HAYNES® HR-120® alloy
Principal Features
HAYNES® HR-120® alloy (UNS N08120) alloy is a solid-solution-strengthened heat-resistant alloy that provides excellent strength at elevated temperature combined with very good resistance to carburizing and sulfidizing environments. Its oxidation resistance is comparable to other widely used Fe-Ni-Cr materials, such as alloys 330 and 800H, but its strength at temperatures up to 2000ºF (1095ºC) is significantly higher, even in comparison to Ni-Cr alloys. The alloy can be readily formed hot or cold, and is commonly welded using HAYNES® 556® filler wire.
Applications
Applications include those which require high strength combined with good resistance to carburizing and sulfidizing environments such as the following:
• Bar Frame Heat Treating Baskets • Radiant Tubes
• Wire Mesh Furnace Belts and Basket Liners • Cast Link Belt Pins
• Muffles, Retorts • Recuperators
• Heat Treating Fixtures • Fluidized Bed Components
• Waste Incinerators
HR-120® alloy heat treat furnace basket and mesh liner. This 3/8 inch diameter rod frame basket has replaced 1/2 inch diameter baskets in similar design in 330 and 600 alloys. This reduction in rod diameter is equivalent to a 43% weight reduction.
Heat Treatment
HAYNES® HR-120® alloy is furnished in the solution annealed condition, unless otherwise specified. Depending on the product form, the alloy is solution annealed at a temperature ranging from 2150 to 2250 °F (1175 to 1230 °C) and rapidly cooled. For more information on heat-treatment, please click here.
*Please contact our technical support team if you have technical questions about this alloy.
Nominal Composition
Weight %
Iron
33 Balance
Nickel
37
Cobalt
3 max.
Chromium
25
Molybdenum
1 max.
Tungsten
0.5 max.
Niobium*
0.7
Manganese
0.7
Silicon
0.6
Nitrogen
0.2
Aluminum
0.1
Carbon
0.05
Boron
0.004
Titanium
0.2 max.
Weight % | |
Iron | 33 Balance |
Nickel | 37 |
Cobalt | 3 max. |
Chromium | 25 |
Molybdenum | 1 max. |
Tungsten | 0.5 max. |
Niobium* | 0.7 |
Manganese | 0.7 |
Silicon | 0.6 |
Nitrogen | 0.2 |
Aluminum | 0.1 |
Carbon | 0.05 |
Boron | 0.004 |
Titanium | 0.2 max. |
*Also known as Columbium
Creep-rupture Data
HR-120® Plate, Solution-annealed
Temperature | Creep | Approximate Initial Stress to Produce Specified Creep in: | ||||||||
10h | 100h | 1,000h | 10,000h | |||||||
°F | °C | % | ksi | MPa | ksi | MPa | ksi | MPa | ksi | MPa |
1200 | 649 | 0.5 | – | – | – | – | 23.0 | 159 | – | – |
1 | – | – | – | – | 26.5 | 183 | – | – | ||
R | 68 | 469 | 54 | 372 | 35 | 241 | 23.0 | 159 | ||
1300 | 704 | 0.5 | – | – | 20.3 | 140 | 14.0 | 97 | – | – |
1 | – | – | 23.5 | 162 | 15.9 | 110 | – | – | ||
R | 45 | 310 | 32 | 221 | 21.7 | 150 | 15.0 | 103 | ||
1400 | 760 | 0.5 | 19.3 | 133 | 14.5 | 100 | 10.8 | 74 | 8.0 | 55 |
1 | 22.2 | 153 | 15.8 | 109 | 12.3 | 85 | 9.5 | 66 | ||
R | 30 | 207 | 21.5 | 148 | 15.3 | 105 | 11.0 | 76 | ||
1500 | 816 | 0.5 | 13.8 | 95 | 10.5 | 72 | 8 | 55 | 5.7 | 39 |
1 | 15.3 | 105 | 11.4 | 79 | 8.4 | 58 | 6.2 | 43 | ||
R | 21.8 | 150 | 15.3 | 105 | 11.0 | 76 | 7.8 | 54 | ||
1600 | 871 | 0.5 | 10.5 | 72 | 8.4 | 58 | 6.1 | 42 | 4.1 | 28 |
1 | 11.4 | 79 | 9.1 | 63 | 6.5 | 45 | 4.4 | 30 | ||
R | 14.0 | 97 | 10.8 | 74 | 7.7 | 53 | 5.0 | 34 | ||
1700 | 927 | 0.5 | 8.0 | 55 | 6.0 | 41 | 3.9 | 27 | 2.4 | 17 |
1 | 8.5 | 59 | 6.7 | 46 | 4.4 | 30 | 2.7 | 19 | ||
R | 11.2 | 77 | 7.8 | 54 | 5.1 | 35 | 3.1 | 21 | ||
1800 | 982 | 0.5 | 5.8 | 40 | 3.7 | 26 | 2.1 | 14 | 1.1 | 7.6 |
1 | 6.2 | 43 | 4.4 | 30 | 2.5 | 17 | 1.3 | 9.0 | ||
R | 7.9 | 54 | 5.1 | 35 | 3.1 | 21 | 1.8 | 12 | ||
1900 | 1038 | 0.5 | 4.0 | 28 | 2.3 | 16 | 1.1 | 7.6 | – | – |
1 | 4.7 | 32 | 2.5 | 17 | 1.2 | 8.3 | 0.60 | 4.1 | ||
R | 5.5 | 38 | 3.3 | 23 | 1.8 | 12 | 0.97 | 6.7 | ||
2000 | 1093 | 0.5 | 1.8 | 12 | 0.90 | 6.2 | – | – | – | – |
1 | – | – | 1.1 | 7.6 | – | – | – | – | ||
R | – | – | 2.0 | 14 | 1.1 | 7.6 | 0.60 | 4.1 | ||
2100 | 1149 | 0.5 | 0.60 | 4.1 | 0.30 | 2.1 | – | – | – | – |
1 | – | – | 0.42 | 2.9 | – | – | – | – | ||
R | – | – | 1.2 | 8.3 | 0.60 | 4.1 | 0.30 | 2.1 |
HR-120® Sheet, Solution-annealed, Limited Data
Temperature | Creep | Approximate Initial Stress to Produce Specified Creep in: | ||||
100 h | 1,000 h | |||||
°F | °C | % | ksi | MPa | ksi | MPa |
1400 | 760 | 1 | 14.6 | 101 | 10.4 | 72 |
R | 21.6 | 149 | 14.4 | 99 | ||
1500 | 816 | 1 | 11.5 | 79 | 8.8 | 61 |
R | 14.9 | 103 | 10.4 | 72 | ||
1600 | 871 | 1 | 8.2 | 57 | 6.6 | 46 |
R | 10.3 | 71 | 7.2 | 50 | ||
1700 | 927 | 1 | 6.0 | 41 | 4.2 | 29 |
R | 7.0 | 48 | 4.3 | 30 | ||
1800 | 982 | 1 | 3.3 | 23 | 2.4 | 17 |
R | 4.4 | 30 | 2.7 | 19 |
Tensile Data
Average Tensile Data, Solution Heat-treated Sheet
Test Temperature | Ultimate Tensile Strength | 0.2% Offset Yield Strength | Elongation | |||
°F | °C | ksi | MPa | ksi | MPa | % |
RT | RT | 104.2 | 718 | 47.5 | 328 | 46.3 |
1000 | 538 | 80.0 | 552 | 28.3 | 195 | 53.6 |
1200 | 649 | 73.5 | 507 | 27.0 | 186 | 55.0 |
1400 | 760 | 57.4 | 396 | 26.4 | 182 | 48.0 |
1600 | 871 | 32.6 | 225 | 24.7 | 170 | 67.2 |
1800 | 982 | 17.1 | 118 | 13.2 | 91 | 74.7 |
2000 | 1093 | 8.8 | 61 | 6.4 | 44 | 56.1 |
RT= Room Temperature
Average Tensile Data, Solution Heat-treated Plate
Test Temperature | Ultimate Tensile Strength | 0.2% Offset Yield Strength | Elongation | Reduction of Area | |||
°F | °C | ksi | MPa | ksi | MPa | % | % |
RT | RT | 104.3 | 719 | 46.8 | 322 | 49.8 | 63.3 |
1000 | 538 | 80.4 | 554 | 26.9 | 186 | 58.7 | 57.7 |
1200 | 649 | 72.9 | 503 | 26.0 | 179 | 55.4 | 59.6 |
1400 | 760 | 59.8 | 412 | 25.6 | 177 | 51.6 | 65.6 |
1600 | 871 | 35.8 | 247 | 26.4 | 182 | 71.1 | 72.3 |
1800 | 892 | 18.6 | 128 | 14.5 | 100 | 83.6 | 77.4 |
2000 | 1093 | 9.6 | 66 | 7.4 | 51 | 84.1 | 69.4 |
RT= Room Temperature
Comparative Yield Strengths
Temperature | 0.2% Yield Strength, ksi | ||||
°F | HR-120® | 800H | RA330 | 600 | 601 |
70 | 46.8 | 35 | 42 | 41 | 35 |
1000 | 26.9 | – | – | – | – |
1200 | 26.0 | 16.9 | 21.5 | 30 | 25.4 |
1400 | 25.6 | 18.5 | 18.8 | 26 | 26.8 |
1600 | 26.4 | 18.5 | 15.9 | 11 | 19.2 |
1800 | 14.5 | 8.1 | 9 | 6 | 10.9 |
2000 | 7.4 | 3.3 | – | 3.1 est | 5.1 |
Hardness and Grain Size
Solution-annealed Room Temperature Hardness
Form | Hardness, HRBW | Typical ASTM Grain Size |
Sheet | 88 | 3.5 – 5 |
Plate | 87 | 0 – 5 |
Bar | 84 | 0 – 4.5 |
HRBW = Hardness Rockwell “B”, Tungsten Indentor.
Thermal Stability
Condition | Ultimate Tensile Strength | 0.2% Offset Yield Strength | Elongation | Reduction of Area | ||
ksi | MPa | ksi | MPa | % | % | |
Solution Heat-treated | 108.0 | 745 | 49.0 | 338 | 48.5 | 69 |
+ 1200°F/8,000 h | 109.2 | 753 | 52.5 | 362 | 26.2 | 32.8 |
+ 1200°F/20,000 h | 112.4 | 775 | 53.5 | 369 | 24.2 | 34 |
+ 1200°F/30,000 h | 112.7 | 777 | 52.3 | 361 | 24.6 | 32.7 |
+ 1200°F/50,000 h | 113.0 | 779 | 53.1 | 366 | 23.2 | 32.5 |
+1400°F/8,000 h | 101.8 | 702 | 47.9 | 330 | 18.2 | 17.6 |
+1400°F/20,000 h | 101.2 | 698 | 43.3 | 299 | 18.0 | 17.2 |
+1400°F/30,000 h | 101.5 | 700 | 44.8 | 309 | 19.7 | 18.4 |
+1400°F/50,000 h | 99.8 | 688 | 44.9 | 310 | 14.8* | 10.8 |
+ 1600°F/8,000 h | 101.0 | 696 | 44.7 | 308 | 22.6 | 22.6 |
+ 1600°F/20,000 h | 96.9 | 668 | 40.9 | 282 | 19.4 | 17.9 |
+ 1600°F/30,000 h | 96.7 | 667 | 40.3 | 278 | 22.0 | 19.5 |
+ 1600°F/50,000 h | 94.3 | 650 | 39.8 | 274 | 20.1 | 18.2 |
*AGL, which tends to be lower; Other data are 4D Elong.
Oxidation Resistance
Metallographic Technique used for Evaluating Environmental Tests
Static Oxidation
HAYNES® HR-120® alloy exhibits good resistance to oxidizing environments and can be used at temperatures up to 2100°F (1150°C). The following are comparative static oxidation test results at 1600°F (870°C), 1800°F (980°C), 2000°F (1090°C), and 2100°F (1150°C) for 1008 hours.
Alloy | 1600°F (870°C) | 1800°F (980°C) | 2000°F (1090°C) | 2100°F (1150°C) | ||||||||||||
Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | |||||||||
mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | |
HR‐120® | 0.1 | 0.00 | 0.9 | 0.02 | 0.4 | 0.01 | 2.1 | 0.05 | 1.0 | 0.03 | 4.4 | 0.11 | 7.9 | 0.20 | 10.1 | 0.26 |
253MA | 0.2 | 0.01 | 0.9 | 0.02 | 1.3 | 0.03 | 3.0 | 0.08 | 0.7 | 0.02 | 8.2 | 0.21 | 8.7 | 0.22 | 16.5 | 0.42 |
800HT | 0.1 | 0.00 | 1.0 | 0.03 | 0.5 | 0.01 | 4.1 | 0.10 | 7.6 | 0.19 | 11.6 | 0.29 | 11.0 | 0.28 | 15.0 | 0.38 |
601 | – | – | – | – | 0.4 | 0.01 | 1.7 | 0.04 | 1.3 | 0.03 | 3.8 | 0.10 | 2.8 | 0.07 | 6.5 | 0.17 |
600 | – | – | – | – | 0.3 | 0.01 | 2.4 | 0.06 | 0.9 | 0.02 | 3.3 | 0.08 | 2.8 | 0.07 | 4.8 | 0.12 |
RA330 | – | – | – | – | 0.3 | 0.01 | 3.0 | 0.08 | 0.8 | 0.02 | 6.7 | 0.17 | – | – | – | – |
304SS | – | – | – | – | 5.5 | 0.14 | 8.1 | 0.21 | NA | NA | >19.6 | >0.498 | NA | NA | >19.5 | >0.498 |
RA85H | – | – | – | – | 0.5 | 0.01 | 8.3 | 0.21 | 3.0 | 0.08 | 26.0 | 0.66 | – | – | – | – |
Dynamic Oxidation
Burner rig oxidation tests were conducted by exposing samples of 3/8” x 2.5” x thickness (9mm x 64 mm x thickness), in a rotating holder to the products of combustion of 2 parts No. 1 and 1 part No. 2 fuel burned at a ratio of air to fuel of about 50:1. Gas velocity was about 0.3 mach. Samples were automatically removed from the gas stream every 30 minutes and fan-cooled to near ambient temperature and then reinserted into the flame tunnel.
<thcolspan=”5″>1800°F/1000-h/2000-Cycles
Alloy | Metal Loss | Average Metal Affected | ||
mils | µm | mils | µm | |
556® | 3.9 | 99 | 6.8 | 173 |
HR-120® | 6.3 | 160 | 8.4 | 213 |
RA 330 | 6.5 | 165 | 9.5 | 241 |
800H/800HT | 8.9 | 226 | 13.7 | 348 |
310 SS | 16.0 | 406 | 18.3 | 465 |
253MA | 16.6 | 422 | 17.8 | 452 |
Long-term Oxidation
Amount of metal affected for high‐temperature plate (0.25”) alloys exposed for 360 days (8,640 hours) in flowing air. Cycled once per month.
Alloy | Exposure Duration | 1600°F | 1800°F | 2000°F | 2100°F | |||||||||||||
Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | Metal Loss | Average Metal Affected | |||||||||||
h | number of cycles | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | |
214® | 8640 | 12 | 0.1 | 0.00 | 0.2 | 0.01 | 0.0 | 0.00 | 0.0 | 0.00 | 0.0 | 0.00 | 0.0 | 0.00 | 0.0 | 0.00 | 0.0 | 0.00 |
230® | 8640 | 12 | 0.2 | 0.01 | 1.4 | 0.04 | 0.1 | 0.00 | 2.5 | 0.06 | 3.4 | 0.09 | 11.0 | 0.28 | 28.5 | 0.72 | 34.4 | 0.87 |
HR-120® | 8640 | 12 | 0.3 | 0.01 | 1.6 | 0.04 | 0.5 | 0.01 | 3.3 | 0.08 | 18.1 | 0.46 | 23.2 | 0.59 | 33.6 | 0.85 | 44.0 | 1.12 |
556® | 8640 | 12 | 0.3 | 0.01 | 1.9 | 0.05 | 0.5 | 0.01 | 6.2 | 0.16 | 15.0 | 0.38 | 24.1 | 0.61 | – | – | – | – |
617 | 8640 | 12 | 0.3 | 0.01 | 1.6 | 0.04 | – | – | – | – | – | – | – | – | – | – | – | – |
800HT | 8640 | 12 | 0.4 | 0.01 | 2.9 | 0.07 | – | – | – | – | – | – | – | – | – | – | – | – |
Water Vapor Testing
Alloy |
1008 hours at 1600ºF Cycled 1x/week in air+10% H2O |
1008 hours at 1600ºF Cycled 1x/week in air+20% H2O |
6 months at 1400ºF Cycled 1x/week in air+10% H2O |
|||||||||
Meal Loss | Average Metal Affected | Meal Loss | Average Metal Affected | Meal Loss | Average Metal Affected | |||||||
mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | mils | mm | |
HR-120® | 0.09 | 0.002 | 0.68 | 0.017 | 0.04 | 0.001 | 0.29 | 0.007 | 0.10 | 0.003 | 0.50 | 0.013 |
253MA | 0.66 | 0.017 | 1.59 | 0.040 | 0.08 | 0.002 | 0.68 | 0.017 | – | – | – | – |
347SS | 0.86 | 0.022 | 1.48 | 0.038 | 0.18 | 0.005 | 0.88 | 0.022 | 0.46 | 0.012 | 1.26 | 0.032 |
800HT | – | – | – | – | – | – | – | – | 0.12 | 0.003 | 0.82 | 0.021 |
Carburization Resistance
HAYNES® HR-120® alloy has good resistance to carburization. Results from 1800°F (982°C) carburization testing show HR-120® alloy to be better than stainless steels. Both pack and gaseous carburization test results are presented.
Metallographic Technique used for Evaluating Environmental Tests
Comparative Sulfidation Resistance
Independent outside testing laboratories have also verified the superior performance of HR-120® alloy in sulfidizing environments. Petten Establishment in the Netherlands found that HR-120® alloy performed significantly better than alloys 800H, 347SS and 321SS at 1290°F (700°C) in hydrogen plus 7 percent carbon monoxide plus 1.5 percent water vapor plus 0.6 percent hydrogen sulfide. The HR-120® alloy was found to be magnitudes better than the other alloys.
Hot Corrosion Comparison
Hot corrosion is an accelerated oxidation or sulfidation attack due to a molten salt deposit. This form of corrosion is seen in gas turbines as well as in other industrial environments. The hot corrosion resistance of the HR-120® alloy was evaluated by performing laboratory burner rig testing. The burner rig used No. 2 fuel oil with a sulfur content of about 1 weight percent and air to generate the test environment. The air-to-fuel ratio was maintained at 35 to 1. The test was run at 1650°F (900°C) for 500 hours with a two-minute cooling cycle to less than 400°F (205°C) every hour. During testing a synthetic sea salt solution (ASTM D1141-52) was continuously injected into the combustion zone. The following photographs show the appearance of the specimens after testing. Specimens of 253 MA, RA 85H, RA 330, and 800H alloys were either severely corroded or partially destroyed. On the other hand, the HR-120® alloy specimen still looks extremely good, showing little attack.
Hot corrosion test specimens after exposure at 1650°F (900°C) for 500 hours
using 50 ppm sea salt injection and 1 percent sulfur fuel.
Burner Rig Hot Corrosion Data for Alloys at 1650°F (900°C) exposed for 500 hours
Alloy | Time | % S in Fuel | Salt | Metal Loss | Average Metal Affected | ||
h | ppm | mils | mm | mils | mm | ||
HR-120® | 500 | 1 | 50 | 0.9 | 0.02 | 5.2 | 0.13 |
RA330 | 500 | 1 | 50 | 1.4 | 0.04 | 5.8 | 0.15 |
800H | 500 | 1 | 50 | 1.0 | 0.03 | 10.3 | 0.26 |
253MA | 500 | 1 | 50 | >25 | >0.64 | >25 | >0.64 |
RA85H | 500 | 1 | 50 | >25 | >0.64 | >25 | >0.64 |
Physical Properties
Physical Property | British Units | Metric Units | ||
Density | RT |
0.291 lb/in.3 |
RT |
8.07 g/cm.3 |
Melting Range | 2375°F | - | 1300°C | - |
Electrical Resistivity | RT | 41.4 µohm.in | RT | 105.2 µohm.cm |
200°F | 42.4 µohm.in | 100°C | 107.8 µohm.cm | |
400°F | 44.4 µohm.in | 200°C | 112.5 µohm.cm | |
600°F | 45.4 µohm.in | 300°C | 114.9 µohm.cm | |
800°F | 46.3 µohm.in | 400°C | 116.7 µohm.cm | |
1000°F | 47.3 µohm.in | 500°C | 119.3 µohm.cm | |
1200°F | 48.2 µohm.in | 600°C | 121.4 µohm.cm | |
1400°F | 48.8 µohm.in | 700°C | 123.1 µohm.cm | |
1600°F | 49.4 µohm.in | 800°C | 124.5 µohm.cm | |
1800°F | 50.0 µohm.in | 900°C | 125.7 µohm.cm | |
2000°F | 50.3 µohm.in | 1000°C | 126.6 µohm.cm | |
2200°F | 50.7 µohm.in | 1100°C | 127.8 µohm.cm | |
- | - | 1200°C | 128.7 µohm.cm | |
Thermal Diffusivity | RT |
4.7 x 10-3 in2/s |
RT |
30.4 x 10-3 cm2/s |
200°F |
5.0 x 10-3 in2/s |
100°C |
32.4 x 10-3 cm2/s |
|
400°F |
5.4 x 10-3 in2/s |
200°C |
34.8 x 10-3 cm2/s |
|
600°F |
5.8 x 10-3 in2/s |
300°C |
37.2 x 10-3 cm2/s |
|
800°F |
6.3 x 10-3 in2/s |
400°C |
39.7 x 10-3 cm2/s |
|
1000°F |
6.7 x 10-3 in2/s |
500°C |
42.2 x 10-3 cm2/s |
|
1200°F |
7.1 x 10-3 in2/s |
600°C |
44.7 x 10-3 cm2/s |
|
1400°F |
7.4 x 10-3 in2/s |
700°C |
46.9 x 10-3 cm2/s |
|
1600°F |
7.5 x 10-3 in2/s |
800°C |
48.1 x 10-3 cm2/s |
|
1800°F |
7.8 x 10-3 in2/s |
900°C |
48.8 x 10-3 cm2/s |
|
2000°F |
78.2 x 10-3 in2/s |
1000°C |
50.7 x 10-3 cm2/s |
|
2200°F |
8.6 x 10-3 in2/s |
1100°C |
52.9 x 10-3 cm2/s |
|
- | - | 1200°C |
54.5 x 10-3 cm2/s |
|
Thermal Conductivity | RT |
78 Btu.in/h.ft2.°F |
RT | 11.4 W/m-°C |
200°F |
84 Btu.in/h.ft2.°F |
100°C | 12.7 W/m-°C | |
400°F |
96 Btu.in/h.ft2.°F |
200°C | 14.1 W/m-°C | |
600°F |
108 Btu.in/h.ft2.°F |
300°C | 15.4 W/m-°C | |
800°F |
121 Btu.in/h.ft2.°F |
400°C | 17.1 W/m-°C | |
1000°F |
134 Btu.in/h.ft2.°F |
500°C | 18.7 W/m-°C | |
1200°F |
150 Btu.in/h.ft2.°F |
600°C | 21.0 W/m-°C | |
1400°F |
168 Btu.in/h.ft2.°F |
700°C | 23.3 W/m-°C | |
1600°F |
180 Btu.in/h.ft2.°F |
800°C | 24.9 W/m-°C | |
1800°F |
191 Btu.in/h.ft2.°F |
900°C | 26.2 W/m-°C | |
2000°F |
205 Btu.in/h.ft2.°F |
1000°C | 28.0 W/m-°C | |
2200°F |
216 Btu.in/h.ft2.°F |
1100°C | 29.6 W/m-°C | |
Specific Heat | RT | 0.112 Btu/lb.°F | RT | 467 J/kg-°C |
200°F | 0.116 Btu/lb.°F | 100°C | 483 J/kg-°C | |
400°F | 0.121 Btu/lb.°F | 200°C | 500 J/kg-°C | |
600°F | 0.125 Btu/lb.°F | 300°C | 522 J/kg-°C | |
800°F | 0.130 Btu/lb.°F | 400°C | 531 J/kg-°C | |
1000°F | 0.135 Btu/lb.°F | 500°C | 558 J/kg-°C | |
1200°F | 0.144 Btu/lb.°F | 600°C | 607 J/kg-°C | |
1400°F | 0.152 Btu/lb.°F | 700°C | 647 J/kg-°C | |
1600°F | 0.159 Btu/lb.°F | 800°C | 655 J/kg-°C | |
1800°F | 0.164 Btu/lb.°F | 900°C | 660 J/kg-°C | |
2000°F | 0.167 Btu/lb.°F | 1000°C | 663 J/kg-°C | |
2200°F | 0.169 Btu/lb.°F | 1100°C | 667 J/kg-°C | |
- | - | 1200°C | 671 J/kg-°C | |
Mean Coefficient of Thermal Expansion | 78-200°F | 7.95 µin/in-°F | 25-100°C | 14.3 µm/m-°C |
78-400°F | 8.29 µin/in-°F | 25-200°C | 14.9 µm/m-°C | |
78-600°F | 8.56 µin/in-°F | 25-300°C | 15.3 µm/m-°C | |
78-800°F | 8.80 µin/in-°F | 25-400°C | 15.8 µm/m-°C | |
78-1000°F | 8.98 µin/in-°F | 25-500°C | 16.1 µm/m-°C | |
78-1200°F | 9.24 µin/in-°F | 25-600°C | 16.4 µm/m-°C | |
78-1400°F | 9.52 µin/in-°F | 25-700°C | 16.9 µm/m-°C | |
78-1600°F | 9.72 µin/in-°F | 25-800°C | 17.3 µm/m-°C | |
78-1800°F | 9.87 µin/in-°F | 25-900°C | 17.6 µm/m-°C | |
- | - | 25-1000°C | 17.8 µm/m-°C | |
Dynamic Modulus of Elasticity | RT |
28.7 x 106 psi |
RT | 198 GPa |
200°F |
28.2 x 106 psi |
100°C | 194 GPa | |
400°F |
27.0 x 106 psi |
200°C | 187 GPa | |
600°F |
25.9 x 106 psi |
300°C | 179 GPa | |
800°F |
24.7 x 106 psi |
400°C | 172 GPa | |
1000°F |
23.7 x 106 psi |
500°C | 165 GPa | |
1200°F |
22.5 x 106 psi |
600°C | 158 GPa | |
1400°F |
21.4 x 106 psi |
700°C | 151 GPa | |
1600°F |
20.2 x 106 psi |
800°C | 143 GPa | |
1800°F |
18.9 x 106 psi |
900°C | 136 GPa | |
2000°F |
17.3 x 106 psi |
1000°C | 129 GPa | |
Dynamic Shear Modulus | RT |
11.0 x 106 psi |
RT | 76 GPa |
200°F |
10.7 x 106 psi |
100°C | 74 GPa | |
400°F |
10.3 x 106 psi |
200°C | 71 GPa | |
600°F |
9.8 x 106 psi |
300°C | 68 GPa | |
800°F |
9.3 x 106 psi |
400°C | 65 GPa | |
1000°F |
8.9 x 106 psi |
500°C | 62 GPa | |
1200°F |
8.4 x 106 psi |
600°C | 59 GPa | |
1400°F |
8.0 x 106 psi |
700°C | 56 GPa | |
1600°F |
7.5 x 106 psi |
800°C | 53 GPa | |
1800°F |
7.0 x 106 psi |
900°C | 50 GPa | |
2000°F |
6.3 x 106 psi |
1000°C | 47 GPa | |
Poisson’s Ratio | RT | 0.31 | RT | 0.31 |
200°F | 0.31 | 100°C | 0.31 | |
400°F | 0.32 | 200°C | 0.32 | |
600°F | 0.32 | 300°C | 0.32 | |
800°F | 0.33 | 400°C | 0.32 | |
1000°F | 0.33 | 500°C | 0.33 | |
1200°F | 0.34 | 600°C | 0.33 | |
1400°F | 0.34 | 700°C | 0.34 | |
1600°F | 0.35 | 800°C | 0.34 | |
1800°F | 0.36 | 900°C | 0.35 | |
2000°F | 0.37 | 1000°C | 0.36 |
Welding
HAYNES® HR-120® alloy is readily welded by Gas Tungsten Arc Welding (GTAW), Gas Metal Arc Welding (GMAW), Shielded Metal Arc Welding (SMAW), and resistance welding techniques. Submerged Arc Welding (SAW) is not recommended as this process is characterized by high heat input to the base metal and slow cooling of the weld. These factors can increase weld restraint and promote cracking.
Base Metal Preparation
The welding surface and adjacent regions should be thoroughly cleaned with an appropriate solvent prior to any welding operation. All greases, oils, cutting oils, crayon marks, machining solutions, corrosion products, paint, scale, dye penetrant solutions, and other foreign matter should be completely removed. It is preferable, but not necessary, that the alloy be in the solution- annealed condition when welded.
Filler Metal Selection
HAYNES® 556® filler metal (AMS 5831, AWS A5.9 ER3556) and MULTIMET® (AMS 5794) coated electrodes are recommended for joining HR-120® alloy. When dissimilar base metals are to be joined, such as HR-120® alloy to a stainless steel, HAYNES® 556® filler metal and MULTIMET® coated electrodes are again recommended. Please click here or the Haynes Welding SmartGuide for more information.
Preheating, Interpass Temperatures, and Postweld Heat Treatment
Preheat is not required. Preheat is generally specified as room temperature (typical shop conditions). Interpass temperature should be maintained below 200°F (93°C). Auxiliary cooling methods may be used between weld passes, as needed, providing that such methods do not introduce contaminants. Postweld heat-treatment is not generally required for HR-120® alloy. For further information, please click here.
Nominal Welding Parameters
Details for GTAW, GMAW and SMAW welding are given here. Nominal welding parameters are provided as a guide for performing typical operations and are based upon welding conditions used in our laboratories.
Tensile Properties of All Weld Metal (AWM)
Test Temperature | 0.2% Yield Strength | Ultimate Tensile Strength | Elongation | |||
°F | °C | ksi | MPa | ksi | MPa | % |
RT | RT | 77.2 | 530 | 115.4 | 795 | 37 |
1200 | 650 | 53.3 | 380 | 81.0 | 560 | 39 |
1400 | 760 | 49.5 | 340 | 66.3 | 455 | 26 |
1600 | 870 | 36.8 | 255 | 40.2 | 270 | 34 |
1800 | 980 | 23.6 | 165 | 24.0 | 165 | 30 |
RT=Room Temperature
Transverse Tensile Tests, HR-120® Base Metal Welded with Haynes 556® filler
Temperature | 0.5 Inch Plate | 0.125 Inch Sheet | |||
UTS | UTS | ||||
°F | °C | ksi | MPa | psi | MPa |
RT | RT | 106 | 731 | 104 | 717 |
200 | 93 | 97 | 666 | 97 | 665 |
300 | 149 | 91 | 625 | 92 | 632 |
400 | 204 | 87 | 600 | 89 | 612 |
500 | 260 | 86 | 595 | 78 | 540 |
600 | 316 | 85 | 589 | 83 | 571 |
700 | 371 | 84 | 576 | 79 | 547 |
800 | 427 | 84 | 581 | 83 | 570 |
900 | 482 | 82 | 568 | 82 | 564 |
1000 | 538 | 79 | 544 | 80 | 549 |
1100 | 593 | 75 | 516 | 77 | 530 |
1200 | 649 | 71 | 490 | 74 | 507 |
1300 | 704 | 68 | 471 | 66 | 455 |
1400 | 760 | 60 | 413 | 55 | 382 |
1500 | 816 | 47 | 327 | 45 | 312 |
1600 | 871 | 35 | 241 | 33 | 226 |
1700 | 927 | 27 | 184 | 26 | 176 |
1800 | 982 | 20 | 136 | 25 | 174 |
1900 | 1038 | 15 | 102 | 16 | 110 |
2000 | 1093 | 12 | 84 | 9 | 64 |
Transverse Tensile Tests, HR-120® Plate Welded with Haynes 556® filler
Temperature | 1 Inch Plate | 0.5 Inch Plate | |||
UTS | UTS | ||||
°F | °C | ksi | MPa | ksi | MPa |
RT | RT | 110 | 762 | 106 | 731 |
200 | 93 | 102 | 703 | 96 | 661 |
300 | 149 | 96 | 665 | 91 | 629 |
400 | 204 | 93 | 641 | 88 | 609 |
500 | 260 | 90 | 622 | 86 | 590 |
600 | 316 | 89 | 611 | 84 | 582 |
700 | 371 | 89 | 612 | 82 | 564 |
800 | 427 | 89 | 611 | 82 | 563 |
900 | 482 | 87 | 602 | 82 | 568 |
1000 | 538 | 78 | 538 | 78 | 534 |
1100 | 593 | 79 | 545 | 75 | 519 |
1200 | 649 | 75 | 515 | 72 | 497 |
1300 | 704 | 72 | 497 | 68 | 471 |
1400 | 760 | 64 | 439 | 60 | 412 |
1500 | 816 | 53 | 362 | 48 | 329 |
1600 | 871 | 40 | 279 | 36 | 247 |
1700 | 927 | 31 | 215 | 27 | 188 |
1800 | 982 | 24 | 166 | 20 | 141 |
1900 | 1038 | 18 | 123 | 15 | 106 |
2000 | 1093 | 12 | 84 | 11 | 74 |
HR-120® Plate and Transverse Weld Room Temperature Charpy Impact Tests
0.5″ Plate, Welded with Haynes 556®
Temperature | 1 Inch Plate | 0.5 Inch Plate | |||
UTS | UTS | ||||
°F | °C | ksi | MPa | ksi | MPa |
RT | RT | 110 | 762 | 106 | 731 |
200 | 93 | 102 | 703 | 96 | 661 |
300 | 149 | 96 | 665 | 91 | 629 |
400 | 204 | 93 | 641 | 88 | 609 |
500 | 260 | 90 | 622 | 86 | 590 |
600 | 316 | 89 | 611 | 84 | 582 |
700 | 371 | 89 | 612 | 82 | 564 |
800 | 427 | 89 | 611 | 82 | 563 |
900 | 482 | 87 | 602 | 82 | 568 |
1000 | 538 | 78 | 538 | 78 | 534 |
1100 | 593 | 79 | 545 | 75 | 519 |
1200 | 649 | 75 | 515 | 72 | 497 |
1300 | 704 | 72 | 497 | 68 | 471 |
1400 | 760 | 64 | 439 | 60 | 412 |
1500 | 816 | 53 | 362 | 48 | 329 |
1600 | 871 | 40 | 279 | 36 | 247 |
1700 | 927 | 31 | 215 | 27 | 188 |
1800 | 982 | 24 | 166 | 20 | 141 |
1900 | 1038 | 18 | 123 | 15 | 106 |
2000 | 1093 | 12 | 84 | 11 | 74 |
Restrained 1/2 inch thick HR-120® plates have been successfully joined using 556® weld wire and MULTIMET® coated electrodes. The results below indicate an absence of hot cracking and microfissuring related weldability problems under the test conditions.
Welding Process | Welding Product | Hot Cracking | 2T Radius Guided Bend Test | |
– | – | – | Face | Side |
GTAW | 556® Filler Metal | None | Pass | Pass |
GMAW | 556® Filler Metal | None | Pass | Pass |
SMAW | MULTIMET® Electrodes | None | Pass | Pass |
Room Temperature Tensile Strength of Transverse Welded Specimens
Welding Process | Welding Product | Tensile Strength | Fracture Location | |
– | – | ksi | MPa | – |
GTAW | 556® Filler Metal | 111.0 | 765 | HR-120® Base Metal |
GMAW | 556® Filler Metal | 109.4 | 755 | HR-120® Base Metal |
SMAW | MULTIMET® Electrodes | 109.7 | 755 | HR-120® Base Metal |
Machining and Grinding
HAYNES® HR-120® alloy can be readily machined using conventional techniques. Generally, the same practices are employed as those used with the 300 series austenitic stainless steels. Some minor adjustments in the machining parameters may be required to obtain optimum results. High speed steel tools are found to be satisfactory, although machining speeds can be substantially increased by using carbide cutting tools. As a general statement, grinding operations with HAYNES® HR-120® alloy are considered equivalent to those of the 300 series stainless steels. As with other alloys, grinding is recommended where a close tolerance is required. Basic “Do’s” and “Don’ts” that should be considered during machining are:
Do:
1. Use machine tools that are rigid and overpowered, where possible.
2. Insure work piece and tools are held rigid. In addition, minimize tool overhang.
3. Make sure tools are always sharp. Change to sharpened tools at regular intervals rather than out of necessity. Remember, cutting edges, particularly throw-away inserts, are expendable. Don’t try to prove how long they can last. Don’t trade dollars in machine times for pennies in tool cost.
4. Use positive rake angle tools for most machining operations. Negative rake angle tools can be considered for intermittent cuts and heavy stock removal.
5. Use heavy, constant, feeds to maintain positive cutting action. If feed slows and the tool dwells in the cut, work hardening occurs, tool life deteriorates and close tolerance is impossible.
6. Avoid conditions such as chatter and glazing. This can cause work hardening of the surface, making subsequent machining difficult.
7. Flood the work with premium-quality sulfochlorinated water soluble oil or water-base chemical emulsion oils with extreme pressure additives. Dilute per the recommendations of the manufacturer.
8. Use heavy-duty sulfochlorinated oil for drilling and tapping. Special proprietary tapping oils can also be used.
9. Use air jet directed on the tool when dry cutting. This can provide substantial increase in tool life.
Don’t:
1. Do not make intermittent cuts, if possible. This tends to work harden the surface, making subsequent cuts more difficult.
Detailed Machining Information
Turning, Boring and Facing
The table below represents a typical range of values for normal turning operations. The depth of cut (particularly for roughing operations) is quite large with relatively low feed rates. These parameters are equipment and component dependent. The larger depths of cuts and higher speeds are recommended only when using heavy, overpowered equipment on large rigid components.
Conditions | Roughing | Finishing |
Depth of Cut | 0.125-0.250 in. | 0.020-0.040 in. |
Feed Rate | 0.008-0.010 ipr | 0.006-0.008 ipr |
Speed-HSS | 30-50 sfpm | 40-60 sfpm |
Speed-Carbide | 100-170 sfpm | 140-180 sfpm |
Drilling
Standard high-speed steel bits are normally used. For drill bits larger than 3/8″, thinning the web may reduce thrust and aid chip control. The following are suggested speed and feed rates for various diameter drills.
Diameter | Speed | Feed Rate |
1/8 in | 250 RPM (max) | 0.002 inch/rev. |
1/4 in | 250 RPM (max) | 0.003 inch/rev. |
1/2 in | 250 RPM | 0.005 inch/rev. |
1 in | 150 RPM | 0.011 inch/rev. |
1-1/2 in | 100 RPM | 0.013 inch/rev. |
2 in | 75 RPM | 0.016 inch/rev. |
For other diameters (above 1/2 inch diameter) the spindle speed may be calculated from the following: RPM = 150/Diameter (inches). This results in a cutting speed of about 40 sfpm. For drill diameters smaller than 1/2 inch, speed rates substantially below 40 sfpm are required.
Reaming
Standard fluted reamers of high-speed steel are generally used. Speeds should be about 20-25 sfpm for diameters above 1/2 inch. For small diameter reamers (less than 1/2 inch diameter) cutting speeds should be reduced substantially. Feed rates will range from 0.002 to 0.006 inch/revolution depending upon diameter. If carbide tipped reamers are used, the speed can be increased to 70 sfpm for reamers above 1/2 inch diameter. If chatter occurs, reduce speed.
Tapping
HAYNES HR-120 alloy is tapped using the same tooling and conditions as used with type 316 stainless steel. High speed steel taps work well. Cutting speed can be up to 20 sfpm for taps above 1/2 inch diameter. For small diameter taps (less than 1/2 inch diameter) cutting speeds should be reduced substantially.
Thread engagement can be reduced because of the high strength of this alloy. Generally, thread engagement of 60 to 75 percent is considered acceptable. Thread engagement is considered a design parameter and therefore should be left to the design engineer. As a general statement, 75 percent thread engagement is common for low strength materials, but only leads to increased tool wear and possible breakage in high strength alloys. It does not increase the holding strength in these alloys.
Milling
High speed steel cutters, with good impact strength, are recommended due to the interrupted nature of the cutting action. A cutting speed of 30 to 40 sfpm with feed rates of 0.002 to 0.005 inch/tooth is generally recommended. If carbide cutters are employed, speeds of 60 to 80 sfpm are possible.
Applications
Comparative Data
Mechanical Property* | HR-120® | 214® | 230® | 556® | X | 600 | 601 | RA330 | 253MA | 800H | 304 SS | 310 SS | 316 SS | |
Annealing Temperature | °F | 2250 | 2000 | 2250 | 2150 | 2150 | 2050 | 2100 | 2050 | 2000 | 2100 | 2000 | 2150 | 2000 |
Typical ASTM Grain Size | – | 3 – 6 | 3 – 5 | 5 – 6 | 5 – 6 | 5 – 6 | 2 – 4 | 2 – 4 | 4 – 6 | 3 – 6 | 2 – 4 | 2 – 5 | 3 – 4 | 5 – 7 |
Ultimate Tensile Strength, ksi | 70°F | 104.3 | 138.9 | 125.4 | 116.4 | 107.5 | 96.0 | 102.0 | 85.0 | 104.0 | 82.0 | 85.0 | 82.7 | 103.9 |
1200°F | 72.9 | 114.9 | 97.7 | 83.1 | 78.5 | 65.0 | 74.0 | 55.7 | 64.6 | 59.0 | 43.0 | 54.0 | 60.5 | |
1400°F | 59.8 | 79.4 | 87.7 | 68.5 | 66.6 | 38.0 | 43.0 | 34.0 | 49.8 | 39.0 | 2736.0 | 35.1 | 39.0 | |
1600°F | 35.8 | 66.4 | 63.1 | 49.3 | 49.6 | 20.0 | 22.0 | 18.7 | 30.8 | 21.0 | 17.5 | 19.1 | 24.6 | |
1800°F | 18.6 | 16.7 | 35.2 | 30.7 | 31.1 | 11.0 | 13.0 | 10.7 | – | 11.0 | **7.4 | 10.5 | 14.0 | |
2000°F | 9.6 | 9.0 | 19.5 | 16.1 | 16.5 | (5.1) | 6.5 | – | – | 5.0 | – | 4.3 | 7.1 | |
2200°F | – | 5.0 | 9.4 | – | – | – | **5.2 | – | – | – | – | – | – | |
0.2% Yield Strength, ksi | 70°F | 46.8 | 82.2 | 57.4 | 54.6 | 49.4 | 41.0 | 35.0 | 42.0 | 50.8 | 35.0 | 27.9 | 35.1 | 36.7 |
1200°F | 26.0 | 75.9 | 39.5 | 30.6 | 30.3 | 30.0 | 25.4 | 21.5 | 24.1 | 16.9 | 11.0 | 20.7 | 20.5 | |
1400°F | 25.6 | 73.6 | 42.5 | 29.3 | 31.0 | 26.0 | 26.8 | 18.8 | 22.4 | 18.5 | 10.5 | 19.3 | 17.9 | |
1600°F | 26.4 | 50.4 | 37.3 | 27.9 | 28.4 | 11.0 | 19.2 | 15.9 | 18.1 | 18.5 | 7.4 | 12.2 | 10.6 | |
1800°F | 14.5 | 8.4 | 21.1 | 18.5 | 17.9 | 6.0 | 10.9 | 9.0 | – | 8.1 | – | 6.4 | – | |
2000°F | 7.4 | 4.2 | 10.8 | 8.7 | 9.1 | (3.1) | 5.1 | – | – | 3.3 | – | 3.1 | – | |
2200°F | – | 1.4 | 4.3 | – | – | – | **2.0 | – | – | – | – | – | – | |
Tensile Elongation, % | 70°F | 50 | 43 | 50 | 51 | 53 | 45 | 50 | 45 | 51 | 49 | 61 | 54 | 59 |
1200°F | 55 | 33 | 55 | 57 | 64 | 49 | 46 | 51 | 44 | 38 | 37 | 21 | 40 | |
1400°F | 52 | 23 | 53 | 53 | 58 | 70 | 72 | 65 | 44 | 43 | 31 | 19 | 49 | |
1600°F | 71 | 34 | 65 | 69 | 75 | 80 | 90 | 69 | – | 87 | 35 | 28 | 59 | |
1800°F | 84 | 86 | 83 | 84 | 95 | 115 | 100 | 74 | – | 100 | **38 | 24 | 41 | |
2000°F | 84 | 89 | 83 | 95 | 98 | (120) | 120 | – | – | 108 | – | – | 85 | |
2200°F | – | 92 | 109 | – | – | – | 121 | – | – | – | – | – | – | |
Stress to Rupture in 1,000 Hours, ksi | 1200°F | 38.0 | – | 42.5 | 38.0 | 34.0 | 20.0 | 28.0 | – | 23.0 | 23.8 | 14.1 | 17.0 | 20.5 |
1400°F | 17.0 | 25.0 | 20.0 | 17.5 | 15.0 | 8.1 | 9.8 | 7.0 | 9.2 | 9.8 | 7.4 | 7.4 | 8.8 | |
1600°F | 8.0 | 8.9 | 9.5 | 7.5 | 6.0 | 3.5 | 4.4 | 3.1 | 4.4 | 4.8 | 3.0 | 3.3 | 3.4 | |
1800°F | 3.5 | 1.8 | 3.0 | 3.0 | 2.4 | 1.8 | 2.2 | 1.3 | 1.9 | 1.9 | 1.2 | 1.4 | 1.3 | |
2000°F | 0.8 | 0.9 | **1.0 | – | **0.8 | (0.9) | 1.0 | 0.7 | 1.0 | – | – | – | – |
( ) Estimated
*Manufacturer’s laboratory or published data
**Limited data
Physical Property* | HR-120® | 214® | 230® | 556® | X | 600 | 601 | RA330 | 253MA | 800H | 304 SS | 310 SS | 316 SS | |
Density, lb/in3 |
0.291 | 0.291 | 0.324 | 0.297 | 0.297 | 0.304 | 0.291 | 0.289 | 0.282 | 0.287 | 0.278 | 0.285 | 0.287 | |
Incipient Melting Point | °F | 2375 | 2475 | 2375 | 2425 | 2300 | 2470 | 2375 | 2450 | 2500 | 2475 | 2250 | 2550 | 2500 |
Electrical Resistivity, μ ohm-in | 70°F | 41.4 | 53.5 | 49.2 | 37.5 | 45.2 | 40.6 | 46.9 | 29.9 | 33.1 | 38.9 | 28.7 | 38.2 | 29.4 |
400°F | 44.4 | 53.9 | 49.8 | 40.5 | 46.7 | 41.5 | 48.2 | 43.0 | 40.6 | 43.0 | 34.6 | 41.7 | 34.5 | |
800°F | 46.3 | 54.3 | 50.7 | 43.5 | 48.4 | 43.0 | 49.2 | 45.6 | 48.8 | 46.1 | 40.6 | 45.7 | 39.3 | |
1200°F | 48.2 | 53.5 | 51.6 | 45.7 | 49.5 | – | 49.5 | 47.8 | 54.3 | – | 45.7 | 48.4 | 43.7 | |
1600°F | 49.4 | 49.6 | 50.3 | 17.3 | 49.8 | – | 50.2 | 49.1 | 56.3 | – | 47.2 | 50.8 | – | |
2000°F | 50.3 | 47.6 | (48.4) | 48.6 | 49.7 | – | 51.1 | – | (57.5) | – | – | – | – | |
Thermal Conductivity, Btu-in/ft2-hr °F |
70°F | 78 | 83 | 62 | 77 | 63 | 103 | 78 | 86 | 101 | 80 | 99 | 91 | 90 |
400°F | 96 | 99 | 87 | 107 | 83 | 121 | 100 | 108 | 121 | 103 | 116 | 112 | 108 | |
800°F | 120 | 132 | 118 | 135 | 121 | 145 | 126 | 134 | 140 | 127 | 141 | 145 | 132 | |
1200°F | 150 | 175 | 148 | 160 | 152 | 172 | 153 | 162 | 156 | 152 | 167 | 182 | 152 | |
1600°F | 180 | 215 | 179 | 185 | 182 | 200 | 178 | 198 | 184 | 181 | 192 | 213 | 172 | |
2000°F | 205 | 234 | (210) | 210 | – | (230) | 203 | – | – | – | – | – | – | |
Mean Coefficient of Thermal Expansion, μ in/in-°F (R to Temp.) | 400°F | 7.9 | 7.4 | 7.2 | 8.2 | 7.9 | 7.7 | 8.0 | 8.6 | 9.3 | 8.8 | 9.1 | 8.9 | 9.1 |
800°F | 8.8 | 7.9 | 7.6 | 8.6 | 8.2 | 8.1 | 8.3 | 9.1 | 9.8 | 9.2 | 9.6 | 9.2 | 9.8 | |
1200°F | 9.2 | 8.6 | 8.1 | 9.0 | 8.6 | 8.6 | 8.9 | 9.6 | 10.1 | 9.6 | 10.2 | 9.7 | 10.3 | |
1400°F | 9.5 | 9.0 | 8.3 | 9.2 | 8.8 | 8.9 | 9.2 | 9.7 | 10.3 | 9.9 | 10.7 | 10.0 | 10.4 | |
1600°F | 9.7 | 9.6 | 8.6 | 9.4 | 9.0 | 9.1 | 9.5 | 9.8 | 10.5 | 10.2 | 10.8 | 10.4 | 10.5 | |
1800°F | 9.9 | 10.2 | 8.9 | 9.5 | 9.2 | 9.3 | 9.8 | 10.0 | 10.8 | (10.5) | 11.0 | 40.7 | 10.7 | |
2000°F | – | 11.1 | (9.2) | 9.6 | (9.4) | (9.5) | 10.2 | (10.2) | (11.1) | – | 11.4 | 11.0 | – | |
Modulus of Elasticity, psi x 106 |
70°F | 28.7 | 31.6 | 30.6 | 29.7 | 29.8 | 31.1 | 30.0 | 28.5 | 29.0 | 28.4 | 27.9 | 29.0 | 28.5 |
400°F | 27.0 | 29.6 | 29.3 | 28.2 | 28.6 | 29.7 | 28.5 | 26.9 | 26.8 | 26.6 | 26.6 | 26.9 | 26.9 | |
800°F | 24.7 | 27.4 | 27.3 | 25.6 | 26.7 | 27.8 | 26.6 | 24.9 | 24.4 | 24.4 | 24.1 | 24.3 | 24.2 | |
1200°F | 22.5 | 25.3 | 25.3 | 23.1 | 24.7 | 25.5 | 24.1 | 22.4 | 21.7 | 22.3 | 21.1 | 21.8 | 21.5 | |
1400°F | 21.4 | 23.9 | 24.1 | 21.8 | 23.3 | 24.3 | 22.5 | 21.0 | 20.2 | 21.1 | 19.4 | 20.5 | 20.0 | |
1600°F | 20.2 | 22.3 | 23.1 | 20.9 | 22.2 | 22.8 | 20.5 | 19.5 | – | 20.0 | – | 19.2 | – | |
1800°F | 18.9 | 20.2 | 21.9 | 20.1 | 20.4 | 21.0 | 18.4 | 18.0 | 17.6 | 18.7 | – | – | – | |
2000°F | 17.3 | 19.0 | – | – | – | – | 16.2 | – | – | 17.2 | – | – | – |
( ) Estimated
*Manufacturer’s labroatory or published data
Specifications and Codes
Specifications
HAYNES® HR-120® alloy (N08120) | |
Sheet, Plate & Strip | AMS 5916SB 409/B 409P= 45 |
Billet, Rod & Bar | SB 408/B 408B 472P= 45 |
Coated Electrodes | – |
Bare Welding Rods & Wire | – |
Seamless Pipe & Tube | SB 407/B 407SB 163/B 163P= 45 |
Welded Pipe & Tube | SB 514/B 514SB 515/B 515P= 45 |
Fittings | SB 366/B 366P= 45 |
Forgings | SB 564/B 564P= 45 |
DIN | No. 2.4854NiFe33Cr25Co |
Others | – |
Codes
HAYNES® HR-120® alloy (N08120) | |||
ASME | Section l | – | |
Section lll | Class 1 | – | |
Class 2 | – | ||
Class 3 | – | ||
Section lV | HF-300.2 | – | |
Section Vlll | Div. 1 |
1800°F (982°C)1,2 |
|
Div. 2 | – | ||
Section Xll | – | ||
B16.5 | – | ||
B16.34 | – | ||
B31.1 | – | ||
B31.3 | – | ||
MMPDS | 6.3.10 |
1Plate, Sheet, Bar, Forgings, fittings, welded pipe/tube, seamless pipe/tube
2Properties up to 1650ºF (899ºC) are found in the latest ASME BPV Code, and from 1650ºF – 1800ºF (899ºC – 982ºC) in ASME Code Case 2672
Disclaimer
Haynes International makes all reasonable efforts to ensure the accuracy and correctness of the data displayed on this site but makes no representations or warranties as to the data’s accuracy, correctness or reliability. All data are for general information only and not for providing design advice. Alloy properties disclosed here are based on work conducted principally by Haynes International, Inc. and occasionally supplemented by information from the open literature and, as such, are indicative only of the results of such tests and should not be considered guaranteed maximums or minimums. It is the responsibility of the user to test specific alloys under actual service conditions to determine their suitability for a particular purpose.
For specific concentrations of elements present in a particular product and a discussion of the potential health affects thereof, refer to the Safety Data Sheets supplied by Haynes International, Inc. All trademarks are owned by Haynes International, Inc., unless otherwise indicated.