发动机排气温度和烟度明显降低，排放指标也在一定程度上得到了改善。
When using emulsified fuels the engine emissions are improved to a certain extent.
从泛函分析的角度出发，将航空发动机排气温度预测问题转换为一种泛函逼近问题。
From the perspective of functional analysis, the prediction of the aeroengine exhaust gas temperature could be seen as a functional approximation problem in nature.
对某型航空发动机排气温度测温原理进行了研究，为该型航空发动机排气温度的监测提供了理论依据。
The paper analyzes the temperature measuring principle of exhaust temperature of a certain type of engine and provides a theoretical basis for monitoring the exhaust temperature of the engine.
由于航空发动机转速高，空气流量大，排气温度高，试车时产生的强烈噪声形成大范围的环境污染；
Aerogine has the features of high rev, heavy air flux and high exhaust temperature, fierceness of noise engenders environment pollution largely during aeroengine test.
从实验结果可知，发动机的缸体的余热量、废气流量和排气温度随着转速和扭矩的增加而增加。
From the experimental results, we can see that the remainder of the engine block heat, air flow and exhaust temperature with the speed and torque increased.
考虑发动机工作过程的多个延迟环节，将算法扩展应用于动态过程的排气温度估计，并得到了基于循环的离散表达式。
Taking into account several delaying links in the engine working process, the algorithm is further extended for being used in transient states of engine in discrete form.
并说明了用此传感器来测量“发动机A 3引气口温度”和“TPU排气温度”的原理及校准方法。
The principles and calibration method by using this sensor to measure "engine outlet A3 temperature" and "TPU exhaust temperature" are also presented.
并说明了用此传感器来测量“发动机A 3引气口温度”和“TPU排气温度”的原理及校准方法。
The principles and calibration method by using this sensor to measure "engine outlet A3 temperature" and "TPU exhaust temperature" are also presented.
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