X20CrMoWV12-1 Forged tube
Description X20CrMoWV12-1 Forgings, X20CrMoWV12-1 Tube, Inventory, On stock Plate X20CrMoWV12-1 Stocklist Properties Technical specifications - DIN EN 10269.
| Product parameters | |
| Material Category:: | Turbine Blade Steel |
| Material Technical Standards:: | DIN EN 10302 / EN 10269 / DIN EN 10095 |
| Place of Origin: | China |
| Terms of Price:: | Ex works, CIF, CFR |
| Stocklist & Inventory Available:: | Diameter 20 ~ 200mm |
| Melting Process Route:: | EAF + VD + LF / BEF + ESR |
| Certification:: | MTR, COC, Co, Invoice, Packing list |
| Mode of transportation:: | Sea shipment, Air cargo or international courier |
| Third-party Inspection Service:: | TUV, SGS, CCIC |
| Heat Treatment Practice:: | Hardened 1030 ℃, water or air cooled, tempered 650 ℃ min, 2 times tempered |
| Surface Condition:: | Rough turned, shot blasted, centre ground |
| Ultrasonic Test Standard:: | EN 10308, MIL-STD-AMS 2154 CLA |
| Customization Service:: | Welcome |
| Standard Export Packing Way:: | Wooden box, pallet, or per buyer's requirements |
| Unit price: | USD4.92 per kg or Negotiable per order size |
Description
Introduction:
X20CrMoWV12-1 is a hardenable stainless steel designed for use at temperatures of up to 1200F. X20CrMoWV12-1 has good resistance to scaling and oxidation. Through heat treatment, high mechanical properties can be developed. X20CrMoWV12-1 is used in applications such as compressors or steam turbines and also in aircraft parts, valves, high temperature bolting, and other mechanical parts used in high temperature circumstances.
X20CrMoWV12-1 is a hardenable stainless steel designed for use at temperatures of up to 1200F. X20CrMoWV12-1 has good resistance to scaling and oxidation. Through heat treatment, high mechanical properties can be developed. X20CrMoWV12-1 is used in applications such as compressors or steam turbines and also in aircraft parts, valves, high temperature bolting, and other mechanical parts used in high temperature circumstances.
Applications:
Aircraft components.
High pressure corrosive fabricated parts such as valves.
Shafts, Fasteners, Fittings and gears.
Aircraft components.
High pressure corrosive fabricated parts such as valves.
Shafts, Fasteners, Fittings and gears.
Technical Standard: DIN EN 10302
All Grades Comparison
| DIN | ASTM | AISI | UNS | JIS | Other |
|---|---|---|---|---|---|
| 1.4935 X20CrMoWV12-1 |
Grade 616 | 422 | S42200 | SUH 616 | 10705BU AMS 5655 |
| C | Si | Mn | P | S | Cr | Ni | Mo | Other |
|---|---|---|---|---|---|---|---|---|
| 0.20 ～ 0.25 | ≤ 0.50 | 0.50 ～ 1.00 | ≤ 0.025 | ≤ 0.025 | 11.0 ～ 12.5 | 0.50 ～ 1.00 | 0.90 ～ 1.25 | W 0.90 ～ 1.25 V 0.20 ～ 0.30 |
Mechanical Properties
| Condition of heat treatment | Tensile Rm(MPa) | Yield Rp0.2(MPa) | Elongation A (%) |
Reduction in cross section on fracture Z (%) |
Impact AKV/AKU(J) | Brinell Hardness(HBW) |
|---|---|---|---|---|---|---|
| annealed | - | - | - | - | - | ≤ 248 |
| Hardened 1022℃ ~ 1050℃ air or oil cooled, ≥620℃ X 2H, tempered | ≥ 965 | ≥ 760 | ≥ 13.0 | ≥ 30.0 | ≥ 11 | 302 ~ 352 |
| Hardened 1022℃ ~ 1050℃ air or oil cooled, ≥677℃ X 2H, tempered | ≥ 825 | ≥ 585 | ≥ 17.0 | ≥ 35.0 | ≥ 20 | 241 ~ 285 |
