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Low Cycle Fatigue Life Estimation and Tracking for Industrial Gas Turbine Blades Using Fatigue Factor Approach

机译:基于疲劳因子方法的工业燃气轮机叶片低周疲劳寿命估计和跟踪

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Low cycle fatigue life consumption analysis was carried out in this work. Fatigue cycles accumulation method suitable even if engine is not often shut down was applied together with the modified universal sloped method for estimating fatigue cycles to failure. Damage summation rule was applied to estimate the fatigue damage accumulated over a given period of engine operation. The concept of fatigue factor which indicates how well engine is operated was introduced to make engine life tracking feasible. The developed fatigue life tracking method was incorporated in PYTHIA, Cranfield University in-house software and applied to 8 months of engine operation. The results obtained are similar to those of real engine operation. At a set power level, fatigue life decreases with increase in ambient temperature with the magnitude of decrease greater at higher power levels. The fatigue life tracking methodology developed could serve as a useful tool to engine operators.
机译:在这项工作中进行了低周疲劳寿命消耗分析。即使发动机不经常停机,疲劳循环累积方法也适用,同时还使用了改进的通用倾斜法来估算故障的疲劳循环。应用损伤求和规则来估计在给定的发动机运行期间累积的疲劳损伤。引入了疲劳因子的概念来指示发动机的运行状况,该疲劳因子表示发动机的运行状况。发达的疲劳寿命跟踪方法已整合到克兰菲尔德大学内部软件PYTHIA中,并适用于8个月的发动机运转。获得的结果与实际发动机运行的结果相似。在设定的功率水平下,疲劳寿命随着环境温度的升高而降低,而在更高的功率水平下,疲劳寿命的降低幅度更大。所开发的疲劳寿命跟踪方法可以为发动机操作员提供有用的工具。

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