在一台单缸135柴油机上对柴油机TR燃烧系统的性能进行了试验优化。
Optimization experiment of diesel TR combustion system was made on a single cylinder 135 diesel.
通过优化试验，使燃烧工况得到基本改善。
The combustion situation is improved basically by means of optimization test.
最后，对锅炉燃烧控制系统进行了试验，对实际运行曲线和数据进行了分析，结果表明，本论文的控制方法与优化方案是可行的和有效的。
In the end, the optimum combustion control plan and system have been tested in the site, and the operation parameter curves and tested data of burning control system are analyzed.
并且通过试验的方法，着重探讨了通过调整过量空气系数来使锅炉燃烧达到优化的低氧燃烧技术。
And by means of testing, the thesis puts emphasis upon the study of the low-oxygen combustion technique, which can optimize boiler's combustion by adjust the excess air factor.
采用遗传算法对某试验超燃冲压模型发动机的燃烧室构型参数进行了优化设计，所得方案的性能大大优于实际方案。
Scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.
结构优化后的燃烧装置进行了实验室试验运行，验证了燃烧装置具有非常好的升温控制能力和温度与能量的平衡能力。
The burning equipment was tested in the laboratory, proving that it had good temperature-rising control ability and temperature and energy balance ability.
用这种方法对S195非直喷式柴油机燃烧系统进行了正交模拟计算，并用该样机的正交试验优化结果对正交模拟优化结果进行了验证和对比。
The method was called the orthogonal simulated calculation method. The orthogonal simulated calculation was used to the combustion system of S195 swirl chamber diesel engine.
用这种方法对S195非直喷式柴油机燃烧系统进行了正交模拟计算，并用该样机的正交试验优化结果对正交模拟优化结果进行了验证和对比。
The method was called the orthogonal simulated calculation method. The orthogonal simulated calculation was used to the combustion system of S195 swirl chamber diesel engine.
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