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1)  turbine diffuser
涡轮扩压段
2)  turbocharging
涡轮增压
1.
Present State and Future Development of Research on Diesel Engine Turbocharging Systems;
柴油机涡轮增压系统研究现状与进展
2.
Research in IC Engine Flowthermodynamics and Turbocharging Technology;
内燃机流动热力学与涡轮增压技术研究
3.
In this paper a new-developed 1+2 MIXPC turbocharging system and its exhaust manifold are introduced.
介绍了最新开发的1+2 MIXPC涡轮增压系统及其排气管系的结构。
3)  low-pressure turbine
低压涡轮
1.
Numerical study of active flow control using jet-flap for a low-pressure turbine cascade;
射流襟翼-低压涡轮叶栅主动流动控制数值研究
2.
Numerically investigate the effects of freestream turbulence on dynamics of a low-pressure turbine stage;
自由流湍流度对某低压涡轮级气动影响的数值研究
3.
Aerodynamic performance of a highly-loaded low-pressure turbine profile
一种大负荷低压涡轮叶型的气动性能
4)  low pressure turbine
低压涡轮
1.
This paper reviews the research progress on complex internal flow in low Reynolds number and low pressure turbine (LPT)in recent years.
结合近年来国内外相关领域的研究工作,对低雷诺数低压涡轮内部复杂流动机理的研究进展进行了介绍,包括低雷诺数情况下低压涡轮内部非定常流动的特点,叶片边界层分离及转捩现象机理,上游周期性尾迹与下游叶片边界层相互作用机理等。
2.
This paper concerning under low Reynolds number condition the low efficiency of low pressure turbines (LPT) presents how to consider the effect of Reynolds number in design cycle, and a reasonable loading distribution form is given with one practical design example.
本文针对低雷诺数条件下低压涡轮效率较低的问题,提出了设计过程中应如何考虑雷诺数影响的思路,给出了适应低雷诺数环境下工作的叶片表面负荷分布形式,并进行了低压涡轮的气动设计。
3.
As a very important component of aeroengines, low pressure turbine affects the mass, the specific fuel consumption, the efficiency of aeroengine greatly.
作为航空发动机非常重要的组成部分,低压涡轮对整个发动机质量、耗油率和效率都有很大的影响。
5)  turbocharge [英]['tə:bəu,tʃɑ:dʒ]  [美]['tɝbo,tʃɑrdʒ]
涡轮增压
1.
Reliability Evaluation of Turbocharged Diesel Engine System Using Fuzzy Sets and Evidential Reasoning;
基于模糊推理方法的涡轮增压柴油机系统可靠性评估
2.
Modeling of a Turbocharged Diesel Engine with Electronic Control System;
采用电子控制系统的涡轮增压柴油机的模拟研究
3.
This paper analysed the turbocharged high speed diesel engine perhrmance athighland,reported the calculation of prediction of turbocharged high speed diesel engineperformance at highland.
本文对于柴油机高原效率进行了详细的分析,并推导了关于涡轮增压柴油机高原性能预测的计算公式。
6)  High pressure turbine
高压涡轮
1.
Based on a 3D N-S code, a cooling air injection model was introduced to simulate the flow field in a high pressure turbine which has the cooling air mixing.
本文在三维N-S程序的基础上,引入一种较为简单的冷气射流计算模型,对一级高压涡轮含有冷气掺混的三维流场进行了数值分析,揭示了冷气掺混对导叶流量特性及损失分布的影响,并通过涡轮叶片排二次流动结构的分析初步探讨了冷气掺混损失机理。
2.
The secondary flow loss plays a main part in the total loss of high pressure turbine\'s(HPT).
叶顶间隙二次流在高压涡轮总损失中占据了较大比重。
补充资料:十报恩 赠段先生 折段字起
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