Crack propagation life prediction of a perforated plate under thermal fatigue

被引:10
|
作者
Tokiyoshi, T [1 ]
Kawashima, F [1 ]
Igari, T [1 ]
Kino, H [1 ]
机构
[1] Mitsubishi Heavy Ind Co Ltd, Nagasaki R&D Ctr, Nagasaki 8510392, Japan
关键词
crack propagation; perforated plate; thermal fatigue; reference stress; boiler header; ligament crack;
D O I
10.1016/S0308-0161(01)00098-9
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Superheater outlet headers of boilers are well known to be subjected to the cycling of high pressure and high thermal stress during pant operations. Thermal stresses during cyclic operation are generally severest on the inside surface of the ligaments between the stub-tube holes, where many examples of ligament cracking due to thermal fatigue have been found recently. A method to predict the crack propagation life of the ligaments of boiler headers under thermal fatigue has been required. Firstly in this paper, to model the crack propagation behavior of the ligament regions of boiler headers, a perforated plate of normalized and tempered 2 1/4Cr-1Mo steel was examined under out-of-phase thermal fatigue at a maximum temperature of 600degreesC in the air. Inelastic analysis of the perforated plate under thermal fatigue was carried out, and the nonlinear fracture mechanics parameters such as the J and C* integral were obtained by the line integral for observed cracks. A simplified method was proposed for predicting these parameters under displacement-controlled conditions such as thermal fatigue. In this method, the change of the macroscopic stress-strain relation of the perforated plate with propagating cracks was combined with the reference stress concept under displacement-controlled conditions. The predicted fracture mechanics parameters from this method coincided well with those from the inelastic analysis. The prediction of the crack propagation life on the basis of the proposed method provided a good correspondence with the test results of the perforated plate under thermal fatigue. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:837 / 845
页数:9
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