低压涡轮的英文

• low pressure turbine
• low-pressure turbine

• "低压"英文翻译    low pressure; slight pressur ...
• "涡轮"英文翻译    turbine; worm wheel
• "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
• "低压涡轮增压器" 英文翻译 :    low pre ure turbocharger; low pressure turbocharger
• "背压涡轮机" 英文翻译 :    back pressure turbine
• "多压涡轮机" 英文翻译 :    multi-pressure turbine
• "复压涡轮机" 英文翻译 :    pressure compounded turbine
• "高压涡轮" 英文翻译 :    high pressure turbine (hpt); high-pressure turbine
• "高压涡轮机" 英文翻译 :    high pressure turbine; highpressureturbine; pre ure turbine; pressure 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
• "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
• "高压涡轮增压器" 英文翻译 :    high pre ure turbocharger; high pressure turbocharger
• "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
• "低压气动涡轮启动机" 英文翻译 :    low-pressure pneumatic turbine starter
• "低压" 英文翻译 :    1.[物理学] (较低的压力) low pressure; slight pressure2.[气象学] (低气压区) low pressure; depression3.[电学] (较低电压) low tension; low voltage (通常指250伏以下)4.[医学] (心脏舒张时血液对血管的压力) minimum pressure
• "等压涡度" 英文翻译 :    isobaric vorticity

• Machinning and assembling of low pressure turbo rotor
  低压涡轮转子的加工与装配
• The long - term life and low cycle fatigue life of low pressure turbine blade for an aeroengine under real loading spectrum is analyzed by using this method
  用该方法对某型发动机低压涡轮工作叶片在实际飞行载荷谱作用下的持久寿命和低循环疲劳寿命进行了分析。
• 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。
• 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。
• These variable geometry components include high pressure - compressor , high - pressure turbine , low - pressure turbine , inlet area ratio of mixer and main nozzle throat area . the results of calculation show that the adjusting of low - pressure turbine and mixer has a remarkable effect on the performance of engine and bypass ratio
  计算结果表明，低压涡轮和混合器的调节对发动机的性能和涵道比的影响尤为显著；在其它部件几何结构不同时，单个部件几何调节后，发动机性能的变化趋势是不同的。
• 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。