Heat-Affected Zone (HAZ) Control for Flight-Critical Parts
The Heat-Affected Zone is the region adjacent to the laser cut where material properties are altered by thermal exposure. For flight-critical aerospace parts, uncontrolled HAZ can reduce fatigue life, alter corrosion resistance, and create initiation sites for stress-corrosion cracking.
Quick Answer
Aerospace specifications typically limit HAZ depth to <0.05mm (50μm) for flight-critical parts and <0.1mm (100μm) for non-critical structures. Recast layer (re-solidified material) must be <0.025mm (25μm). These are achieved by maximizing cutting speed, using minimum effective power, and maintaining high assist gas pressure for enhanced cooling.
HAZ Specification Limits by Material
| Material | HAZ Depth Limit | Recast Layer Limit | Micro-Crack | Typical Spec |
|---|---|---|---|---|
| Ti-6Al-4V (flight) | ≤0.05mm | ≤0.013mm | Zero permitted | AMS 2774 |
| Inconel 718 (flight) | ≤0.05mm | ≤0.025mm | Zero permitted | AMS 2759 |
| Aluminum (structural) | ≤0.1mm | ≤0.05mm | ≤25μm | Customer spec |
| 17-4PH SS (brackets) | ≤0.15mm | ≤0.075mm | ≤50μm | BAC 5000 series |
HAZ Measurement Methods
Metallographic Cross-Section
- • Method: Mount, polish, etch, examine at 200–500×
- • Etchant: Kroll's solution (Ti), oxalic acid (Inconel)
- • Measure: HAZ depth from cut edge to unaffected base
- • Frequency: Per qualification, then per lot/setup change
- • Accuracy: ±0.005mm at 500× magnification
Micro-Hardness Traverse
- • Method: Vickers micro-hardness at 25–50μm intervals
- • Start: 25μm from cut edge, traverse into base material
- • HAZ boundary: Where hardness returns to ±5% of base value
- • Load: HV 0.1 (100g) or HV 0.025 (25g) for thin HAZ
- • Standard: ASTM E384 for micro-hardness testing
Fatigue Life Impact
HAZ depth directly correlates with fatigue life reduction. For Ti-6Al-4V, published data shows that a 0.1mm HAZ reduces high-cycle fatigue life by approximately 25–40% compared to machined edges. Keeping HAZ below 0.05mm limits fatigue life reduction to <10%, which is acceptable for most flight-critical applications with appropriate safety factors applied.
| HAZ Depth | Fatigue Reduction (Ti-6Al-4V) | Fatigue Reduction (Inconel 718) | Aerospace Acceptability |
|---|---|---|---|
| <0.025mm | <5% | <5% | All applications |
| 0.025–0.05mm | 5–10% | 5–8% | Flight-critical OK |
| 0.05–0.1mm | 10–25% | 8–20% | Non-critical only |
| >0.1mm | 25–50% | 20–40% | Reject / rework |
HAZ Minimization Strategies
Process Optimization
- • Maximize cutting speed (reduce thermal input per unit length)
- • Use minimum effective power (avoid excess energy)
- • High-pressure inert gas (18–25 bar) for convective cooling
- • Short focal length optics for smaller spot, higher power density
- • Pulsed mode for tight corners and small features
Equipment Selection
- • Low BPP fiber laser source (high beam quality = smaller HAZ)
- • Single-mode laser for thin materials (<2mm)
- • Autofocus cutting head with real-time standoff control
- • High-dynamic servo drives for consistent speed in corners
- • Trailing gas shield nozzle for titanium >2mm
Related Topics
Disclaimer: HAZ limits vary by customer specification and part criticality. Fatigue reduction data is based on published research and may not apply to all alloy conditions. Validate with coupon testing per your applicable specification.