高压涡轮的英文

• high pressure turbine (hpt)
• high-pressure turbine

• "高压"英文翻译    high-handed
• "涡轮"英文翻译    turbine; worm wheel
• "高压涡轮机" 英文翻译 :    high pressure turbine; highpressureturbine; pre ure turbine; pressure turbine
• "高压涡轮增压器" 英文翻译 :    high pre ure turbocharger; high pressure turbocharger
• "背压涡轮机" 英文翻译 :    back pressure turbine
• "低压涡轮" 英文翻译 :    low pressure turbine; low-pressure turbine
• "低压涡轮机" 英文翻译 :    low pressure turbine; low-pressure turbine
• "低压涡轮级" 英文翻译 :    low-pressure turbine stage
• "多压涡轮机" 英文翻译 :    multi-pressure turbine
• "复压涡轮机" 英文翻译 :    pressure compounded turbine
• "混压涡轮机" 英文翻译 :    mixed pre ure turbine; mixed pressure turbine
• "增压涡轮" 英文翻译 :    charging turbine
• "中压涡轮" 英文翻译 :    intermediate-pressure turbine
• "中压涡轮机" 英文翻译 :    intermediate pressure turbine
• "高压涡汽轮" 英文翻译 :    high pre ure turbine; high pressure turbine
• "定压涡轮增压" 英文翻译 :    constant pressure turbo-charging
• "高背压涡轮机" 英文翻译 :    high back pre ure turbine; high back pressure turbine
• "增压涡轮机组" 英文翻译 :    charging turbine set; charging-turbine set
• "低压涡轮增压器" 英文翻译 :    low pre ure turbocharger; low pressure turbocharger
• "涡轮高压级" 英文翻译 :    high-pressure turbine stage
• "冲压涡轮泵收放手柄" 英文翻译 :    ram-air turbine control handle
• "增压涡轮螺旋浆发动机" 英文翻译 :    supercharged turboprop
• "增压涡轮螺旋桨发动机" 英文翻译 :    supercharged turbo-propeller engine
• "反动式涡轮机, 压力涡轮机, 不等压涡轮机" 英文翻译 :    reaction turbine
• "高压蒸汽涡轮" 英文翻译 :    high pressure steam turbine; high-pressure steam turbine

• The main work of this paper is the heat transfer experiment in rotating cavity of an advanced aero - engine of rrd company
  本文工作围绕rrd公司某型先进发动机高压涡轮盘腔内换热实验进行。
• And those characteristics of compressor and turbine are put into the steady - state design and off - design performance program of augmented turbofan engine , to calculate the influence of the geometry changing of single component on the performance of engine
  计算了单个可变几何部件的调节(包括高压压气机、高压涡轮、低压涡轮、混合器进口面积比和喷管喉道面积)对发动机稳态性能的影响。
• Based on an engineering background , through numerical simulation of the flow field in the hp turbine of the energy efficient engine ( e3 ) , the article research the unsteady flow in a transonic turbine stage , the unsteady phenomena in the stage include the shockwave , wake , shedding vortex , endwall vortex , passage vortex and leakage vortex , etc . there are two shockwaves generated on the vane the tailing edge , one on suction side is named moving shockwave , and name another on pressure side steady shockwave
  本文首先对于研究的意义和国内外研究的现状做了简要的介绍，再从某工程背景出发，通过对e3发动机高压涡轮内流场的数值模拟，研究了干涉的周期性的问题，以及涡轮级内常见的非定常现象：激波、尾迹、脱落涡、根脚涡、通道涡、漏流涡。导向器尾缘会出现两道激波，在吸力面的激波可称为“运动”激波，压力面的激波可称为“定常”激波。
• The result of the calculation for tip clearance is reasonable when it is compared with theory . two ways are put forward for convention of dimension of the turbine components from high temperature to low one , which is related with tip clearance , a simple example is used to illuminate that the two ways are useful , using the method of design optimization , axiisk and a blade of a certain turhine is analysed , it showes that the method of design optimization is feasible to be used for convertion of dimension of the turbine components . finally , ansys software is used to analyzed the variation of tip clearance with the method of cyclic symmetry analysis when engine works under the conditions of temperature and rotational speed , am using a new method to deal with thermal contact resistance in the calculation
  本文完善了计算涡轮叶尖间隙的简化算法程序，增加了程序的计算功能，并将其应用于某高压涡轮进行叶尖间隙分析，所得结果与理论结果进行了对比，得出修改后的程序用于叶尖间隙计算是合理的；同时提出了与叶尖间隙相关的涡轮典型部件的冷、热态的尺寸两种换算方法，使用优化设计的方法进行了实例分析，说明了所提出的计算方法是可行的；最后应用ansys有限元软件利用循环对称的方法分析了某型发动机高压涡轮在温度场及离心力作用下的叶尖间隙在发动机工作过程中变化情况，并分析了计算中的接触热阻的处理问题。
• 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。
• 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。