Gears and transmission
AeroMorph-GD UAV Wing Assembly (Exploded, FEA-Ready)
- Bounding box
- 1671.1 × 830.0 × 821.0 mm
- Engine
- Precision B-rep
- Parameters
- 41
- Published
- September 22, 2026
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Free to download and use. See the terms.
The prompt
Create a precise parametric 3D CAD model of the COMPLETE AeroMorph-GD UAV wing assembly for STRUCTURAL ANALYSIS / FEA. Combine: 1. Left NACA 4412 wing 2. Right NACA 4412 wing 3. Main spars 4. Wing-root hinge system 5. Gear-driven mechanism 6. Output shaft 7. Bearings 8. Hinge brackets 9. Locking index plate 10. Locking pin and spring 11. Spar adapters 12. Gearbox housing 13. Motor and gears UNITS: mm WING: - Total span: 1600 mm - Half span: 800 mm - Chord: 200 mm - Airfoil: NACA 4412 - Thickness: 24 mm - Main spar: Ø12 mm - Spar location: 50 mm from leading edge - Aileron: 300 × 50 mm MECHANISM: - Gearbox: 60 × 50 × 30 mm - Motor: Ø28 × 30 mm - Pinion: Ø10 mm - Main gear: Ø40 mm - Output shaft: Ø6 × 50 mm - Bearing: Ø25 × 7 mm - Hinge bracket: 50 × 50 × 5 mm - Locking plate: R30 × 5 mm - Locking pin: Ø5 mm - Spring: Ø8 × 20 mm - Spar adapter: 40 × 35 × 3 mm ASSEMBLY: Motor → Pinion → Main Gear → Output Shaft → Hinge → Wing Spar Create three configurations: - 0° dihedral - 10° dihedral - 20° dihedral STRUCTURAL ANALYSIS REQUIREMENTS: Create clean, watertight solid bodies suitable for FEA. Separate all structural components into individual bodies/parts. Define realistic contact interfaces: - Wing–spar - Spar–adapter - Adapter–hinge - Shaft–bearing - Gear–shaft - Bracket–housing - Locking pin–index plate Do NOT use cosmetic geometry. Remove unnecessary small fillets, threads, logos and cosmetic details that could interfere with meshing. Maintain all important load-bearing geometry. Provide: - Material assignment placeholders - Fixed-support faces - Load-application faces - Hinge/shaft contact regions - Locking-pin contact regions - Symmetry references - Coordinate system - Global origin FEA LOAD CASES: CASE 1: 0° dihedral static structural analysis. CASE 2: 10° dihedral static structural analysis. CASE 3: 20° dihedral static structural analysis. Evaluate: - Von Mises stress - Total deformation - Principal stress - Factor of safety - Reaction forces - Shaft stress - Gear stress - Hinge stress - Spar stress - Locking-pin stress - Wing-root stress Create a clean FEA-ready assembly with no gaps, duplicate bodies or unintended intersections. OUTPUT: 1. Complete 3D assembly 2. Exploded assembly 3. FEA-ready geometry 4. 0° configuration 5. 10° configuration 6. 20° configuration 7. Section view through hinge 8. Section view through gear mechanism 9. Section view through locking mechanism 10. Structural load-path view 11. Fully dimensioned assembly drawing 12. Separate editable parts 13. Assembly BOM IMPORTANT: Do not invent material properties, loads, boundary conditions or safety factors. Mark unspecified parameters as: PARAMETER TO BE VERIFIED The model must be suitable for ANSYS Static Structural / SolidWorks Simulation / equivalent FEA software.
Parameters
| Name | Value | Range |
|---|---|---|
| Exploded Layout Gap | 60 mm | 5 – 400 |
| Half Span | 800 mm | 200 – 2000 |
| Chord | 200 mm | 80 – 600 |
| Max Thickness | 24 mm | 6 – 80 |
| Aileron Span | 300 mm | 50 – 700 |
| Aileron Chord | 50 mm | 10 – 120 |
| Spar Loc. from LE | 50 mm | 10 – 150 |
| Spar Diameter | 12 mm | 4 – 30 |
| Spar Length | 800 mm | 100 – 2000 |
| Bracket Length | 50 mm | 20 – 200 |
| Bracket Width | 50 mm | 20 – 200 |
| Bracket Thickness | 5 mm | 2 – 20 |
| Gearbox Length X | 60 mm | 30 – 200 |
| Gearbox Width Y | 50 mm | 30 – 200 |
| Gearbox Height Z | 30 mm | 15 – 150 |
| Gearbox Wall | 3 mm | 1.5 – 10 |
| Motor Diameter | 28 mm | 10 – 100 |
| Motor Length | 30 mm | 10 – 150 |
| Gear Module | 0.5 mm | 0.2 – 2 |
| Pinion Teeth | 20 teeth | 8 – 60 |
| Main Gear Teeth | 80 teeth | 12 – 200 |
| Gear Face Width | 8 mm | 2 – 40 |
| Output Shaft Dia. | 6 mm | 2 – 30 |
| Output Shaft Length | 50 mm | 10 – 200 |
| Bearing OD | 25 mm | 8 – 80 |
| Bearing Bore | 6.2 mm | 2 – 60 |
| Bearing Width | 7 mm | 2 – 40 |
| Bearing Pair Spacing | 20 mm | 0 – 200 |
| Index Plate Radius | 30 mm | 10 – 150 |
| Index Plate Thickness | 5 mm | 1 – 30 |
| Index Hole Radius | 22 mm | 5 – 140 |
| Max Index Angle | 20 deg | 0 – 90 |
| Index Angle Step | 10 deg | 1 – 90 |
| Locking Pin Dia. | 5 mm | 1 – 30 |
| Locking Pin Length | 20 mm | 5 – 100 |
| Spring OD | 8 mm | 3 – 50 |
| Spring Envelope ID | 5 mm | 1 – 40 |
| Spring Free Length | 20 mm | 5 – 150 |
| Adapter Length | 40 mm | 10 – 200 |
| Adapter Width | 35 mm | 10 – 200 |
| Adapter Thickness | 3 mm | 1 – 20 |
Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.
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