Electro-Discharge Machining (EDM) is critical for post-processing precision features in superalloy investment castings. It enables tight-tolerance machining without inducing mechanical stress in high-hardness materials or complex geometries that are difficult to conventionally machine.
At Neway Aerotech, our superalloy EDM services complement vacuum investment casting to produce high-performance components for aerospace, energy, and nuclear applications.
EDM Process | Surface Roughness (Ra, μm) | Dimensional Tolerance (mm) | Aspect Ratio | Heat Affected Zone (HAZ, μm) | Min. Feature Size (mm) |
|---|---|---|---|---|---|
Wire EDM | 0.3–1.2 | ±0.002–±0.01 | Up to 20:1 | 2–5 μm | ~0.1 |
Sinker EDM | 0.4–2.5 | ±0.005–±0.02 | Up to 10:1 | 5–10 μm | ~0.2 |
Hole Drilling EDM | 0.5–3.0 | ±0.02–±0.05 | Up to 30:1 | 10–15 μm | ~0.1 |
Micro-EDM | 0.1–0.4 | ±0.001–±0.005 | Up to 15:1 | <2 μm | <0.05 |
HAZ varies depending on energy level, pulse duration, and material conductivity.
Wire EDM: Ideal for trimming parting lines, tight contours, and gate removal on investment castings.
Sinker EDM: Best for refining internal cavities, cooling channels, and casting-based electrode seat features.
Hole Drilling EDM: Used for cooling or lubrication passages in turbine blades and nozzle rings.
Micro-EDM: Enables ultra-fine finishing in cast micro-feature zones or pilot-hole creation for complex assemblies.
Material | Hardness (HRC) | Thermal Fatigue | Casting Suitability | EDM Efficiency | Applications |
|---|---|---|---|---|---|
36–42 | Excellent | Good | High | Turbine wheels, vanes | |
38–44 | High | Excellent | Moderate | Combustor segments, aerospace brackets | |
42–46 | Superior | Single-crystal only | Low | Turbine blades, high-temperature airfoils | |
30–35 | Good | Very good | High | Exhaust manifolds, chemical processing | |
40–45 | Excellent | Moderate | Moderate | Rocket nozzles, valve seats |
Inconel 713C: Best for vanes with tight-profile machining; responds well to wire EDM with minimal recast.
Rene 77: Ideal for parts needing high creep strength; EDM recommended for sealing features and bolt holes.
CMSX-4: Requires low-energy EDM; used only where grinding is infeasible due to thermal damage risks.
Hastelloy X: Easily machined by sinker or wire EDM; good choice for welded cast assemblies.
Nimonic 115: Useful for high-cycle tooling; EDM ensures repeatability in fitting and flow-critical areas.
A client in the power generation sector needed final machining of a Rene 77 turbine nozzle ring cast using vacuum investment technology. Tolerances of ±0.005 mm were required across 22 radial ports and sealing shoulders.
Casting: Investment cast Rene 77, hot isostatically pressed post-casting at 1195°C, 100 MPa, 4 hours.
Rough Machining: CNC-turned interfaces and ring surface, 0.5 mm stock left for EDM finishing.
Wire EDM: Profiled each radial cooling port (Ø1.2 mm) at ±0.003 mm using 0.25 mm brass wire.
Sinker EDM: Machined three internal cavities, spark gap 0.08 mm, depth 10 mm with ±0.005 mm tolerance.
Stress relief at 950°C for 2 hours under inert gas
Hot Isostatic Pressing to seal casting porosity
TBC Coating applied on heat-facing zones
Electro-polished to Ra ≤ 0.6 μm
Passivated for corrosion resistance
Deburred under microscope to remove <50 μm edge burrs
CMM inspection on 50 points, all within ±2 μm
X-ray void check revealed zero shrinkage cavities
SEM verified clean spark surface and grain integrity
Ultrasonic immersion testing confirmed full structural soundness
EDM finishing held consistent profile tolerances of ±0.003 mm across all port entrances and sealing zones on the ring.
HIP post-processing resulted in 100% pore sealing, confirmed by ASTM E192 testing and X-ray level 2 acceptance.
Surface integrity after electro-polishing exceeded Ra ≤ 0.6 μm, eliminating risk of flow-induced erosion or fatigue cracking.
SEM analysis showed uniform spark-textured zones without recast layers or microcracking at grain boundaries.
Final inspection confirmed complete geometric compliance and zero internal defects, exceeding aerospace turbine component acceptance standards.
What surface finish can be achieved using EDM on cast superalloy components?
How does EDM affect the metallurgical integrity of investment cast parts?
Can internal cooling channels in turbine castings be processed with EDM?
Is EDM suitable for single crystal or directionally solidified components?
What post-treatment is required after EDM of aerospace castings?