Alloys 800H (UNS N08810) and 800HT (UNS N08811) are dual-certifiable Nickel-Iron-Chromium materials that resist oxidation, carburization and other high temperature corrosion. The chemical composition of the two alloys are identical to Alloy 800 (UNS N08800), with the exception of the higher level of carbon present in both grades — (0.05 – 0.10%) in alloy 800H, and (0.06 – 0.10%) in alloy 800HT. Alloy 800HT also has an addition of up 1.0% aluminum and titanium.
In addition to the chemistry restrictions, both alloys receive a high temperature annealing treatment that produces an average grain size of ASTM 5 or coarser. The restricted chemical compositions, combined with the high temperature anneal, assure these materials have greater creep and rupture strength when compared to Alloy 800.Alloy 800H has good creep- rupture properties at temperatures above 1100°F (600°C). It remains ductile during long term use at temperatures below 1290°F (700°C) due to a maximum titanium and aluminum content of 0.7%. Alloy 800 with a standard anneal is recommended for service below 1100°F (600°C). Alloy 800H resists reducing, oxidizing and nitriding atmospheres, as well as, atmospheres that alternate between reducing and oxidizing. The alloy remains stable in long term high temperature service.
Form |
Standard |
---|---|
Metal Type |
UNS N08800 / N08810 / N08811 |
Bar |
ASTM B408 |
Wire |
|
Sheet |
ASTM B409 |
Plate |
ASTM B409 |
Fitting |
ASTM B366 |
Forging |
ASTM B564 |
Weld Wire |
|
Weld Electrode |
|
Typical Dimension ranges <Other upon request> | |||
Form | Specification | Supply Form | Others |
Sheet | Thickness:0.40-4.75mm,General Width:1000,1219,1500mm | Whole Coil or piece of it | Cold Annealed,Surface 2B,2E |
Plate | Thickness:4.76-60mm,Width:1500,2000,2500mm,Length:3000,6000,8000,8500mm(Under 10mm plate can be coiled) | Whole Coil or piece of it | Single hot rolling,Solid solution annealed state,Surface 1D |
Belt | Thickness:0.10-3.0mm,Width:50-500mm | Whole Coil or Specified size | Cold Annealed,Surface 2B,2E |
Bar & Rod | Rolled barΦ5-45mm,Length≤1500mm | Polished Bar(circle,Square) | Solution annealing,descaling |
Forged barΦ26-245mm,Length≤4000mm | |||
Weld tube | Outer diameterΦ4.76-135mm,Wall Thickness0.25-4.00mm,Length:≤35000 mm | Base on your requirement | |
Seamless Tube | Outer diameterΦ3-114mm,Wall Thickness0.2-4.5mm | Base on your requirement | |
Wire | Outer diameterΦ0.1-13mm | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
Forged piece | discs,rings,squares,blocks,slabs | Base on your requirement | Steel, Alloy |
Flangs | All kinds of Flangs | Base on your requirement | Steel, Alloy |
Welding Material | Coil wire Φ0.025mm-1.6mm | Base on your requirement | Certificate of Origin:America, Sweden, Britain, Germany, Austria, Italy, France. |
Straight WireΦ1.6mm-4.0mm | |||
Welding rodΦ1.2mm-4.0mm | |||
Tube | Elbow, three links, four links, different diameter size | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
Explosive bonded laminate | Raw Sheet Thickness≥2mm | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
Petroleum Refining — steam/hydrocarbon reformers and hydrodealkylation units
Power Generation — steam super-heaters and high temperature heat exchangers in gas-cooled nuclear reactors, heat exchangers and piping systems in coal-fired power plants
Thermal Processing Fixtures — radiant tubes, muffles, retorts and fixtures for heat-treating furnaces
Limiting Chemical Compositions, %, for INCOLOY alloys 800, 800H, and 800HT
UNS designation | N08800 | N08810 | N08811 |
INCOLOY alloys | 800 | 800H | 800HT |
Nickel | 30.0-35.0 | 30.0-35.0 | 30.0-35.0 |
Chromium | 19.0-23.0 | 19.0-23.0 | 19.0-23.0 |
Iron | 39.5 min. | 39.5 min. | 39.5 min. |
Carbon | 0.10 max. | 0.05-0.10 | 0.06-0.10 |
Aluminum | 0.15-0.60 | 0.15-0.60 | 0.25-0.60 |
Titanium | 0.15-0.60 | 0.15-0.60 | 0.25-0.60 |
Aluminum + Titanium | 0.30-1.20 | 0.30-1.20 | 0.85-1.20 |
ASTM grain size | Not specified | 5 or coarser | 5 or coarser |
Note: These alloys can be specified to more restrictive compositions on a specific order basis.
Hardness and Tensile Properties of INCOLOY alloy 800 at High Temperatures
Condition |
Temperature | Hardness BHN | Tensile Strength | Yield Strength (0.2% Offset) | |||
°F | °C | ksi | MPa | ksi | MPa | ||
Annealeda | 80 | 25 | 138 | 85.5 | 590 | 36.2 | 250 |
800 | 425 | 120 | 74.1 | 511 | 24.9 | 172 | |
1000 | 540 | 119 | 73.7 | 508 | 25.8 | 178 | |
1200 | 650 | 110 | 58.7 | 405 | 25.5 | 176 | |
1300 | 705 | 97 | 46.3 | 319 | 25.3 | 174 | |
1400 | 760 | 66 | 34.5 | 238 | 21.6 | 149 | |
Hot-rolled | 80 | 25 | 198 | 96.4 | 665 | 64.6 | 445 |
800 | 425 | 170 | 84.5 | 583 | 52.0 | 359 | |
1000 | 540 | 161 | 84.0 | 579 | 52.4 | 361 | |
1200 | 650 | 145 | 65.3 | 450 | 48.3 | 333 | |
1300 | 705 | 120 | 53.5 | 369 | 46.8 | 323 | |
1400 | 760 | 91 | 44.5 | 307 | 41.2 | 284 |
INCOLOY alloy 800 has high mechanical strength over a broad temperature range. In general, alloy 800 is used for its strength characteristics at service temperatures up to about 1500°F (816°C). At those temperatures, equipment design is usually based on tensile properties. For applications that require high creep or rupture strength, INCOLOY alloys 800H and 800HT are used.
INCOLOY alloy 800 exhibits high tensile properties at room and elevated temperatures. Figures 2 and 3 show tensile properties at temperatures to 1500°F (815°C) of hot-rolled rod in the as-rolled and the annealed conditions. Tensile properties at room temperature and from 1200°F (650°C) to 1800°F (980°C) of as-extruded tubing are given in Table 6.
Table 6 - Tensile Properties of INCOLOY alloy 800 As-extruded Tubinga
Temperature | Tensile Strength | Yield Strength (0.2% Offset) |
Elong- ation, % |
Reduc- tion of Area, % |
|||
°F | °C | ksi | MPa | ksi | MPa | ||
85 | 30 | 76.0 | 524 | 26.6 | 183 | 60.0 | – |
1200 | 650 | 52.5 | 362 | 18.0 | 124 | 47.0 | 59.0 |
1400 | 760 | 30.3 | 209 | 15.7 | 108 | 85.0 | 73.0 |
1500 | 815 | 23.6 | 163 | 17.3 | 119 | 98.0 | 79.5 |
1600 | 870 | 16.0 | 110 | 13.5 | 93 | 109.5 | 92.5 |
1700 | 925 | 11.8 | 81 | 9.2 | 63 | 111.5 | 93.0 |
1800 | 980 | 8.9 | 61 | 7.2 | 50 | 131.5 | 94.0 |
Cold work substantially increases the tensile properties of the alloy. Properties of cold-drawn rod in the as-drawn condition are given in Table 7.
High-temperature hardness and tensile properties of annealed and hot-rolled material are shown in Table 8.
Table 7 - Tensile Properties of INCOLOY alloy 800 Cold-Drawn Roda
Temperature | Tensile Strength | Yield Strength (0.2% Offset) |
Elong- ation, % |
Reduc- tion of Area, % |
|||
°F | °C | ksi | MPa | ksi | MPa | ||
85 | 30 | 111.8 | 771 | 100.0 | 690 | 17.0 | 64.0 |
200 | 95 | 107.5 | 741 | 95.0 | 655 | 16.0 | 63.3 |
400 | 205 | 102.5 | 707 | 94.2 | 650 | 13.0 | 58.8 |
600 | 315 | 99.5 | 686 | 93.0 | 641 | 12.0 | 56.6 |
700 | 370 | 96.3 | 664 | 91.5 | 631 | 15.0 | 53.2 |
900 | 480 | 96.3 | 664 | 90.0 | 621 | 15.0 | 52.5 |
1000 | 540 | 93.0 | 641 | 86.3 | 595 | 16.5 | 54.0 |
1100 | 595 | 87.3 | 602 | 80.7 | 556 | 15.0 | 50.0 |
1200 | 650 | 78.5 | 541 | 66.8 | 461 | 19.5 | 44.5 |
1300 | 705 | 64.4 | 444 | 61.4 | 423 | 28.0 | 42.5 |
Condition |
Temperature | Hardness BHN | Tensile Strength | Yield Strength (0.2% Offset) | |||
°F | °C | ksi | MPa | ksi | MPa | ||
Annealeda | 80 | 25 | 138 | 85.5 | 590 | 36.2 | 250 |
800 | 425 | 120 | 74.1 | 511 | 24.9 | 172 | |
1000 | 540 | 119 | 73.7 | 508 | 25.8 | 178 | |
1200 | 650 | 110 | 58.7 | 405 | 25.5 | 176 | |
1300 | 705 | 97 | 46.3 | 319 | 25.3 | 174 | |
1400 | 760 | 66 | 34.5 | 238 | 21.6 | 149 | |
Hot-rolled | 80 | 25 | 198 | 96.4 | 665 | 64.6 | 445 |
800 | 425 | 170 | 84.5 | 583 | 52.0 | 359 | |
1000 | 540 | 161 | 84.0 | 579 | 52.4 | 361 | |
1200 | 650 | 145 | 65.3 | 450 | 48.3 | 333 | |
1300 | 705 | 120 | 53.5 | 369 | 46.8 | 323 | |
1400 | 760 | 91 | 44.5 | 307 | 41.2 | 284 |
The high nickel and chromium content of Alloys 800H and 800HT generally means they will have very similar aqueous corrosion resistance. The alloys have corrosion resistance that is comparable to 304 when used in nitric and organic acid service. The alloys should not be used in sulfuric acid service. They are subject to chromium carbide precipitation if in service for prolonged exposure in the 1000 – 1400°F (538 – 760°C) temperature range.
Since Alloys 800H and 800HT were developed primarily for high- temperature strength, corrosive environments to which these grades are exposed normally involve high temperature reactions such as oxidation and carburization.
Alloys 800H and 800HT can be easily welded and processed by standard shop fabrication practices. However, because of the high strength of the alloys, they require higher powered process equipment than standard austenitic stainless steels.
The hot-working temperature range for Alloy 800H and 800HT is
1740 – 2190°F (950 – 1200°C) if deformation is 5 percent or greater. If the degree of hot deformation is less than 5 percent a hot working temperature range between 1560 – 1920°F (850 – 1050°C) is recommended. If the hot working metal temperature falls below the minimum working temperature, the piece must be re-heated. The alloys should be water quenched or rapid air cooled through the temperature range of 1000 – 1400°F (540 – 760°C). Alloys 800H and 800HT require solution annealing after hot working to ensure optimal creep resistance and properties.
The alloys should be in the annealed condition prior to cold forming. Work hardening rates are higher than the austenitic stainless steels. This should be taken into account when selecting process equipment. An intermediate heat treatment may be necessary with a high degree of cold working or with more than 10 percent deformation.
Alloys 800H and 800HT can be readily welded by most standard processes including GTAW (TIG), PLASMA, GMAW (MIG/MAG), and SMAW (MMA). The
material should be in the solution-annealed condition, and free from grease, markings or scale. A post weld heat treatment is not necessary. Brushing with a stainless steel wire brush after welding will remove the heat tint and produce a surface area that does not require additional pickling.
Alloys 800H and 800HT should preferably be machined in the annealed condition. Since the alloys are prone to work–hardening, only low cutting speeds should be used and the cutting tool should be engaged at all times. Adequate cut depth is necessary to assure avoiding contact with the
previously formed work-hardened zone.
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