HAYNES® 556™ alloy - Haynes International, Inc.

More documents

Recommendations

Info

$P:\P25065\H-# Literature\H-2082 - Haynes International, Inc.$

Typical Tensile Properties (continued)Hot-Rolled and Solution Annealed Plate, 0.250 to 0.500 Inches (6.4 to 12.7 mm) Thick*TestTemperature°F °CUltimateTensileStrengthKsi MPaYield Strengthat 0.2% OffsetKsi MPaElongation in2 in. (50.8 mm)%RoomRoom116.4 80554.6 37551.41000 5401200 65090.3 62583.1 57530.6 21030.6 21060.357.41400 76068.5 47029.3 20052.61600 8701800 98049.3 34030.7 21027.9 19018.5 13069.183.92000 109516.1 1108.7 6095.2* Based upon 56 TestsASME VESSEL CODE ALLOWABLE STRESSESHAYNES ® 556 alloy is approved forASME Vessel Code Section I constructionto 1200°F (650°C) under Code Case No.2010 and Section VIII Division 1 constructionto 1650°F (900°C). Allowable stressesare reprinted here by permission of theASME.NOTE (1)Due to the relatively low yield strength of this material, thesehigher stress values were established at temperatures wherethe short time tensile properties govern to permit the use ofthese alloys where slightly greater deformation is acceptable.These higher stress values exceed 67%, but do not exceed90% of the yield strength at temperature. Use of these stressmay result in dimensional changes due to permanent strain.These stress values are not recommended for flanges ofgasketed joints or other applications where slight amounts ofdistortion can cause leakage or malfunction.HAYNES ® 556 TM alloyASME Vessel Code Allowable StressesMetalMaximum Allowable Stress ValuesTemperaturesNot ExceedingStandardNote (1)°F °C Ksi (MPa) Ksi (MPa)100 37 25.0 (172) 25.0 (172)200 93 25.0 (172) 25.0 (172)300 149 23.1 (159) 24.5 (168)400 204 21.3 (146) 23.7 (163)500 260 20.1 (138) 23.1 (159)600 315 19.3 (133) 22.8 (157)650 343 19.0 (131) 22.7 (156)700 371 18.7 (129) 22.5 (155)750 398 18.5 (127) 22.4 (154)800 426 18.2 (125) 22.3 (153)850 454 18.0 (124) 22.2 (153)900 482 17.8 (122) 22.1 (152)950 510 17.6 (121) 21.8 (150)1000 537 17.4 (120) 21.6 (148)1050 565 17.2 (118) 21.4 (147)1100 593 17.1 (118) 20.8 (143)1150 621 16.9 (116) 16.9 (116)1200 648 13.6 (93) 13.6 (93)1250 676 10.9 (75) 10.9 (75)1300 7048.8 (60) 8.8 (60)1350 7327.0 (48) 7.0 (48)1400 7605.6 (38) 5.6 (38)1450 7874.5 (31) 4.5 (31)1500 8153.6 (25) 3.6 (25)1550 8432.8 (19) 2.8 (19)1600 8712.2 (15) 2.2 (15)1650 8981.8 (12) 1.8 (12)18
TYPICAL CREEP AND STRESS-RUPTURE PROPERTIESSolution Annealed Sheet, Plate and BarTemperature°F °C1200 6501300 7051400 7601500 8151600 8701700 9251800 980Creep,Percent0.51.0Rupture0.51.0Rupture0.51.0Rupture0.51.0Rupture0.51.0Rupture0.51.0Rupture0.51.0RuptureAverage Initial Stress, Ksi (MPa)*to Produce Specified Creep and Rupture10 Hours 100 Hours 1,000 Hours 10,000 Hours44.0 (305) 32.0 (220) 24.0 (165) - -49.0 (340) 35.0 (240) 25.5 (175) 18.5 (130)- - 53.0 (365) 38.0 (260) 27.5 (190)29.0 (200) 21.0 (145) 15.0 (105) - -33.0 (230) 24.0 (165) 17.5 (120) 12.5 (86)52.0 (360) 37.0 (255) 26.0 (180) 17.0 (115)19.0 (130) 13.5 (93) 9.4 (65) - -22.0 (150) 16.0 (110) 11.5 (79) 8.5 (59)35.0 (240) 25.0 (170) 17.5 (120) 11.9 (82)13.0 (90) 9.0 (62) 6.5 (45) - -15.0 (105) 11.0 (76) 8.2 (57) 6.0 (41)25.0 (170) 17.0 (115) 11.8 (81) 7.6 (52)8.9 (61) 6.4 (44) 4.6 (32) - -10.0 (69) 7.5 (52) 5.5 (38) 4.1 (28)17.0 (115) 11.5 (79) 7.5 (52) 4.9 (34)6.2 (43) 4.5 (31) 3.2 (22) - -7.2 (50) 5.0 (34) 3.5 (24) 2.5 (17)12.0 (83) 7.6 (52) 4.8 (33) 3.0 (21)4.4 (30) 3.0 (21) 2.0 (14) - -5.0 (34) 3.4 (23) 2.3 (16) 1.6 (11)7.5 (52) 4.8 (33) 3.0 (21) 1.9 (13)TYPICAL IMPACT PROPERTIESMaterialalloy 800Halloy 600556 alloy188 alloyS alloyalloy 625X alloyV-Notch Impact Strength 1Room Temperatureft.-lb.Joules239 2 324 2180 244177 2 240 2143 194140 19081 11054 731Average of 4 or more tests2Samples did not break19HAYNES ® 556 TM alloy
Page 1 and 2: HIGH-TEMPERATURE ALLOYSHAYNES ® 55
Page 3 and 4: PRINCIPAL FEATURESHigh Strength and
Page 5 and 6: Field Experience - Municipal Waste
Page 7 and 8: Comparative 1700°F (925°C) Mix Ga
Page 9 and 10: OXIDATION RESISTANCEHAYNES ® 556 a
Page 11 and 12: APPLICATIONSThis high-temperature f
Page 13 and 14: OTHER HIGH TEMPERATURE ENVIRONMENTS
Page 15 and 16: Typical Physical Properties (contin
Page 17: TYPICAL TENSILE PROPERTIESCold-Roll
Page 21 and 22: Thermal Stability (continued)Room-T
Page 23 and 24: Fabrication Characteristics (contin
Page 25 and 26: Manual Gas Tungsten Arc WeldingV-or
Page 27 and 28: MACHININGHAYNES ® 556 alloy is sim

HAYNES® 556™ alloy - Haynes International, Inc.

Create successful ePaper yourself

Delete template?

Save as template?