Extended-finger load review
Actual linear-static FEM of the two 50 mm exposed fingers, with a separate rigid-body planar drive calculation. The final CAD geometry is preserved in both finger analyses.
Load case and model
| Condition | Applied value |
|---|---|
| Material | Aluminium 7075-T6; E = 71,700 MPa; Poisson ratio 0.33; assigned yield 503 MPa |
| Support | Entire bottom mounting-foot face fixed in all three translations |
| Normal load | 25 N per finger; +X on the right, −X on the left |
| Tangential load | 7.405 N in −Y in each separate case |
| Assumption | Entire 0.5 kg × (9.81 + 5 m/s²) assigned to each individual finger |
| Load application | Forces distributed on the aluminium tip face at Z = 82 mm |
| Engine | Installed METHEUS FEM service · FreeCAD 1.1.1 / CalculiX 2.22 |
Mesh refinement
| Finger | Maximum element size | Nodes | Raw peak stress | Maximum displacement |
|---|---|---|---|---|
| R | 1.8 mm | 22,881 | 17.132 MPa | 0.051740 mm |
| R | 1.2 mm | 45,891 | 18.558 MPa | 0.051913 mm |
| R | 0.8 mm | 105,369 | 21.479 MPa | 0.051972 mm |
| L | 1.8 mm | 21,751 | 16.592 MPa | 0.039111 mm |
| L | 1.2 mm | 42,780 | 17.739 MPa | 0.039257 mm |
| L | 0.8 mm | 95,833 | 19.593 MPa | 0.039307 mm |
The material values are analysis-card assumptions, not a material certificate. Production fillets, local stress convergence, mounting-foot screws, carrier flexibility, pad bond and contact, eccentric torsion, fatigue and physical payload retention remain to be checked.
Separate planar drive review
| Calculation | Result |
|---|---|
| Normal-load pair peak | 1.913390 N·m |
| Combined conservative sample peak | 1.955724 N·m |
| Motor demand at 85% assumed efficiency | 2.300852 N·m |
| Selected motor rated torque | 2.5 N·m |
Rigid-body virtual work uses the original 72 motion samples, 25 N normal load per jaw and 7.405 N total tangential load. Absolute component contributions are combined at each sample; separate component maxima are not simply added. The change in finger Z reach does not double the planar rotary torque. Inertia, friction, motor thermal duty and out-of-plane assembly strength are outside this calculation.
Historical plate analysis and source checks
The v1.2 three-plate planar MFBD result is retained as historical evidence only. It is not a fresh validation of the longer fingers, revised adapter or full assembly. The actual finger solids were compared against the final native CAD in local coordinates: both Boolean differences are zero for each side. Distributed load sums and fixed/loaded face planes were independently checked in all six solver input decks.
Independent review record · Recorded prompts and subsequent review