Aerospace Alloy Bar
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- Aerospace Alloy Bar
- Aerospace Alloy Sheet
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- Titanium Alloy Pipe and Fitting
- Stainless Steel Strip Coil/Sheet
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- Angle Steel/Channel Steel
| Product Origin: | China |
| MinimumOrder Quantity: | 10KG |
| Packaging Details: | Standard export packaging or as per customer requirements. |
| Delivery Time: | 5 – 10days |
| Payment Method: | Letter of Credit, Telegraphic Transfer, Western Union Remittance |
| Supply Capacity: | 3,000 tons per month |
| Delivery Method: | FOB/CFR/CNF/CIF/EXW |
Product Description
Product details and core characteristics of internationally used Aerospace Alloy Bar
- High-strength alloy steel bar: Bearing ultimate static loads and impacts
- Ultra-high strength (1.8-2.2 GPa)
- High fracture toughness (K₁C ≥ 50 MPa·m¹/²)
- Excellent fatigue resistance
- Fine tempered martensite matrix with controlled impurity elements and grain boundary segregation.
- Applications: Aircraft landing gear struts, main load-bearing joints, seat rails, high-strength fasteners.
- Superalloy bar: Operating continuously in extreme thermal-mechanical environments
- Exceptional high-temperature strength and creep resistance
- Outstanding oxidation/thermal corrosion resistance
- Excellent thermomechanical fatigue performance
- Stability in the quantity, size, morphology, and distribution of γ' phase (Ni₃(Al, Ti)).
- Applications: Engine turbine disks, turbine shafts, compressor disks, key fasteners for combustion chambers.
- Titanium alloy bar: Achieving a combination of high strength, light weight, and corrosion resistance
- Top-tier specific strength
- Excellent fatigue resistance and crack propagation resistance
- Superior corrosion resistance
- The ratio, morphology, and texture of α+β phases. Purity (control of interstitial elements O and N) is crucial.
- Applications: Airframe frames/beams, engine fan/compressor disks and blades, landing gear torque arms, fasteners.
- Aluminum alloy bar: Enabling efficient lightweighting and manufacturing of complex components
- Good specific strength and workability
- Excellent fatigue performance
- Mature supply chain and cost-effectiveness
- Control of the size, distribution of aging precipitated phases (such as θ', η') and grain boundary precipitate-free zones.
- Applications: Aircraft seat frames, control system rods, engine brackets, various connecting brackets.
Core standards and typical grades of the four major standard systems
| Standard System | Material Category | Implementation Standard | Typical Grade/Designation | Key Characteristics and Aerospace Applications |
| American standards SAE/AMS | High-strength alloy steel bar | AMS 6427 | 4340 | Landing gears, transmission shafts and other key load-bearing components. |
| Superalloy bar | AMS 5662 | Inconel 718 (UNS N07718) | Core materials for engine turbine disks and blades. | |
| AMS 5759 | L605 | Combustion chambers and nozzle areas of aerospace engines. | ||
| Titanium alloy bar | AMS 4928 | Ti-6Al-4V (Gr.5) | The most widely used aerospace titanium alloys. | |
| Copper alloy bar | ASTM B150/B150M | C63000(UNSC63000 ) | High strength, wear-resistant and corrosion-resistant, used for bearings and gears. | |
| Titanium alloy bar | SAE/AMS (4120,4121,4122) | 7075-T6(AMS4120) 7076-T73(AMS4121) 2024-T3/T3511(AMS4127 | It is specially used for aerospace, specifying specific processes, inspections and quality control that meet aviation requirements. | |
| European standards EN | Alloy steel/special steel bar | EN 10250-4 | 34CrNiMo6 (1.6582) | High - toughness core load - bearing components |
| Titanium alloy bar | EN 2002-1 | Ti-P64001 (≈Ti-6Al-4V) | Core grades in European aviation | |
| Copper alloy bar | EN 12163/12164 | CW307G (≈CuAl10Ni5Fe4) | Corresponding high - strength aluminum bronze in Europe | |
| Aluminum alloy bar | EN2076/EN4269 | EN AW-7075/EN AW-2024 EN AW-6082 | Aerospace projects will reference standards and add strict additional technical conditions. | |
| Russian standards ГОСТ | High-strength corrosion-resistant steel bar | ГОСТ 4543 | 30ХГСНА (30KhGSN2A) | Classic high-strength steel for key aircraft structures |
| Titanium alloy bar | ГОСТ 26492 | ВТ6 (VT6, ≈Ti-6Al-4V) | Main aerospace titanium alloys | |
| Copper alloy bar | ГОСТ 1628 | БрАЖН 10-4-4 (BrAZHN10-4-4) | High-strength aluminum-iron-nickel bronze | |
| Aluminum alloy bar | ГОСТP,OCT | AK8,AK4-1u,B95nu,B96u | Independent naming system, with the suffix "u" indicating aviation grade and "n" indicating plates | |
| Chinese standards GB/GJB/HB | High-strength alloy steel bar | GJB 1951A | 30CrMnSiNi2A | Key steel for the main load-bearing structures of domestic aircraft. |
| Superalloy bar | GJB/T3165A-2018 | GH4169 (≈Inconel 718) | Core hot-end components of the engine. | |
| GJB 3317A-2019 | GH605(L605) | Combustion chambers and nozzle areas of aerospace engines. | ||
| Titanium alloy bar | GJB 2218A | TC4 (Ti-6Al-4V) | Military standards, with technical requirements higher than national standards. | |
| Copper alloy bar | GB/T 13808 | QAl10-4-4 | High-strength aluminum-nickel-iron bronze. | |
| Aluminum alloy bar | GJB2351A HB5202 | 2A12(≈2024)/7A04(≈7075) 7B04(7475)/6A02(≈6061) | The technical requirements of GJB/HB are much higher than international ones, including special metallurgical and testing requirements. |
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