
Turbomachinery Blades & Vanes: Enabled with PECM
Voxel applies PECM to aerospace blades and vanes where edge condition, feature consistency, and repeatability across parts directly affect aerodynamic performance and reliability. PECM enables burr-free machining and finishing of thin sections, edge features, and repeated geometries without introducing tool-induced damage or residual stress. Through the use of custom-designed cathodes, Voxel supports consistent feature replication across production volumes, making PECM well suited for blade and vane components where geometric variation or post-processing risk must be tightly controlled.

Blade and vane performance is highly sensitive to edge geometry and surface condition. Leading and trailing edge definition influences boundary layer behavior and local flow separation, while dimensional variation across airfoils can alter stage efficiency and loading distribution. In repeated blade arrays, small geometric inconsistencies from part to part may accumulate into measurable aerodynamic imbalance at the assembly level.
Conventional machining processes rely on mechanical tool contact, which can introduce localized stress or deformation in thin sections. In high-aspect-ratio airfoil regions, especially near trailing edges or tight fillets, tool-induced forces may require secondary finishing steps to achieve final geometry. Each additional operation increases handling risk and potential geometric drift.
Electrical discharge machining (EDM), while capable of complex geometry formation, removes material through localized thermal erosion. Depending on the application, this may introduce surface microstructural changes that must be addressed in subsequent processing. In fatigue-critical aerospace components, surface integrity and microgeometry consistency are closely evaluated as part of overall reliability considerations.
PECM removes material through controlled electrochemical dissolution without mechanical contact at the cutting interface. Thin sections and repeated features can be generated with reduced risk of distortion, and edge transitions can be controlled through cathode geometry and pulse parameter management. This is particularly advantageous in blade and vane components incorporating slot arrays, cooling features, or repeated aerodynamic contours.
As engine architectures evolve toward higher efficiency and increased thermal loading, manufacturing stability becomes a design constraint rather than an afterthought. Feature-to-feature consistency within a single airfoil is critical, but part-to-part repeatability across production lots ultimately determines assembly balance and long-term reliability. By integrating cathode design, electrolyte control, and pulsed parameter optimization, Voxel supports production-scale replication of complex blade and vane geometries where aerodynamic performance and fatigue resistance must be tightly managed.

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300μm microholes in copper

Demonstration of internal "s-shaped" non-line-of-sight finishing capabilities via PECM

PECM finishing on conal-shaped sample parts to demonstrate postprocessing capability

300μm microholes in copper
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