Metallographic structure: The microstructure of this alloy in its standard heat treatment state is determined by γ Matrix, Ti (C, N), Nb (C, N), M23C6 carbides, and γ' [Ni3 (Al, Ti, Nb)] phase composition, γ' The content is approximately 14.5%, which is the main strengthening phase of the alloy.
Process treatment:
1. Annealing: 955-1010 ℃, water-cooled.
2. Annealing before welding of welded parts: 980 ℃, 1 hour.
3. Stress relief annealing of welded parts: 900 ℃, moisturizing for 2 hours.
4. Stress relief annealing: 885 ℃± 15 ℃, 24 hours, air-cooled
Element | Ni +Co | Cr | Nb | Ti | C | Mn | Si | Cu | Al | S | Iron |
Chemical Composition (%) | 70% Min | 14%- 17% | 0.7%- 1.2% | 2.25%- 2.75% | 0.08% max | 1% max | 0.5% max | 0.30% max | 0.4%-1.0% | 0.01% max | 5%-9% |
1. Aerospace Industry:
Inconel X-750 wire is commonly used in manufacturing components for aircraft engines, such as turbine blades, compressor blades, and jet pipes.
2. Nuclear Industry:
In the nuclear energy sector, Inconel X-750 wire is utilized for fabricating components for nuclear reactors, such as reactor pressure vessels and nuclear fuel cladding.
3. Chemical Industry:
Due to its excellent corrosion resistance, Inconel X-750 wire finds wide applications in chemical equipment such as chemical reactors and steam generators.
4. Medical Devices:
Inconel X-750 wire can also be used for manufacturing medical devices and equipment, such as implantable medical devices and surgical instruments.
AMS Number | Alloy | Type | UNS | Cross Ref. Spec | Misc./Shape | |
---|---|---|---|---|---|---|
AMS 5542 Custom Tube | Inconel X750 | Nickel | N07750 | - | Custom Tube | ![]() |
AMS 5542 Plate | Inconel X750 | Nickel | N07750 | - | Plate | ![]() |
AMS 5542 Sheet | Inconel X750 | Nickel | N07750 | - | Sheet | ![]() |
AMS 5542 Strip | Inconel X750 | Nickel | N07750 | - | Strip | ![]() |