螺(旋)桨发动机 turbo-propeller engine; turbo-prop[drive]; 涡轮螺桨式客机 turbo-liner
• "凸轮的凸轮部分" 英文翻译 :    beak of cam
• "泵部件" 英文翻译 :    pumparts
• "部件,零件" 英文翻译 :    parts
• "部件，成员" 英文翻译 :    member
• "部件，组件" 英文翻译 :    pack unit
• "部件的" 英文翻译 :    partial
• "部件号" 英文翻译 :    part number; parts number
• "部件架" 英文翻译 :    rack for assembly unit
• "部件名" 英文翻译 :    comname; name of parts
• "部件族" 英文翻译 :    component family; part family
• "尺寸(部件)" 英文翻译 :    dimension
• "串部件" 英文翻译 :    string unit
• "多部件" 英文翻译 :    multicomponent; multi-unit◇多部件机器 multi-unit machine; 多部件计算机 multiunit computer
• "分部件" 英文翻译 :    sub-unit
• "分量,部件" 英文翻译 :    component
• "核部件" 英文翻译 :    nuclear component
• "空部件" 英文翻译 :    null part

• The numerical simulation of the design condition and test condition in wp6 turbine
  6涡轮部件设计状态及实验状态的数值模拟
• The parametric method is used in the process of turbine parts modeling and tip clearance analysis . due to the complexity of the turbine parts , some characters are predigested
  本文引入了近年来迅速发展的参数化设计思想,应用于涡轮部件的建模和叶尖间隙的分析。
• To investigate the aerodynamic design ideas and concrete methods of high performance low pressure turbine ( lpt ) at low reynolds number condition , a new lpt of high load , large chord and proper velocity distribution was designed
  摘要为了探索高空低雷诺数情况下高性能低压涡轮部件的气动设计思路和设计方法，通过采用高负荷、大弦长的叶片设计和选择恰当的叶片表面速度分布形式设计了一台新低压涡轮。
• In this paper , the status quo of the tip clearance of aero - engine is surveyed , the theory and the method of the numerical computation of tip clearance are introduced , the simple tip clearance calculation program is modified and refined and the computation method of the turbine temperature field is improved
  本文阐述了国内外航空发动机叶尖间隙的研究现状,介绍了涡轮叶尖间隙计算的理论和方法。对涡轮叶尖间隙准二维计算程序作了修改和完善,改进涡轮部件温度场的计算方法,增加了变量显示/修改、程序控制和结果显示界面,使软件更加直观,实用。
• A simplify high pressure turbine ( hpt ) tip clearance model is analyzed with the cyclic symmetry method . research on the flow , heat and structure integration analyses is achieved in this paper . flow / heat analysis is done by fluent software , and heat / structure analysis is done by ansys software
  针对涡轮部件的结构特点,进行了适当的简化,利用参数化设计思想建立了涡轮叶尖间隙计算模型,用循环对称的方法分析了某型发动机高压涡轮叶尖间隙在工作过程中变化的情况。