ASME STP-NU-041-2011 UPDATE AND IMPROVE SUBSECTION NH C ALTERNATIVE SIMPLIFIED CREEP-FATIGUE DESIGN METHODS《更新和改进分段NH 可替代简化的蠕变疲劳设计方法》.pdf
《ASME STP-NU-041-2011 UPDATE AND IMPROVE SUBSECTION NH C ALTERNATIVE SIMPLIFIED CREEP-FATIGUE DESIGN METHODS《更新和改进分段NH 可替代简化的蠕变疲劳设计方法》.pdf》由会员分享,可在线阅读,更多相关《ASME STP-NU-041-2011 UPDATE AND IMPROVE SUBSECTION NH C ALTERNATIVE SIMPLIFIED CREEP-FATIGUE DESIGN METHODS《更新和改进分段NH 可替代简化的蠕变疲劳设计方法》.pdf(125页珍藏版)》请在麦多课文档分享上搜索。
1、 STP-NU-041 UPDATE AND IMPROVE SUBSECTION NH ALTERNATIVE SIMPLIFIED CREEP-FATIGUE DESIGN METHODS Prepared by: Tai Asayama Japan Atomic Energy Agency Date of Issuance: March 31, 2011 This report was prepared as an account of work sponsored by the U.S. Department of Energy (DOE) and the ASME Standards
2、 Technology, LLC (ASME ST-LLC). This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or re
3、sponsibility for the accuracy, completeness or usefulness of any information, apparatus, product or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process or service by trade name, trademark, manufacturer
4、or otherwise does not necessarily constitute or imply its endorsement, recommendation or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.
5、 Neither ASME, ASME ST-LLC, the author nor others involved in the preparation or review of this report, nor any of their respective employees, members or persons acting on their behalf, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, complet
6、eness or usefulness of any information, apparatus, product or process disclosed, or represents that its use would not infringe upon privately owned rights. Reference herein to any specific commercial product, process or service by trade name, trademark, manufacturer or otherwise does not necessarily
7、 constitute or imply its endorsement, recommendation or favoring by ASME ST-LLC or others involved in the preparation or review of this report, or any agency thereof. The views and opinions of the authors, contributors and reviewers of the report expressed herein do not necessarily reflect those of
8、ASME ST-LLC or others involved in the preparation or review of this report, or any agency thereof. ASME ST-LLC does not take any position with respect to the validity of any patent rights asserted in connection with any items mentioned in this document, and does not undertake to insure anyone utiliz
9、ing a publication against liability for infringement of any applicable Letters Patent, nor assumes any such liability. Users of a publication are expressly advised that determination of the validity of any such patent rights, and the risk of infringement of such rights, is entirely their own respons
10、ibility. Participation by federal agency representative(s) or person(s) affiliated with industry is not to be interpreted as government or industry endorsement of this publication. ASME is the registered trademark of the American Society of Mechanical Engineers. No part of this document may be repro
11、duced in any form, in an electronic retrieval system or otherwise, without the prior written permission of the publisher. ASME Standards Technology, LLC Three Park Avenue, New York, NY 10016-5990 ISBN No. 978-0-7918-3364-3 Copyright 2011 by ASME Standards Technology, LLC All Rights Reserved Alternat
12、ive Simplified Creep-Fatigue Design Methods STP-NU-041 iii TABLE OF CONTENTS Foreword x Executive Summary xi 1 INTRODUCTION . 1 2 PREREQUISITES FOR EVALUATION 2 2.1 Evaluated Data 2 2.2 Representation of Material Properties . 2 2.3 Prediction Using Time Fraction Rule 2 3 OUTLINE AND PREDICTABILITY O
13、F NEWLY PROPOSED CREEP-FATIGUE EVALUATION METHODS . 7 3.1 Modified Ductility Exhaustion Method . 7 3.2 Strain Range Separation Method . 25 3.3 Approach for Pressure Vessel Applications 42 3.4 Hybrid Method of Time Fraction and Ductility Exhaustion . 58 3.5 Simplified Model Test Approach 72 4 POTENTI
14、AL TO DEPLOYING THE METHODS INVESTIGATED TO ASME-NH 79 4.1 Evaluation of Creep-Fatigue Life Predictability of the Methods Investigated in Short-Term and Long-Term Regions 79 4.2 Evaluation of Basic Potential of the Methods Investigated . 98 4.3 Evaluation of Extendibility of the Methods Investigated
15、 102 4.4 Evaluation of Applicability of the Methods Investigated to ASME-NH 103 4.5 Recommendations . 104 5 CONCLUSIONS . 106 References 107 Appendix 1 - Creep fatigue experiment data of Mod.9Cr-1Mo . 109 Acknowledgments 111 LIST OF TABLES Table 1 - Additive Stress in the Rupture Curve 28 LIST OF FI
16、GURES Figure 1 - Creep Rupture Data at 450-600C 2 Figure 2 - Fatigue Data and Design Fatigue Curves at 550C . 3 Figure 3 - Static and Cyclic Stress-Strain Curves at 550C . 3 Figure 4 - Creep-Fatigue Data at 500C 4 Figure 5 - Creep-Fatigue Data at 550C 4 Figure 6 - Creep-Fatigue Data at 600C 5 Figure
17、 7 - Creep-Fatigue Data at 550C (Stress Controlled Tests) 5 STP-NU-041 Alternative Simplified Creep-Fatigue Design Methods iv Figure 8 - Observed and Predicted Creep-Fatigue Life with Time Fraction Rule 6 Figure 9 - Observed and Predicted Creep-Fatigue Life with Time Fraction Rule 6 Figure 10 - Rela
18、tion between Creep Rupture Time and Fracture Elongation . 10 Figure 11 - Relation between Inelastic Strain Rate and Creep Rupture Elongation at 500C 10 Figure 12 - Relation between Inelastic Strain Rate and Creep Rupture Elongation at 550C 11 Figure 13 - Relation between Inelastic Strain Rate and Cr
19、eep Rupture Elongation at 600C 11 Figure 14 - Relation between Temperature and Tensile Fracture Elongation 12 Figure 15 - Observed and Predicted Creep-Fatigue Life by Ductility Exhaustion Method 12 Figure 16 - Creep-Fatigue Damage Calculated by Ductility Exhaustion Method 13 Figure 17 - Observed and
20、 Predicted Creep-Fatigue Life by Modified Ductility Exhaustion Method 13 Figure 18 - Creep-Fatigue Damage Calculated by Modified Ductility Exhaustion Method 14 Figure 19 - Creep-Fatigue Damage Calculated by Modified Ductility Exhaustion Method 14 Figure 20 - Observed and Predicted Creep-Fatigue Life
21、 by Modified Ductility Exhaustion Method 15 Figure 21 - Creep-Fatigue Damage Calculated by Modified Ductility Exhaustion Method 15 Figure 22 - Creep-Fatigue Damage Calculated by Modified Ductility Exhaustion Method 16 Figure 23 - Observed and Predicted Creep-Fatigue Life with Modified Ductility Exha
22、ustion Method for Stress Controlled Tests 16 Figure 24 - Creep-Fatigue Damage Calculated by Modified Ductility Exhaustion Method for Stress Controlled Tests 17 Figure 25 - Ratio of Predicted Life to Observed Life against Hold Time 17 Figure 26 - Life Reduction Coefficient as a Function of Pure Fatig
23、ue Life when p is 0.1 . 18 Figure 27 - Life Reduction Coefficient as a Function of Pure Fatigue Life when p is 0.5 . 18 Figure 28 - Observed and Predicted Creep-Fatigue Life by Modified Ductility Exhaustion Method for Compressive Hold Tests 19 Figure 29 - Observed and Predicted Creep-Fatigue Life by
24、 Modified Ductility Exhaustion Method for Compressive Hold Tests 19 Figure 30 - Observed and Predicted Creep-Fatigue Life by Modified Ductility Exhaustion Method 20 Figure 31 - Observed and Predicted Creep-Fatigue Life by Modified Ductility Exhaustion Method 20 Figure 32 - Observed and Predicted Ten
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