Thermal Spray & Coating
HVOF & Thermal Spray Masking Shadow Tolerance Calculator
Model supersonic particle in-flight velocity ($v_p$), gun standoff distance ($L_{stand}$), plume divergence angle ($\theta_{div}$), shadow mask edge blur ($R_{blur}$), and chamfer relief angles for tungsten carbide and MCrAlY coatings.
1. Input Parameters
Distance from the spray torch nozzle exit to the substrate.
Angular spread of the supersonic particle jet.
Gap between the underside of the shadow mask and the target part.
Thickness of hardened steel / copper shadow mask plate.
Finished nominal coating layer thickness.
2. Calculation Results
Mask Shadow Blur ($R_{blur}$)
0.00 mm
Rec. Mask Chamfer Angle ($\alpha$)
0.0°
Spot Diameter on Surface
0.0 mm
Edge Transition Quality
Sharp Edge (<0.15mm)
DXF Mask Inward Offset
0.00 mm
Estimated Robot Passes
0 Passes
3. Dynamic Visualizer & CAM Preview
4. Engineering Notes & Physics Specifications
HVOF Supersonic Particle Dynamics & Shadow Masking Geometry:
- Shadow Blur Radius: Particles traveling at angle $\theta_{div}$ cast a penumbra under the mask edge: $R_{blur} = d_{mask} \cdot \tan(\theta_{div})$. To achieve aerospace sharp edge cutoffs, $d_{mask}$ must be clamped to $< 0.5\text{ mm}$.
- Knife-Edge Mask Chamfer: Thick mask plates reflect supersonic shockwaves and cause heavy buildup ridges on mask edges. The outer edge must feature a $30^\circ - 45^\circ$ chamfer relief facing the oncoming jet: $\alpha_{chamfer} \ge 90^\circ - \theta_{div} - 15^\circ$.
- CAM Offset Calibration: Because the coating profile tapers in the shadow zone, the vector mask boundary in DXF must be offset inward by $\Delta w = R_{blur} / 2$ to place the nominal thickness boundary at the true design datum.
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