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Description
Inconel 600 is face-centered cubic lattice structure for use at temperature up to 1425°C (2600°F).The Nickel-Chromium alloy is characterized by good corrosion resistance to the reduction, oxidation, Nitric and other media,good stress corrosion cracking resistance,good corrosion resistance of the dry chlorine and chlorine hydride,good mechanical property when below zero, room temperature and high temperature,good anti-creep rupture strength. with the higher chemical stability in water, organic acids and salt solution Usage:so it is widely used in chemical industry, precision machinery, marine engineering, and used as important resistor and thermocouple alloy.
A Nickel-Chromium alloy being precipitation hardenable and having high creep-rupture strength at high temperatures to about 700 C (1290F). It has higher strength than Inconel X-750 and better mechanical properties at lower temperatures than Nimonic 90 and Inconel X-750.
| Chemical Composition | Specifications | Designations | Key Features | Typical Applications |
|---|---|---|---|---|
ElementMin %Max %C–0.08Mn–0.35Si–0.35P–0.015S–0.015Cr17.0021.00Ni50.0055.00Mo2.803.30Nb/Cb4.755.50Ti0.651.15Al0.200.80Co–1.00Ta–0.05B–0.006Cu–0.30Pb–0.0005Bi–0.00003Se–0.0003Febal | AMS 5662 AMS 5663 AMS 5832 AMS 5962 ASTM B637 GE B5OTF14/15 GE B14H89 ISO 15156-3 (NACE MR 0175) | W.NR 2.4668 UNS N07718 AWS 013 | Good creep rupture strength at high temperatures Higher strength than Inconel X-750 Better mechanical properties at lower temperatures than Nimonic 90 & Inconel X-750 Age hardenable High temperature dynamic applications | Gas Turbines Rocket Motors Space Craft Nuclear Reactors Pumps |
| Density | 8.19g/cm3 | 0.296 lb/in3 |
| Melting Point | 1336 C | 2437 F |
| Coefficient of Expansion | 13.0 μm/m C (20 – 100 C) | 7.2 x 10 (-6) in/in F (70 – 212 F) |
| Modulus of Rigidity | 77.2 kN/mm2 | 11197 ksi |
| Modulus of Elasticity | 204.9 kN/mm2 | 29719 ksi |
| Heat Treatment of Finished Parts | |||||
|---|---|---|---|---|---|
| Condition as supplied by Alloy Wire | Type | Temperature | Time (Hr) | Cooling | |
| C | F | ||||
| No. 1 or Spring Temper | Anneal Age Harden Total Age | 980 720 620 | 1800 1330 1150 | 1 8 18 | Air Furnace Air |
| No. 1 or Spring Temper (for ISO 15156-3 / NACE MR 0175) | Anneal Age Harden | 1010 790 | 1850 1455 | 2 6 | Air Air |
| No. 1 Temper or Spring Temper | Age Harden Total Age | 720 620 | 1330 1150 | 8 18 | Furnace Air |
| Properties | ||||
|---|---|---|---|---|
| Condition | Approx. tensile strength | Approx. operating temperature | ||
| N/mm2 | ksi | C | F | |
| Annealed | 800 – 1000 | 116 – 145 | – | – |
| No 1 Temper | 1000 – 1200 | 145 – 175 | – | – |
| Spring Temper | 1300 – 1500 | 189 – 218 | – | – |
| No 1 Temper + Annealed + Aged | 1250 – 1450 | 181 – 210 | -200 to +550 | -330 to +1020 |
| No 1 Temper + Aged | 1520 – 1720 | 220 – 250 | Contact Alloy Wire Technical Dept | |
| Spring Temper + Annealed + Aged | 1250 – 1450 | 181 – 210 | -200 to +550 | -330 to +1020 |
| Spring Temper + Aged | 1700 – 1950 | 247 – 283 | Contact Alloy Wire Technical Dept | |
The above tensile strength ranges are typical. If you require different please ask.
