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
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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
