Superalloy-GH3536
-
-
Superalloy
Grade：
GH4080A（GH80A、4705YC1、4705FC1、4705BA1、NiCr20TiAl、Ni80TiAl、Nimonic80A、UNS N07080）Standards and Technical Conditions：
GB/T 14992 HB/Z140 DB MS4705Y R03 QHY JT-184 SQMS 25.05.02-01WS9-7009 WS9-7011 WS9-7095 WS9-7156 遼新6-0051
-
Product Characteristics
-
GJ4080A is a Ni-Cr formed nickel-based precipitation hardened superalloy. It has good creep resistance, corrosion resistance, oxidation resistance and fracture toughness at high temperatures of 650-850℃. It is widely used in aviation & aerospace, ships, thermal power, nuclear power and transportation. It is commonly used to manufacture various high temperature critical components, such as low pressure turbine working blades of aero engines, load bearing rings, bolts and sleeves, marine engine air valves, gas turbine blades, and steam turbine blades.
-
Industrial Application
-
The alloy's main products are flat bars and bars. The alloy has been used to make steam turbine blades, gas turbine fasteners, and steam turbine bolts. flat bars for steam turbine blades has undergone long-term production and use testing, showing good performance.
-
Company Product Applications
-
Large-size bars produced by the Company are used for gas turbine fasteners, small-size bars for steam turbine bolts, and flat bars for steam turbine blades.
Common Delivery Condition
Standard Heat Treatment Procedure
Excerpted from G GB/T 14992, HB/Z140, DB MS4705Y R03, QHY JT-184, SQMS 25.05.02-01, WS9-7009, WS9-7011, WS9-7095, WS9-7156, LX 6-0051.
| Type | Treatment Procedure | Remarks |
| Rolled flat bars | (1050~1080) ℃*8h/AC+845℃*24h/AC+700℃*16h/AC | |
| Round bars | (1050~1080) ℃*8h/AC+845℃*24h/AC+700℃*16h/AC |
Main Specifications
| Forming Method | Type | Nominal Diameter (mm) | Nominal Length (mm) |
| Forging/rolling | Bars | d20mm~400mm | |
| Rolling | flat bars | Thickness: 40mm-140mm × Width: 40-140mm |
Delivery Condition
Bars undergone the heat treatment or solid-solution, supplied after polishing or turning; flat bars shall undergo the solid-solution and aging heat treatment, and supplied after turning.
Chemical Composition
Chemical Composition
Excerpted from GB/T 14992, differences in impurity element analysis are excerpted from GJB 3317A and GJB 3318A.
| Type | C | Cr | Ni | Mo | Al | Ti |
| Mass fraction /% | ≤0.08 | 19.00~22.00 | Allowance | 1.80~2.30 | 0.35~0.75 | 0.35~0.75 |
| Element | Nb | Mn | Si | P | S | Cu |
| Mass fraction /% | 0.90~1.30 | ≤0.40 | ≤0.80 | ≤0.020 | ≤0.012 | ≤0.20 |
| Element | Fe | |||||
| Mass fraction /% | ≤3.00 | |||||
| Element | ||||||
| Mass fraction /% | ||||||
| GJB 3317A and GJB 3318A stipulate: Cu≤0.07%. | ||||||
Mechanical Properties
Hardness
| Standard No. | Grade | Hardness HBW |
| DB MS 4705Y R03 | Quenched-and-tempered flat bars | 310~400 |
Impact Toughness
| Standard No. | Grade | Impact KV2 |
| DB MS 4705Y R03 | Quenched-and-tempered flat bars | ≥20 |
Tensile Properties
| Room Temperature Tensile | High Temperature Tensile | |||||||||
| Standard | Heat Treatment Procedure | Spec. (mm) | Yield Strength | Tensile Strength | Elongation | Reduction of Area | Temperature | Yield Strength | Elongation | Reduction of Area |
| GJB1952A | 1050-1090)°C/A °C | 220 | ≥735 | ≥40 | - | 800 | 245 | ≥40 | - | |
Endurance Properties
| Test Temperature (℃) | Stress (MPa) | Duration (h) | Elongation | Reduction of Area |
| 650 | 245 | ≥100 | ≥9 | ≥40 |
