[1] U.S. Department of Transportation, Federal Aviation Administration. Guidance material for aircraft engine life-limited parts requirements:Advisory Circular 33.70-1[R]. Washington, D.C.:FAA, 2009:30-50.
[2] VITTAL S, HAJELA P, JOSHI A. Review of approaches to gas turbine life management:AIAA-2004-4372[R]. Reston:AIAA, 2004:2-5.
[3] 王卫国. 轮盘低循环疲劳寿命预测模型和试验评估方法研究[D]. 南京:南京航空航天大学, 2006:25-53. WANG W G. Disc LCF life prediction models and experiment assessment methodologies[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2006:25-53(in Chinese).
[4] U.S. Department of Defense. Engine structural integrity program:MIL-HDBK-1783B[S]. Washington, D.C.:U.S. Department of Defense, 2002:13-18.
[5] 丁水汀, 张弓, 蔚夺魁, 等. 航空发动机适航概率风险评估方法研究综述[J]. 航空动力学报, 2011, 26(7):1142-1143. DING S T, ZHANG G, YU D K, et al. Review of probabilistic risk assessment on aero-engine airworthiness[J]. Journal of Aerospace Power, 2011, 26(7):1142-1143(in Chinese).
[6] MCCLUNG R C, LEVERANT G R, ENRIGHT M P. Turbine rotor material design-Phase Ⅱ:Grant 99-G-016[R]. Washington, D.C.:FAA, 2008:50-55.
[7] DENG J, GU D S, LI X B, et al. Structural reliability analysis for implicit performance functions using artificial neural network[J]. Structural Safety, 2005, 27(1):25-48.
[8] GOMES H M, AWRUCH A M. Comparison of response surface and neural network with other methods for structural reliability analysis[J]. Structural Safety, 2004, 26(1):49-67.
[9] GUPTA S, MANOHAR C S. An improved response surface method for the determination of failure probability and importance measure[J]. Structure Safety, 2004, 26(2):123-139.
[10] ZHU M H, ZHOU Z R. Composite fretting wear of aluminum alloy[J]. Key Engineering Materials, 2007, 353-358:868-873.
[11] GAVIN H P, YAU S C. High-order limit state functions in the response surface method for structural reliability analysis[J]. Structural Safety, 2008, 30(2):162-179.
[12] JIN C G, LI Q S, XIAO R C. A new artificial neural network-based response surface method for structural reliability analysis[J]. Probabilistic Engineering Mechanics, 2008, 23(1):51-63.
[13] GUAN X L, MELCHERS R E. Effect of response surface parameter variation on structural reliability estimates[J]. Structural & Safety, 2001, 23(4):429-438.
[14] KIM S H, NA S W. Response surface method using vector projected sampling points[J]. Structural & Safety, 1997, 19(1):3-19.
[15] GAVIN H P, YAU S C. High-order limit state functions in the response surface method for structural reliability analysis[J]. Structural & Safety, 2008, 30(2):162-179.
[16] KLEIJNEN J P C. Kriging metamodeling in simulation:A review[J]. European Journal of Operation Research, 2009, 192(3):707-716.
[17] KAPPAS J. Review of risk and reliability methods for aircraft gas turbine engines:DSTO-TR-1306[R]. Victoria, Australia:DSTO Aeronautical and Maritime Research Laboratory, 2002:20-30.
[18] MILLWATER H R, ENRIGHT M P, FITCH S H K. A convergent probabilistic technique for risk assessment of gas turbine disks subject to metallurgical defects:AIAA-2002-1382[R]. Reston:AIAA, 2002:1-3.
[19] WU Y T, ENRIGHT M P, MILLWATER H R. Probalistic methods for design assessment of reliability with inspection[J]. AIAA Journal, 2002, 40(5):937-946.
[20] U.S. Department of Transportation, Faderal Aviation Adminisrtation. Airworthiness standards:Aircraft engines:CFR 14 Part 33[S]. Washington, D.C.:FAA, 2009:10-30.
[21] KAYMAZ I. Application of Kriging method to structural reliability problems[J]. Structural Safety, 2005, 27(2):133-151.
[22] BICHON B J, ELDRED M S, SWILER L P, et al. Efficient global reliability analysis for nonlinear implicit performance functions[J]. AIAA Journal, 2008, 46(10):2459-2468.
[23] SAE International. Guidelines and methods for conducting the safety assessment process on civil airborne systems and equipment:ARP 4761[S]. New York:SAE International, 1996:20-30.
[24] 黄庆南, 张连祥. 航空发动机转子非包容顶层事件安全性分析与思考[J]. 航空动力学报, 2009, 35(2):6-9. HUNG Q N, ZHANG L X. Safety analysis and thought of uncontained top event for aero-engine rotor[J]. Journal of Aerospace Power, 2009, 35(2):6-9(in Chinese).
[25] 姚卫星. 结构疲劳寿命分析[M]. 北京:国防工业出版社, 2003:72-73. YAO W X. Fatigue life prediction of structures[M]. Beijing:National Defence Industry Press, 2003:72-73(in Chinese).
[26] 吴学仁. 飞机结构金属材料力学性能手册:静强度疲劳/耐久性[M]. 北京:航空工业出版社, 1997:30-35. WU X R. Handbook of mechanical prosperities of aircraft structural metals:Static strength/durability[M]. Beijing:Aviation Industry Press, 1997:30-35(in Chinese). |