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A Model to Study Circumferential Hot Gas Ingestion into Secondary Air Flow Path of an Engine

机译:一种模型,用于研究发动机二次空气流动路径的圆周热气体

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Of interest in this study is to model and predict the extent of local hot gas ingestion into secondary air system flow path. In real engines, asymmetry and resulting local hot gas ingestion may occur due to various reasons. Normally, asymmetry in geometric gaps and tolerances and variations in primary gas path pressure may result in some hot gas ingestion. But more importantly, deterioration and failure of critical sealing segment(s), and failure of cooling air supply pipes may result in severe hot gas ingestion. Hot gas ingestion would result in warmer turbine parts, limiting their life and performance significantly. Additionally, asymmetry in temperatures due to local hot gas ingestion may result in distorted bearing support structure leading to detrimental effects. In this study, a simple model is developed by using 1-D pressure, flow and enthalpy modules (Kutz and Speer, 1994) in a network enveloping the extent of an engine. The pseudo-3D modeling approach is applied to a real engine component to estimate the extent of damage due to local hot gas ingestion. Results demonstrate that the model provides a quick and powerful tool for estimating flow and heat transfer information in complex engine cavities with extremely low flow rates without resorting to complex and nearly impossible 3-D CFD simulations. In this study, failure of cooling air supply pipe during engine operation is simulated. The cooling air supply pipes bleed air from high pressure compressor (HPC) and feed air into inter transition duct of a development engine. Failure of supply pipe is simulated by venting one of the pipes to atmosphere. Results demonstrate severe asymmetry in flow and pressure in the secondary airflow path leading to large local hot gas ingestion. Further, large amount of local hot gas ingestion induces circumferential temperature gradients resulting in non-uniform heating and consequent distortions of static and rotating parts. Based on the knowledge of extent of damages, corrective arrangements are also discussed.
机译:本研究的兴趣是模拟和预测局部热气体摄取到二次空气系统流动路径的程度。在真正的发动机中,由于各种原因可能发生不对称性并产生局部热气体摄取。通常,几何间隙和公差的不对称性和初级气体路径压力的变化可能导致一些热气体摄取。但更重要的是,临界密封段的劣化和失效,以及冷却空气供应管的失效可能导致严重的热气体摄取。热气体摄入会导致温暖的涡轮机部件,限制它们的寿命和性能显着。另外,由于局部热气体摄入引起的温度中的不对称可能导致扭曲的轴承支撑结构导致有害效果。在这项研究中,通过在包围发动机范围的网络中使用1-D压力,流量和焓模块(Kutz和Sper,1994)来开发一个简单的模型。伪3D建模方法应用于真正的发动机部件,以估计由于局部热气体摄取而导致的损坏程度。结果表明,该模型提供了一种快速而强大的工具,用于估计复杂发动机空腔中的流量和传热信息,其流量极低,而不诉诸复杂,几乎不可能的3-D CFD模拟。在该研究中,模拟了发动机操作期间的冷却空气供应管失效。冷却空气供应管道从高压压缩机(HPC)的空气流出,并进入发动机的帧间过渡管道。通过将其中一个管道通风到大气来模拟供应管的失效。结果证明了次级气流路径中的流动和压力的严重不对称,导致大型局部热气体摄取。此外,大量局部热气体摄取诱导周向温度梯度,导致不均匀的加热和随之而来的静态和旋转部件的扭曲。基于对损害程度的知识,还讨论了纠正安排。

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