Ti-5Al-5V-5Mo-3Cr, widely known as Ti5553, is a high-strength near-beta titanium alloy developed for aerospace, defense, and structural applications requiring exceptional mechanical performance. It is known for its excellent strength-to-weight ratio, high fatigue resistance, and deep hardenability, making it ideal for components under extreme loading conditions.
Due to its hardness and metallurgical complexity, Ti5553 is best processed using advanced CNC machining services. High-precision CNC machined titanium parts made from Ti5553 must meet tight dimensional tolerances and stringent surface finish requirements, especially for use in aircraft structural elements, landing gear, and military systems.
Element | Composition Range (wt.%) | Key Role |
---|---|---|
Titanium (Ti) | Balance | Provides corrosion resistance and base strength |
Aluminum (Al) | 4.5–5.5 | Alpha stabilizer, increases high-temperature strength |
Vanadium (V) | 4.5–5.5 | Beta stabilizer, improves fatigue and toughness |
Molybdenum (Mo) | 4.5–5.5 | Enhances creep resistance and hardenability |
Chromium (Cr) | 2.5–3.5 | Contributes to phase stability and corrosion resistance |
Zirconium (Zr) | ≤0.3 | Increases creep and fatigue resistance |
Oxygen (O) | ≤0.15 | Strengthens alloy, affects ductility |
Iron (Fe) | ≤0.25 | Residual element |
Hydrogen (H) | ≤0.015 | Controlled to prevent embrittlement |
Property | Value (Typical) | Test Standard/Condition |
---|---|---|
Density | 4.78 g/cm³ | ASTM B311 |
Melting Range | 1600–1650°C | ASTM E1268 |
Thermal Conductivity | 6.8 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 1.70 µΩ·m at 20°C | ASTM B193 |
Thermal Expansion | 8.6 µm/m·°C | ASTM E228 |
Specific Heat Capacity | 560 J/kg·K at 20°C | ASTM E1269 |
Elastic Modulus | 115 GPa | ASTM E111 |
Property | Value (Typical) | Test Standard |
---|---|---|
Tensile Strength | 1100–1350 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 1030–1250 MPa | ASTM E8/E8M |
Elongation | ≥8% | ASTM E8/E8M |
Hardness | 340–390 HB | ASTM E10 |
Creep Resistance | Excellent | ASTM E139 |
Fatigue Resistance | High | ASTM E466 |
Ultra-High Strength: With yield strengths exceeding 1200 MPa, Ti5553 rivals steel in performance while offering nearly half the density.
Beta Phase Dominance: Its near-beta microstructure provides excellent hardenability and good thermal processability, ideal for forged or thick-section components.
Superior Fracture Toughness: Performs well in high-cycle fatigue environments, critical for aerospace fasteners and structural links.
Thermal Stability and Weldability: Although welding is challenging due to beta content, it can be achieved with proper filler and post-weld heat treatment.
High Strength and Work Hardening: Ti5553 rapidly works and hardens, leading to increased cutting forces and surface distortion if not machined with optimized tools.
Low Thermal Conductivity: Generates heat at the tool-workpiece interface, accelerating tool wear and risking dimensional drift.
Tool Adhesion and Notching: The alloy’s beta phase promotes galling and notch wear, especially on tool edges during turning and drilling.
Tight Tolerance Control: Springback and elastic recovery (~115 GPa modulus) require compensation in the final finishing stages.
Parameter | Recommendation | Rationale |
---|---|---|
Tool Material | Fine-grain carbide or CBN | Ensures durability under high cutting stress |
Coating | AlTiN or TiSiN (≥4 µm) | Provides thermal and abrasive protection |
Geometry | Positive rake, edge honed | Minimizes cutting pressure and edge wear |
Cutting Speed | 20–50 m/min | Reduces thermal buildup |
Feed Rate | 0.10–0.25 mm/rev | Ensures clean chip formation |
Coolant | High-pressure emulsion ≥100 bar | Prevents tool overheating and chip welding |
Operation | Speed (m/min) | Feed (mm/rev) | Depth of Cut (mm) | Coolant Pressure (bar) |
---|---|---|---|---|
Roughing | 20–30 | 0.15–0.20 | 2.0–3.0 | 80–100 (Through-tool) |
Finishing | 45–60 | 0.05–0.10 | 0.2–0.5 | 100–150 |
Hot Isostatic Pressing (HIP) increases fatigue resistance and structural soundness, ideal for landing gear and linkage systems.
Heat Treatment involves treating the solution at ~830–870°C and aging at 480–600°C for strength optimization.
Superalloy Welding requires a beta-compatible filler and post-weld stress relief to prevent alpha cases or brittleness.
Thermal Barrier Coating (TBC) protects components in high-temperature thrust and propulsion environments.
CNC Machining ensures ±0.01 mm tolerances on parts like control arms and high-load structural brackets.
Electrical Discharge Machining (EDM) suits complex internal profiles and fine features.
Deep Hole Drilling delivers straightness <0.3 mm/m with Ra ≤1.6 µm in thick or structural aerospace assemblies.
Material Testing includes SEM, hardness mapping, creep analysis, and ultrasonic inspection to ensure aerospace-grade compliance.
Ti5553 is evaluated through high-temperature tensile testing, microstructural phase validation, creep resistance testing, and ultrasonic NDT, following AMS and ASTM standards.
Aerospace: Used in bulkheads, landing gear beams, and structural members requiring ultra-high strength.
Defense: Applied in armor frames, missile components, and blast-resistant structures.
Power Generation: Ideal for compressor casings and turbine components exposed to cyclical loads.
Industrial Equipment: High-stress mechanical couplings and load-bearing assemblies in automation and robotics.
What CNC techniques are best for machining Ti5553 structural components?
How does Ti5553 compare to Ti-6Al-4V in terms of mechanical performance?
What post-machining heat treatments are recommended for Ti5553 parts?
Which aerospace assemblies typically use Ti5553 titanium alloy?
What tolerance and finish standards can be achieved for CNC machined Ti5553?