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Modeling of Start-Up From Engine-Off Conditions Using High Fidelity Turbofan Engine Simulations

机译:使用高保真涡扇发动机仿真在发动机熄火条件下进行启动建模

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Engine models are widely used to simulate the engine behavior at steady state and transient operating conditions over the full flight envelope. Within the engine development process such simulations are used to support component design, evaluate engine performance, operability and test data, as well as to develop and optimize the engine controls. Recent developments have raised interest in the modeling of start-up processes of turbofan engines in order to support the definition of sufficient engine control laws. This implies that simulations are started at a condition where the engine shafts are static and temperatures and pressures are equal to ambient. During start-up the engine can only be operated transiently through the sub-sub-idle region (near zero speed) using a starter torque. The activity presented here was targeted to support the development of industrial-standard high-fidelity turbofan engine models capable of simulating start-up, shutdown or windmilling operation. Within the three previously mentioned cases starting from an engine-off condition, ground start from zero-speed is the most challenging in terms of physical and numerical modeling. For this reason, this paper concentrates on that case only. Zero mass flow and speed at the beginning of the simulation impose a set of special problems that do not exist in standard simulations: the modeling of a static engine-off condition, the modeling of static friction, and the modeling of reverse flows. The requirement to support an existing industrial model development process also made it necessary to apply the same quality of physical modeling to start-up simulations as would be the case for above-idle engine simulations. The physical effects present during engine start are discussed and modeling solutions are presented. Finally, results of a dry crank simulation are presented and discussed, illustrating that the expected effects are present and that the simulation is capable of predicting the correct trends.
机译:发动机模型被广泛用于在整个飞行范围内模拟稳态和瞬态工况下的发动机性能。在发动机开发过程中,此类模拟用于支持组件设计,评估发动机性能,可操作性和测试数据,以及开发和优化发动机控制。为了支持定义足够的发动机控制定律,最近的发展引起了对涡轮风扇发动机的启动过程的建模的兴趣。这意味着在发动机轴静止且温度和压力等于环境的条件下开始模拟。在起动过程中,发动机只能使用起动转矩在子空转区域(零速附近)短暂运行。此处介绍的活动旨在支持能够模拟启动,关闭或风车运行的工业标准高保真涡扇发动机模型的开发。在前面提到的三种情况下,从发动机关闭状态开始,从零速开始地面行驶在物理和数值建模方面是最具挑战性的。由于这个原因,本文只关注这种情况。在模拟开始时,零质量流量和速度会带来一系列特殊问题,这些问题在标准模拟中不存在:静态发动机关闭条件的建模,静态摩擦的建模以及反向流动的建模。支持现有工业模型开发过程的要求也使得有必要将与初始发动机仿真相同的物理模型质量应用于启动仿真。讨论了发动机启动过程中出现的物理影响并提供了建模解决方案。最后,提出并讨论了干曲柄模拟的结果,说明了存在预期的效果并且该模拟能够预测正确的趋势。

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