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SENSITIVITY ANALYSIS AND UNCERTAINTY QUANTIFICATION FOR RIM SEAL INGESTION WITH 1-D NETWORK MODELS

机译:用1-D网络模型对RIM密封摄取的敏感性分析及不确定度量化

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Accurate prediction of turbine rim seal ingestion remains a challenge, even sophisticated unsteady computational models have had limited success due to the complexity and uncertainties present in this type of problems. For this reason, it is of interest to perform stochastic analysis taking into account the variability in the input parameters as well as uncertainties and assumptions associated with a given model of choice. This study focuses on a Secondary Air System (SAS) of a gas turbine, considering a generic cavity in a high pressure turbine (HPT) in which hot gas ingestion occurs and uncertainty in geometrical, operational and modelling parameters is present. Several statistical methods are applied to a 1D gas network model in order to evaluate the impact of the tolerances of the main geometrical parameters in the output, followed by a broader analysis including other operational and modelling variables. Results indicate that most influential parameters are the sealant mass flow rate, a modelling constant and the minimum gap of the wheelspace cavity.
机译:精确预测涡轮边缘密封摄入仍然是一个挑战,甚至在这种类型问题中存在的复杂性和不确定性,甚至复杂的不稳定计算模型也有有限的成功。因此,考虑到输入参数的可变性以及与给定的选择模型相关联的不确定性和假设,表达随机分析感兴趣。本研究专注于燃气轮机的二级空气系统(SAS),考虑到高压涡轮机(HPT)中的通用腔,其中存在热气体摄取和在几何,操作和建模参数中的不确定性。将几种统计方法应用于1D气体网络模型,以便评估输出中主要几何参数的公差的影响,然后是更广泛的分析,包括其他操作和建模变量。结果表明,大多数有影响力的参数是密封剂质量流速,模型恒定和轮空腔的最小间隙。

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