Lifetime prediction modeling of airfoils for advanced power generation

作者: Ventzislav Gueorguiev Karaivanov

DOI:

关键词: Finite element methodElectricity generationMechanical engineeringWorking fluidCreepMaterials scienceDamage mechanicsTurbineAirfoilNanoindentation

摘要: The use of gases produced from coal as a turbine fuel offers an attractive means for efficiently generating electric power our Nation's most abundant fossil resource. oxy-fuel and hydrogen-fired concepts promise increased efficiency low emissions on the expense inlet temperature (TIT) different working fluid. Developing technology materials is critical to creation these near-zero emission generation technologies. A computational methodology, based three-dimensional finite element analysis (FEA) damage mechanics presented predicting evolution creep fatigue in airfoils. We took first look at airfoil thermal distributions advanced systems CFD analysis. mechanics-based models were implemented user modified routine commercial package ANSYS. This was used visualize over airfoils turbines concepts, regions susceptible failure indentified. Model allows interaction between thus due processes acting separately one cycle will affect both rates next cycle. Simulation results various conductivity top coat. Surface maps created showing development TGO scale Al depletion bond coat.In conjunction with model development, laboratory-scale experimental validation executed evaluate influence operational compressive stress levels performance TBC system. coated single crystal coupons exposed isothermally air 900, 1000, 1100oC without load. Exposed samples cross-sectioned evaluated scanning electron microscope (SEM). Performance data collected image Energy-dispersive x-ray (EDX) employed study elemental distribution system after exposure. Nanoindentation mechanical properties (Young's modulus hardness) components their time.

参考文章(18)
R. W. Trice, Y. Jennifer Su, J. R. Mawdsley, K. T. Faber, A. R. De Arellano-López, Hsin Wang, W. D. Porter, Effect of heat treatment on phase stability, microstructure, and thermal conductivity of plasma-sprayed YSZ Journal of Materials Science. ,vol. 37, pp. 2359- 2365 ,(2002) , 10.1023/A:1015310509520
Jean Lemaitre, A Course on damage mechanics Springer Berlin Heidelberg. ,(1992) , 10.1007/978-3-642-18255-6
H. Echsler, D. Renusch, M. Schütze, Bond coat oxidation and its significance for life expectancy of thermal barrier coating systems Materials Science and Technology. ,vol. 20, pp. 307- 318 ,(2004) , 10.1179/026708304225012143
F. J. Cunha, M. T. Dahmer, M. K. Chyu, Thermal-Mechanical Life Prediction System for Anisotropic Turbine Components Journal of Turbomachinery-transactions of The Asme. ,vol. 128, pp. 240- 250 ,(2006) , 10.1115/1.2137740
D. W. MacLachlan, D. M. Knowles, Fatigue behaviour and lifing of two single crystal superalloys Fatigue & Fracture of Engineering Materials & Structures. ,vol. 24, pp. 503- 521 ,(2001) , 10.1046/J.1460-2695.2001.00392.X
G. R. Wallwork, A. Z. Hed, SOME LIMITING FACTORS IN THE USE OF ALLOYS AT HIGH TEMPERATURES. Oxidation of Metals. ,vol. 3, pp. 171- 184 ,(1971) , 10.1007/BF00603485
D.W. MacLachlan, D.M. Knowles, Modelling and prediction of the stress rupture behaviour of single crystal superalloys Materials Science and Engineering A-structural Materials Properties Microstructure and Processing. ,vol. 302, pp. 275- 285 ,(2001) , 10.1016/S0921-5093(00)01829-3
Danny W. Mazzotta, Minking K. Chyu, Mary Anne Alvin, Airfoil Heat Transfer Characteristics in Syngas and Hydrogen Turbines Volume 3: Turbo Expo 2007. pp. 793- 801 ,(2007) , 10.1115/GT2007-28296
Jean Lemaitre, How to use damage mechanics Nuclear Engineering and Design. ,vol. 80, pp. 233- 245 ,(1984) , 10.1016/0029-5493(84)90169-9