Astroloy M,Astroloy M Plate,UNS N13017,E FORU

British Specs:，American Specs:AMS 5882 Forgings，German Specs:

### **Product Introduction: Astroloy M (UNS N13017) Plate** **Astroloy M (UNS N13017) Plate** is a premium powder metallurgy nickel-based superalloy supplied in plate form, designed for the most demanding high-temperature applications in aerospace and power generation industries. Manufactured through advanced powder metallurgy (PM) processes followed by thermomechanical working, this plate product offers exceptional strength, creep resistance, and microstructural stability that surpass conventional wrought superalloys. The plate configuration of Astroloy M provides a versatile platform for manufacturing large structural components that must withstand extreme temperatures up to 980°C (1800°F) while maintaining structural integrity under high mechanical loads. --- #### **Key Features & Advantages** * **Exceptional High-Temperature Strength**: Maintains superior mechanical properties at temperatures up to 980°C (1800°F) * **Outstanding Creep Resistance**: Excellent long-term performance under constant stress at elevated temperatures * **Superior Microstructural Homogeneity**: PM processing ensures uniform, fine-grained structure free from chemical segregation * **Excellent Oxidation Resistance**: Withstands aggressive high-temperature environments and corrosive conditions * **Enhanced Fabrication Capability**: Plate form allows for machining of large, complex components with consistent properties * **Optimized Thermal Stability**: Maintains dimensional stability and mechanical properties after prolonged high-temperature exposure --- #### **Chemical Composition (Typical Weight %)** | Element | Content (%) | Element | Content (%) | |---------|-------------|---------|-------------| | **Nickel (Ni)** | Balance | **Molybdenum (Mo)** | 4.5 - 5.5 | | **Chromium (Cr)** | 14.0 - 16.0 | **Aluminum (Al)** | 4.0 - 4.5 | | **Cobalt (Co)** | 16.0 - 18.0 | **Titanium (Ti)** | 3.4 - 3.8 | | **Carbon (C)** | 0.02 - 0.06 | **Boron (B)** | 0.015 - 0.030 | | **Zirconium (Zr)** | 0.025 - 0.050 | **Iron (Fe)** | ≤ 0.50 | | **Manganese (Mn)** | ≤ 0.10 | **Silicon (Si)** | ≤ 0.10 | | **Sulfur (S)** | ≤ 0.015 | **Copper (Cu)** | ≤ 0.10 | --- #### **Physical Properties** | Property | Metric Unit | Imperial Unit | |----------|-------------|---------------| | **Density** | 8.0 g/cm³ | 0.289 lb/in³ | | **Melting Range** | 1330 - 1380 °C | 2425 - 2515 °F | | **Thermal Expansion Coefficient** | 12.8 μm/m·°C (20-100°C) | 7.1 × 10⁻⁶ in/in·°F | | **Modulus of Elasticity** | 210 GPa | 30.5 × 10⁶ psi | | **Thermal Conductivity** | 11.5 W/m·K (100°C) | 80 Btu·in/hr·ft²·°F | | **Specific Heat** | 420 J/kg·K (20°C) | 0.10 Btu/lb·°F | --- #### **Mechanical Properties (Typical for HIPed + Heat-Treated Plate)** | Property | Value (Metric) | Value (Imperial) | |----------|----------------|------------------| | **Tensile Strength, Ultimate** | 1400 - 1600 MPa | 203 - 232 ksi | | **Tensile Strength, Yield (0.2% Offset)** | 1100 - 1300 MPa | 160 - 189 ksi | | **Elongation at Break** | 10 - 20 % | 10 - 20 % | | **Reduction of Area** | 12 - 25 % | 12 - 25 % | | **Creep Rupture Strength (980°C/100h)** | ≥ 120 MPa | ≥ 17.4 ksi | --- #### **International Standards** * **AMS 6306**: Primary specification for "Bars, Forgings, and Rings, Powder Metallurgy Nickel-Base Superalloy" * **ASTM B670**: Standard specification for precipitation-hardened nickel alloy plate, sheet, and strip * **ASME SB670**: ASME boiler and pressure vessel code specification * **UNS N13017**: Unified Numbering System designation * **OEM Specifications**: Meets proprietary standards for major aerospace manufacturers --- #### **Product Applications** **Aerospace & Defense:** - Jet engine structural components and mounting systems - Afterburner components and combustion chamber structures - Rocket motor casings and structural supports - Turbine mid-frame structures and support rings - High-temperature thermal protection systems **Power Generation:** - Advanced gas turbine structural components - Combustion liner supports and transition pieces - Turbine casing components and support structures - Heat treatment furnace components and fixtures **Specialized Industrial:** - High-temperature processing equipment - Hot work tooling and dies - Nuclear reactor core components - Specialized test and measurement equipment --- **Disclaimer:** *Astroloy is a trademark associated with various high-performance alloy manufacturers. The information provided is for reference purposes only. Astroloy M plate represents a specialized product form requiring advanced manufacturing expertise. Final material properties and performance characteristics depend on specific manufacturing processes, heat treatments, and end-use conditions. Consultation with materials engineers and strict adherence to relevant specifications is mandatory for critical applications.*

Packing of Standard Packing: Typical bulk packaging includes palletized plastic 5 gallon/25 kg. pails, fiber and steel drums to 1 ton super sacks in full container (FCL) or truck load (T/L) quantities. Research and sample quantities and hygroscopic, oxidizing or other air sensitive materials may be packaged under argon or vacuum. Solutions are packaged in polypropylene, plastic or glass jars up to palletized 3085 gallon liquid totes Special package is available on request.