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Combustion Optimization in an Unmanned Aerial Vehicle Diesel Engine

机译:无人机柴油机燃烧优化

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This study utilizes Design of Experiments methodology to optimize the performance of a multi-cylinder aviation diesel engine. Through a rigorous approach, design variables and response parameters were selected, and their ranges defined. Based on the specified variable ranges, a software tool was used to generate a test matrix of the minimum-size required to define the relationships between variables. Experimental work was conducted to acquire real engine data for all points in the test matrix, and used to build a Stochastic Process Model of engine performance. The empirical model was used to predict the optimal values for the design variables that would produce the most power from the engine. These conditions were then experimentally validated. Through this approach it was found that engine power at sea level could be increased by as much as 12% compared to the reference calibration, while still maintaining safe operating conditions in terms of exhaust gas temperature and in-cylinder peak pressure. This approach using Design of Experiments was found to dramatically reduce the amount of experimental work required to quantify the full capability of the engine.
机译:这项研究利用“实验设计”方法论来优化多缸航空柴油发动机的性能。通过严格的方法,选择了设计变量和响应参数,并定义了它们的范围。根据指定的变量范围,使用软件工具生成定义变量之间关系所需的最小大小的测试矩阵。进行了实验工作,以获取测试矩阵中所有点的真实发动机数据,并用于建立发动机性能的随机过程模型。该经验模型用于预测将产生最大功率的设计变量的最佳值。然后通过实验验证了这些条件。通过这种方法,发现与基准校准相比,海平面上的发动机功率可以提高多达12%,同时仍在废气温度和缸内峰值压力方面保持安全的运行条件。发现这种使用“实验设计”的方法可以显着减少量化发动机的全部功能所需的实验工作量。

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