ASME STP-PT-087-2018 YIELD STRENGTH VALUES UP TO MAXIMUM TEMPERATURE DESIGN.pdf

1、YIELD STRENGTH VALUES UP TO MAXIMUM TEMPERATURE DESIGNSTP-PT-087STP-PT-087 YIELD STRENGTH VALUES UP TO MAXIMUM TEMPERATURE DESIGN Prepared by: Wolfgang Hoffelner RWH consult GmbH Date of Issuance: June 22, 2018 This publication was prepared by ASME Standards Technology, LLC (“ASME ST-LLC”) and spons

2、ored by The American Society of Mechanical Engineers (“ASME”). Neither ASME, ASME ST-LLC, the author, nor others involved in the preparation or review of this publication, nor any of their respective employees, members, or persons acting on their behalf, makes any warranty, express or implied, or as

3、sumes any legal liability or responsibility for the accuracy, completeness, 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 b

4、y trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by ASME ST-LLC or others involved in the preparation or review of this publication, or any agency thereof. The views and opinions of the authors, contributors and

5、 reviewers of the publication expressed herein do not necessarily reflect those of ASME ST-LLC or others involved in the preparation or review of this publication, or any agency thereof. ASME ST-LLC does not take any position with respect to the validity of any patent rights asserted in connection w

6、ith any items mentioned in this document, and does not undertake to insure anyone utilizing 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 p

7、atent rights, and the risk of infringement of such rights, is entirely their own responsibility. 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 trademar

8、k of the American Society of Mechanical Engineers. No part of this document may be reproduced in any form, in an electronic retrieval system or otherwise, without the prior written permission of the publisher. ASME Standards Technology, LLC Two Park Avenue, New York, NY 10016-5990 ISBN No. 978-0-791

9、8-7242-0 Copyright 2018 ASME Standards Technology, LLC All Rights Reserved STP-PT-087: Yield Strength Values up to Maximum Temperature Design iii TABLE OF CONTENTS Foreword . viii Abstract ix Abbreviations and Acronyms . x 1 INTRODUCTION 1 2 STEELS 5 2.1 S20910 / XM-19/ 22Cr-13Ni-5Mn up to 1200F 5 2

10、.2 S30400/ 304/ 18Cr-8Ni up to 1500F 8 2.3 S30403/ 304L/18Cr-8Ni up to 1200F 11 2.4 S30908/ 309 S/ 23Cr-12Ni up to 1500F . 14 2.5 S31008/ 310 S/ 25Cr-20Ni up to 1500F . 17 2.6 S31600/SS 316/ 16Cr-12Ni-2Mo up to 1500F . 20 2.7 S31603/ 316L/ 16Cr-12Ni-2Mo up to 1200F . 22 2.8 S31635/ 316Ti/16Cr-12Ni-2

11、Mo-Ti up to 1500F 24 2.9 S31700/ SS317/and S31703/SS317 L/ 18Cr-13Ni-3Mo up to 1500F (1200F) 27 2.10 S32100/ SS321/ 18Cr-10Ni-Ti up to 1500F . 28 2.11 S34700/ SS347 and S34800/ SS348/ 18Cr-10Ni-Cb up to 1500F . 31 3 COPPER . 34 3.1 C23000 / Cu 230 / 85 Cu-15 Zn up to 500F . 34 3.2 C28000 / Cu 280 /

12、59 Cu-40Zn-0.07Fe-0.3Pb up to 500F . 35 3.3 C36500 / Cu 365 / 60Cu-39.4 Zn-0.6 Pb . 37 3.4 C44300 / Cu 443 C44400 / Cu 444 C44500 / Cu 445 up to 500F . 38 3.5 C46400 / Cu 464 C46500 / Cu-465 up to 500F 41 3.6 C64200 / Cu 642 / 91.2 Cu, 7.0 Al, 1.8 Si up to 500F . 42 3.7 C68700 / Cu 687 / 77.5 Cu, 20

13、.5 Zn, 2.0 Al, 0.1 As up to 500F 44 3.8 C70400 / Cu 704 / 92.4 Cu, 5.5 Ni, 1.5 Fe, 0.6 Mn up to 500F . 46 3.9 C71000 / Cu 710 / 79 Cu, 21 Ni up to 700F 47 4 NICKEL . 49 4.1 N02201 / Ni 201 up to 1200F . 49 4.2 N06002 / Ni X up to 1650F 52 4.3 N06022 up to 1250F . 55 4.4 N06600 / Ni 600 up to 1200F .

14、 58 4.5 Annealed 58 4.6 Hot Worked 61 4.7 Seamless Pipe 63 4.8 N06625 / Ni 625 SA up to 1600F. 65 4.9 N06625 / Ni 625 Ann up to 1200F . 68 4.10 N08330 / Ni 330 up to 1650F . 71 4.11 N08800 / Ni 800 up to 1500F . 74 4.12 N08810 / Ni 800H and N08811 / Ni 811 up to 1650F . 77 4.13 N10276 / Ni C276 up t

15、o 1500F 80 STP-PT-087: Yield Strength Values up to Maximum Temperature Design iv 4.14 N10003 / Ni N / Hastelloy N up to 1500F 83 Appendix A . 86 LIST OF FIGURES Figure 1-1: List of steels and required maximum temperatures . 2 Figure 1-2: Current ASME Y-1 data and data from the current new evaluation

16、 3 Figure 1-3: Matching current Y-1 data and new evaluation by shifting the new curve. Using 1.045 instead of 1.07 as constant in the polynomial for the new values . 3 Figure 1-4: Matching current Y-1 data and new evaluation by making a joint polynomial fit . 4 Figure 2-1: YS stress ratios from curr

17、ent ASME (2015) Y-1 Tables compared with literature data (Material: S20910 / XM-19/ 22Cr-13Ni-5Mn) . 5 Figure 2-2: Graphical representations of the customary Y-1 data S20910 / XM-19/ 22Cr-13Ni-5Mn 6 Figure 2-3: Graphical representations of the metric Y-1 data S20910 / XM-19/ 22Cr-13Ni-5Mn 6 Figure 2

18、-4: YS stress ratios (customary and metric) for XM-19 up to 1200 F . 7 Figure 2-5: YS stress ratios from current ASME (2015) Y-1 Tables compared with literature data (Material: S30400/ 304/ 18Cr-8Ni) . 8 Figure 2-6: YS stress ratios from current ASME (2015) Y-1 Tables compared with polynomial fit th

19、rough literature data . 8 Figure 2-7: Plot of proposed customary YS stress reduction factors for S30400. Y-1-new obtained using 1.07 instead of 1.1 in the polynomial 9 Figure 2-8: Plot of proposed metric YS stress reduction factors for S30400. Y-1-new obtained using 1.07 instead of 1.1 in the polyno

20、mial 9 Figure 2-9: YS stress ratios (customary and metric) for SS304 up to 1500 F. Y-1-new obtained using 1.07 instead of 1.1 in the polynomial 10 Figure 2-10: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S30403) . 11 Figure 2-11: Polynom

21、ial fit through relevant data (material S30403) 11 Figure 2-12: Plot of proposed customary YS stress reduction factors for S304L. Y-1-new obtained using 1.07 instead of 1.1 in the polynomial 12 Figure 2-13: Plot of proposed metric YS stress reduction factors for S304L. Y-1-new obtained using 1.16 in

22、stead of 1.1 in the polynomial 12 Figure 2-14: YS stress ratios (customary and metric) for S304L up to 1200F. Y-1-new obtained using 1.16 instead of 1.1 in the polynomial 13 Figure 2-15: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S30908

23、) . 14 Figure 2-16: Polynomial fit through relevant data (material S30908) 14 Figure 2-17: Plot of proposed customary YS stress reduction factors for S30908 . 15 Figure 2-18: Plot of proposed metric YS stress reduction factors for S30908 . 15 Figure 2-19: YS stress ratios (customary and metric) for

24、S30908 up to 1500F 16 Figure 2-20: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S31008) . 17 Figure 2-21: Polynomial fit through relevant data (material: S31008) . 17 Figure 2-22: Plot of proposed customary YS stress reduction factors for

25、 S31008 . 18 Figure 2-23: Plot of proposed metric YS stress reduction factors for S31008 . 18 Figure 2-24: YS stress ratios (customary and metric) for S31008 up to 1500F 19 Figure 2-25: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S31600)

26、 . 20 Figure 2-26: Plot of proposed customary YS stress reduction factors for S31600 . 20 Figure 2-27: Plot of proposed metric YS stress reduction factors for S31600 . 21 Figure 2-28: YS stress ratios (customary and metric) for S31600 up to 1500F 21 STP-PT-087: Yield Strength Values up to Maximum Te

27、mperature Design v Figure 2-29: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S31603) . 22 Figure 2-30: Plot of proposed customary YS stress reduction factors for S31603 . 22 Figure 2-31: Plot of proposed metric YS stress reduction factors

28、 for S31603 . 23 Figure 2-32: Yield strength reduction factors for S31603 up to 1200F 23 Figure 2-33: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S31635) . 24 Figure 2-34: ATI data for S316, 316L, 317, 317L and 316Ti 24 Figure 2-35: Plot

29、 of proposed customary YS stress reduction factors for S31635 . 25 Figure 2-36: Plot of proposed metric YS stress reduction factors for S31635 . 25 Figure 2-37: Yield strength reduction factors for S31635 up to 1500F 26 Figure 2-38: YS strength reduction factors for 317 and 317L from current Y-1 Tab

30、les 27 Figure 2-39: YS strength reduction factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S32100) . 28 Figure 2-40: Plot of proposed customary YS stress reduction factors for S32100. Y-1-new obtained using 1.04 instead of 1.06 in the polynomial 28 Figure 2-41: Pl

31、ot of proposed metric YS stress reduction factors for S32100. Y-1-new obtained using 1.04 instead of 1.06 in the polynomial 29 Figure 2-42: YS stress ratios (customary and metric) for S32100 up to 1500F. Y-1-new obtained using 1.04 instead of 1.06 in the polynomial 30 Figure 2-43: YS strength reduct

32、ion factors from current ASME (2015)-Y-1 Tables compared with literature data (material: S34700) . 31 Figure 2-44: Plot of proposed customary YS stress reduction factors for S34700. Y-1-new obtained using 1.08 instead of 1.1 in the polynomial 31 Figure 2-45: Plot of proposed metric YS stress reducti

33、on factors for S34700. Y-1-new obtained using 1.08 instead of 1.1 in the polynomial 32 Figure 2-46: Yield strength reduction factors for SS347 and SS348 up to 1500F 33 Figure 3-1: Comparison of available data for C23000 34 Figure 3-2: Proposed YS stress ratios for C23000 up to 600F. Current B1 Table

34、 values remain the same 34 Figure 3-3: Yield strength reduction factors for C23000 35 Figure 3-4: Comparison of available data; 1_B: (Table 1B allowable stress*3)/(2 YS at RT) (material C28000). 35 Figure 3-5: Proposed YS stress ratios for C28000 up to 500F. Current B-1 Table values remain the same

35、36 Figure 3-6: Yield strength reduction factors for C28000 36 Figure 3-7: Comparison of available data . 37 Figure 3-8: Proposed YS stress ratios for C36500 up to 500F 37 Figure 3-9: Yield strength reduction factors for C36500 38 Figure 3-10: Comparison of available data; C44300, C44400 and C44500 a

36、re expected to show the same tensile data. B-1: (Table 1B allowable stress*3)/(2 YS at RT) 38 Figure 3-11: Proposed YS stress ratios for C44300, C44400 and C44500 . 39 Figure 3-12: Proposed YS stress ratios for annealed C44300, C44400 and C44500 39 Figure 3-13: Comparison of data from Record 15-539

37、with data shown in Figure 3-10. It is proposed to use the 15-539 data . 40 Figure 3-14: Yield strength reduction factors for C44300, C44400 and C44500 based on 15-539 data40 Figure 3-15: Comparison of available data; C46400 and C46500 are expected to show the same tensile data. B-1: (Table 1B allowa

38、ble stress*3)/(2 YS at RT) 41 Figure 3-16: Proposed YS stress ratios for C46400 and C46500 . 41 Figure 3-17: Yield strength reduction factors for C46400 and C46500 . 42 Figure 3-18: Comparison of available data; C64200. 1-B: (Table 1B allowable stress*3)/(2 YS at RT)42 STP-PT-087: Yield Strength Val

39、ues up to Maximum Temperature Design vi Figure 3-19: Proposed YS stress ratios for C64200 43 Figure 3-20: Yield strength reduction factors for C64200 43 Figure 3-21: Comparison of available data for C68700. Y-1: (Table 1B allowable stress*3)/(2 YS at RT) 44 Figure 3-22: Proposed YS stress ratios for

40、 C68700 44 Figure 3-23: Comparison of data for C68700 from Gene Shapiro with the current evaluation. Up to 700F no differences were found 45 Figure 3-24: Yield strength reduction factors for C68700 45 Figure 3-25: Comparison of available data for C70400 46 Figure 3-26: Proposed YS stress ratios for

41、C70400 46 Figure 3-27: Yield strength reduction factors for C70400 47 Figure 3-28: Comparison of available data for C71000. 1-B: (Table 1B allowable stress*3)/(2 YS at RT) 47 Figure 3-29: Proposed YS stress ratios for C71000 48 Figure 3-30: Yield strength reduction factors for C71000 48 Figure 4-1:

42、Comparison of available data for N02201. Y-1: Taken from Table IID Y-1 . 49 Figure 4-2: Proposed YS stress ratios for N02201 49 Figure 4-3: Plot of proposed customary YS stress reduction factors for N02201 using 1.03 instead of 1.07 in the polynomial 50 Figure 4-4: Plot of proposed metric YS stress

43、reduction factors for N02201 using 1.03 instead of 1.07 in the polynomial 50 Figure 4-5: Yield strength reduction factors for N02201 using 1.03 instead of 1.07 in the polynomial51 Figure 4-6: Comparison of available data for N06002. Y-1 Hast X: Table IID Y-1 values . 52 Figure 4-7: Proposed YS stres

44、s ratios for N06002 52 Figure 4-8: Plot of proposed customary YS stress reduction factors for N06002 53 Figure 4-9: Plot of proposed metric YS stress reduction factors for N06002 . 53 Figure 4-10: Yield strength reduction factors for N06002 54 Figure 4-11: Comparison of available data for N06022. Y-

45、1: Taken from Table IID Y-1 55 Figure 4-12: Proposed YS stress ratios for N06022 . 55 Figure 4-13: Plot of proposed customary YS stress reduction factors for N06022 using 1.09 instead of 1.0834 in the polynomial 56 Figure 4-14: Plot of proposed metric YS stress reduction factors for N06022 using 1.0

46、9 instead of 1.0834 in the polynomial 56 Figure 4-15: Yield strength reduction factors for N06022 using 1.09 instead of 1.0834 in the polynomial57 Figure 4-16: Comparison of available data for N06600. Several Y-1 values were taken from Table IID Y-1 58 Figure 4-17: Proposed YS stress ratios for N066

47、00 annealed 58 Figure 4-18: Plot of proposed customary YS stress reduction factors for N06600 annealed using 1.05 instead of 1.10 in the polynomial 59 Figure 4-19: Plot of proposed metric YS stress reduction factors for N06600 annealed using 1.05 instead of 1.10 in the polynomial 59 Figure 4-20: Yie

48、ld strength reduction factors for N06600 annealed using 1.05 instead of 1.1 in the polynomial 60 Figure 4-21: Proposed YS stress ratios for N06600 hot worked 61 Figure 4-22: Plot of proposed customary YS stress reduction factors for N06600 hot worked using 0.98 instead of 1.0078 in the polynomial 61

49、 Figure 4-23: Plot of proposed metric YS stress reduction factors for N06600 hot worked using 0.98 instead of 1.0078 in the polynomial 62 Figure 4-24: Yield strength reduction factors for N06600 hot worked using 0.98 instead of 1.0078 in the polynomial 62 STP-PT-087: Yield Strength Values up to Maximum Temperature Design vii Figure 4-25: Proposed YS stress ratios for N06600 seamless pipe 63 Figure 4-26: Plot of proposed customary YS stress reduction factors for N06600 seamless pipe using 1.045 instead of 1.07 in the polynomial 63 Figure 4-27: Plo