2.4668
2.4668 Chemical composition:
C | Mn | Si | P | S | Cu | B | Co | Mg | Cr | Ni | Mo | Ti | Al | Nb | Fe | |
Min | ≤ | 17 | 50 | 2.8 | 0.65 | 0.2 | 4.75 | Bal | ||||||||
Max | 0.08 | 0.35 | 0.015 | 0.35 | 0.015 | 0.3 | 0.006 | 1 | 0.1 | 21 | 55 | 3.3 | 1.15 | 0.8 | 5.5 |
2.4668 Physical properties:
Densityg/cm3 | 8.24 |
Melting point℃ | 1260-1336 |
2.4668 Mechanical properties:
Condition | Diameter | Tensile strength | Yield strength 0.2% offset | Elongation % | Hardness | ||
Min | Max | Min | Max | ||||
Cold working, solution annealing and aging | 0.5-3 | 150 | 120 | 140 | 40 | 30 | 40 |
Annealing and aging of thermal working solutions | 0.5-8 | 150 | 120 | 140 | 40 | 30 | 40 |
Annealing and aging of thermal working solutions | 8-10 | 150 | 120 | 140 | 40 | 30 | 40 |
2.4668 Alloy properties:
Corrosion resistance: HuaNickel 2.4668 alloy has excellent corrosion resistance to many media. These resistances are similar to those of other nickel-based alloys and are determined by their composition. In addition to being present in a strong oxidizing environment, nickel contributes to the corrosion resistance of many inorganic, organic and mixed acids and bases over a wide pH range. Nickel is also useful for preventing chloride stress corrosion cracking. Chromium gives the alloy the ability to withstand oxidizing media and sulfide attack. Molybdenum is widely recognized for its contribution to pitting resistance in many media.
High Temperature Strength: HuaNickel 2.4668 alloy retains high strength and good corrosion resistance in temperatures ranging from 700°C to 2500°F
2.4668 Uses of alloys:
It is widely used in aerospace, petrochemical, electric power and other fields, especially in the occasions that require high temperature, high pressure and corrosive environments.
2.4668 Process performance:
Welding Performance: HuaNickel 2.4668 is capable of welding using the Tigon Arc Welding (TIG) process using 2.4668 wire. The slow response of the 718 to age hardening allows the component to be welded and then aged hardened without any intermediate stress relief.
Heat treatment:
(1) Solution annealing at 1700-1850°F followed by rapid cooling (usually with water), plus precipitation hardening at 1325°F for 8 hours, furnace cooling to 1150°F, total aging time at 1150°F to 18 hours and then air cooling.
(2) Solution annealing at 1900-1950°F followed by rapid cooling (usually in water), plus precipitation hardening at 1400°F for 10 hours, air cooling to 1200°F and holding to a total aging time of 20 hours then air cooling.
Relevant standards:
rods, slats, wire rods and forgings – ASTM B 637, ASME SB 637, SAE AMS 5662, SAE AMS 5663, SAE AMS 5664,
SAE AMS 5832, SAE AMS 5914, SAE AMS 5962, ASME Code Case 1993, ASME Code Case 2206, ASME Code
Case 2222, AECMA PrEN 2404, AECMA PrEN 2405, AECMA PrEN 2952, AECMA PrEN 2961, AECMA PrEN 3219, AECMA PrEN 3666, ISO 9723, ISO 9724, ISO 9725, DIN 17752-17754。
Hot plates, cold plates, and strips – ASTM B 670, ASTM B 906, ASME SB 670, ASME SB 906, SAE AMS 5596, SAE AMS 5597, SAE AMS 5950, AECMA PrEN 2407, AECMA PrEN 2408, ISO 6208, DIN 17750
Conveyor pipes and tubes – SAE AMS 5589, SAE AMS 5590, ASME Code Case N-253, DIN 17751
Welding products – INCONEL Filler Metal 718 – AWS 5.14 / ERNiFeCr-2
other – ASME Code Case N-62, ASME Code Case N- 208, DIN 17744