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钻井工具多轴高周疲劳寿命预测模型优选 被引量:1
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作者 Narayanan Govindarajan 《石油勘探与开发》 SCIE EI CAS CSCD 北大核心 2015年第6期808-811,共4页
针对钻井工具多轴高周疲劳问题,进行了疲劳寿命预测模型优选。结合多轴疲劳理论,分析了非比例加载条件下的多轴应力状态及多轴疲劳情况下材料开裂行为,总结了多轴疲劳模型,并推荐Dang Van模型用于判断钻井工具在特定应力下是否会发生疲... 针对钻井工具多轴高周疲劳问题,进行了疲劳寿命预测模型优选。结合多轴疲劳理论,分析了非比例加载条件下的多轴应力状态及多轴疲劳情况下材料开裂行为,总结了多轴疲劳模型,并推荐Dang Van模型用于判断钻井工具在特定应力下是否会发生疲劳失效。介绍了Dang Van模型的基本准则、推导原理、适用范围及疲劳极限计算公式。基于钻井现场实际应用的稳定器转向定子驱动轴实际故障验证了Dang Van多轴疲劳模型,并将其与原始平均应力模型进行了对比,结果表明,原始平均应力模型计算结果偏于保守,Dang Van模型更适用于钻井工具多轴高周疲劳寿命预测。 展开更多
关键词 钻井工具 非比例载荷 多轴高周疲劳 疲劳寿命 预测模型
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Influence of Turbulators in Blade Cooling Passages on Film Hole Discharge Coefficients
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作者 H.-P. SCHIFFER J. TAEGE F. HASELBACH 《Journal of Thermal Science》 SCIE EI CAS CSCD 2004年第3期245-254,共10页
This paper details the results of a joint project between Rolls-Royce Deutschland (RRD) and the Northwestern Polytechnical University of China (NWPU). The objective of the project was the determination of the influenc... This paper details the results of a joint project between Rolls-Royce Deutschland (RRD) and the Northwestern Polytechnical University of China (NWPU). The objective of the project was the determination of the influence of tabulators in turbine blade cooling passages on film hole discharge coefficients (Cd coefficients). A large-scale plexiglas model was used by the NWPU to measure the turbulator influence on Cd coefficients for a wide range of different geometrical parameters, Reynolds numbers and cooling flow off take ratios. RRD specified the comprehensive test matrix and analysed the test data. The CFD code FLUENT was used by RRD for numerical simulation of the test cases with the main objective to support the interpretation of observed trends. Both, experimental and numerical results will be presented in this paper for a selection of test configurations. 展开更多
关键词 film HOLE DISCHARGE COEFFICIENT TURBULATOR BLADE cooling.
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AITEB - An European Research Project on Aero-thermodynamics of Turbine Endwalls and Blades
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作者 F. HASELBACH H.-P. SCHIFFER 《Journal of Thermal Science》 SCIE EI CAS CSCD 2004年第2期97-108,共12页
The paper delivers an overview on the European research project AITEB - Aerothermal Investigations on Turbine Endwalls and Blades, which started in year 2000 in the course of the 5. Framework Programme (GROWTH). The a... The paper delivers an overview on the European research project AITEB - Aerothermal Investigations on Turbine Endwalls and Blades, which started in year 2000 in the course of the 5. Framework Programme (GROWTH). The aim is to submit an integrated technology and design tool package for the advanced, aerothermal highly loaded design of turbines, especially: Experimental/numerical investigation on heat transfer and film-cooling in separated flow for highly loaded blades including advanced trailing edge cooling Heat transfer/ improved cooling of turbine endwalls: Experimental/numerical work on cooling of turbine endwalls, shrouds and recessed blade tips. Optimised CFD-process (drawing-grid-modelling-postprocessing-risk assessment) in order to derive the 'best practice' to use CFD as a time effective tool. After most of the project life, an overview on the project is delivered. Experimental results of test series at various test sites are compared to numerical simulations of the industrial and university partners. 展开更多
关键词 turbines aerothermal endwalls BLADES cooling-technology EXPERIMENT CFD.
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