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DEVELOPMENT AND INTEGRATION OF RAIN INGESTION EFFECTS IN ENGINE PERFORMANCE SIMULATIONS

机译:发动机性能模拟中雨水吸收作用的发展与整合

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Rain ingestion can significantly affect the performance and operability of gas turbine aero-engines. In order to study and understand rain ingestion phenomena at engine level, a performance model is required that integrates component models capable of simulating the physics of rain ingestion. The current work provides, for the first time in the open literature, information about the set-up of a mixed-fidelity engine model suitable for rain ingestion simulation and corresponding overall engine performance results. Such a model can initially support an analysis of rain ingestion during the pre-design phase of engine development. Once components and engine models are validated and calibrated versus experimental data, they can then be used to support certification tests, the extrapolation of ground test results to altitude conditions, the evaluation of control or engine hardware improvements and eventually the investigation of inflight events. In the present paper, component models of various levels of fidelity are firstly described. These models account for the scoop effect at engine inlet, the fan effect and the effects of water presence in the operation and performance of the compressors and the combustor. Phenomena such as velocity slip between the liquid and gaseous phases, droplet break-up, droplet-surface interaction, droplet and film evaporation as well as compressor stages re-matching due to evaporation are included in the calculations. Water ingestion influences the operation of the components and their matching, so in order to simulate rain ingestion at engine level a suitable multi-fidelity engine model has been developed in the PROOSIS simulation platform. The engine model's architecture is discussed and a generic high bypass turbofan is selected as a demonstration test case engine. The analysis of rain ingestion effects on engine performance and operability is performed for the worst case scenario, with respect to the water quantity entering the engine. The results indicate that rain ingestion has a strong negative effect on high-pressure compressor surge margin, fuel consumption and combustor efficiency, while more than half of the water entering the core is expected to remain unevaporated and reach the combustor in the form of film.
机译:摄入雨水会严重影响燃气轮机航空发动机的性能和可操作性。为了研究和理解发动机级的雨水吸收现象,需要一个性能模型,该模型集成了能够模拟雨水吸收物理特性的组件模型。当前的工作首次在公开文献中提供了有关适用于雨水摄入模拟的混合保真度发动机模型的建立以及相应的整体发动机性能结果的信息。这样的模型最初可以在发动机开发的预设计阶段支持对雨水摄入量的分析。一旦验证了组件和发动机模型并相对于实验数据进行了校准,它们就可以用于支持认证测试,将地面测试结果外推到海拔条件,评估控制或发动机硬件的改进以及最终对飞行事件进行调查。在本文中,首先描述了各种保真度的组件模型。这些模型考虑了在发动机入口处的铲斗效应,风扇效应以及水的存在对压缩机和燃烧室的运行和性能的影响。计算中包括诸如液相和气相之间的速度滑移,液滴破裂,液滴-表面相互作用,液滴和薄膜蒸发以及由于蒸发而导致的压缩机级重新匹配等现象。进水会影响组件的运行及其匹配,因此,为了在发动机级别模拟雨水的摄入,已经在PROOSIS仿真平台中开发了合适​​的多保真发动机模型。讨论了引擎模型的体系结构,并选择了通用的高旁通涡轮风扇作为演示测试用例引擎。对于进入发动机的水量,在最坏的情况下分析了雨水摄入对发动机性能和可操作性的影响。结果表明,雨水的摄入对高压压缩机的喘振裕度,燃料消耗和燃烧器效率具有强烈的负面影响,而进入堆芯的水中有一半以上有望保持不蒸发并以薄膜形式到达燃烧器。

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