Heat Resistant Alloy 800 / 800H Stainless Steel Plate Thickness 0.6 - 20.0mm in Stock
Products | 416 stainless steel sheet |
Thickness | 0.3 - 4.0mm |
Width | 1000mm 1219mm 1500mm or as request |
Standard | ASTM A240/240M-18 |
Brand | TISCO BAOSTEEL POSCO |
Service | Cutting , bending , surface finishing |
Other Grade | 201 202 304 304L 304H 309S 310S 316L 316Ti 317L 321 347 410 420 430 431 444,2205 2507 904L 254SMO 253MA N08020 C276 625 600 800 825 monel 400 500.etc |
Standard Size | 1000*2000mm 1219*2438mm 1500*6000mm |
Material Description of Alloy 800/800H
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.
Alloy 800HT has excellent creep strength at temperatures above 1290°F (700°C). If the application involves frequent temperature excursions under 1290°F (700°C) or parts of are permanently exposed to a temperature below 1290°F (700°C), Alloy 800H should be utilized. The high temperature resistance of Alloy 800HT is comparable to Alloy 800H. It also remains stable in long term high temperature service.
Chemical Analysis of Alloy 800 / 800H
Weight % (all values are maximum unless a range is otherwise indicated)
Element | 800H | 800HT |
---|---|---|
Nickel | 30.0 min.-35.0 max. | 30.0 min.-35.0 max. |
Chromium | 19.0 min.-23.0 max. | 19.0 min.-23.0 max. |
Iron | 39.5 | 39.5 |
Carbon | 0.05 min.-0.10 max. | 0.06 min.-0.10 max. |
Manganese | 1.50 | 1.50 |
Phosphorus | 0.045 | 0.045 |
Sulfur | 0.015 | 0.015 |
Silicon | 1.0 | 1.0 |
Aluminum | 0.15 min.-0.60 max. | 0.25 min.-0.60 max. |
Titanium | 0.15 min.-0.60 max. | 0.25 min.-0.60 max. |
Aluminum & Titanium | 0.30 min.-1.20 max. | 0.85 min.-1.20 max. |
Corrosion Resistance of 800 / 800H Alloy
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 hightemperature strength, corrosive environments to which these grades are exposed normally involve high temperature reactions such as oxidation and carburization.
Application of 800/800H alloy
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