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汽轮机隔板高温蠕变寿命评估方法的研究 被引量:3

An Assessment Method of High Temperature Creep Life of Steam Turbine Diaphragm
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摘要 针对现役引进型机组高温蠕变现象难于正确评估的情况,提出了根据机组历次大修记录的变形数据和有限元计算相结合的方法得到材料蠕变参数.采用该方法对某电厂600 MW机组T11级隔板的高温蠕变变形问题进行了分析研究,并应用商用软件对隔板在继续运行中的变形和应力情况作出了预测和评估.结果表明:隔板最大应力产生的位置在隔板外环叶片的出汽侧,靠近中分面边缘叶根、叶片的出汽边处,其值为160 MPa.按每年连续运行8 000 h计算,隔板的使用寿命约为30年,与制造商提供的设计寿命一致,得出了机组在一个大修期内不必立即更换隔板的结论,节约了维修费用,为汽轮机或燃气轮机高温部件的蠕变寿命的评估提供了一种实用方法. Aiming at the difficult to assess high temperature creep in the imported unit properly, a method was put forward, which is to get material creep parameters by history deformation data of the diaphragm recorded in all previous overhaul, combined with the finite element analysis. By the method, the creep deformation under high temperature conditions was analyzed for Tll diaphragm of the 600 MW turbine, the prediction and assess for the deformation and stress of the diaphragm in posterior operation were done by commercial software. Results show that the highest stress of the diaphragm appeared at the blade's exit side of the shroud, at the blade root and trailing edge near the adge of horizontal split with its value of 160 MPa. If the unit runs 8000 hours every year, the hours that the diaphragm may be continuously used in service is about 30 years. It is same to the manufacturer's design data. So the diaphragm may not be replaced during a period of overhaul, and the maintenance costs are saved. It offers a practical method to assess the creep life of high temperature part of steam turbine and gas turbine.
出处 《动力工程》 CSCD 北大核心 2009年第3期232-235,共4页 Power Engineering
关键词 汽轮机 隔板 寿命 高温蠕变 Ansys计算 steam turbine diaphragm life high temperature creep Ansys calculation
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  • 1王正东.[D].上海:华东化工学院,1986.
  • 2Ainsworth R A, Hooton D G, Green G. Failure Assessment Diagrams for High Temperature Defect Assessment. Engineering Fracture Mechanics,1999, 62(1): 95-109.
  • 3Wang Z D, Wu D D. A Damage Mechanics Approach to the Prediction of Creep Crack Growth. Int. J. of Pres. Vessel & Piping, 1991, 18(3):305-319 .
  • 4Davies CM, O'Dowd NP, Dean DW, et al. Failure assessment diagram analysis of creep crack initiation in 316H stainless steel,Int. J of Pres. Ves & Piping[J]. 2003, 80:541-551.
  • 5ASTM Standrad E1457-98. Standrad test method for measuring creep crack growth rates in metals, ASTM Philadelphia[M].1998.
  • 6.GB 2030-80 金属拉伸蠕变试验方法[S].北京:国家标准出版社,1981..
  • 7Koichi YG, Masaaki T, Kiyoshi KB. The influence of fracture mechanisms on the creep crack growt benaviour of 316 stainless steel, Engineering Fracture Mechanics[J]. 1997, (5): 463- 473.
  • 8王正东.[D].上海:华东化工学院,1986.
  • 9BS 7910. Guide to methods assessing the acceptability of flaws in fusion welded structures. London:BSI[M]. 1999.
  • 10轩福贞,涂善东,王正东,罗娜.高温环境下在用压力容器检测与安全评估技术研究进展(一)——检测技术及数据库[J].压力容器,2002,19(9):1-4. 被引量:5

共引文献9

同被引文献16

  • 1刘平.典型隔板的强度刚度有限元分析[J].汽轮机技术,2004,46(5):333-335. 被引量:5
  • 2轩福贞,涂善东,王正东.材料的蠕变断裂韧性及影响因素分析[J].中国机械工程,2005,16(5):456-460. 被引量:7
  • 3于涵,戴兴建,沈祖培.储能飞轮轮毂的蠕变温度特性与蠕变影响[J].清华大学学报(自然科学版),2006,46(6):805-808. 被引量:2
  • 4Prasad S C, Rao I J,Rajagopal K R. A continuum model for the creep of single crystal nickel-base superalloys [ J ]. Aeta Materialia, 2005,53 (3) :669-679.
  • 5马显锋.用于大型燃气轮机的镍基单品合金高温低周疲劳性能研究[D].北京:清华大学工程力学系,2010.
  • 6Diologent F, Caron P. On the creep behavior at 1033 C of new generation single-crystal superalloys [ J ]. Materials Science and Engineering: A, 2004,385 ( 1-2 ) :245-257.
  • 7张俊善.材料的高温变形与断裂[M]北京:科学出版社,20073-4.
  • 8王恭义;程凯;徐芬.百万超超临界汽轮机高压缸旋转部件热弹性-蠕变分析[A]黑龙江哈尔滨,2010511-520.
  • 9MONDOLF LF. Aluminum alloys:structure and properties[M].London:Butterworth-Heinemann,1974.34-35.
  • 10Chen J P, Yang G H, Yang B. Finite element analysis ofsteam turbine diaphragm [J]. Computer Aided Drafting,Design and Manufacturing, 2014, 24(4): 60-63.

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