Enclosures and housings
UAV Center Fuselage
- Bounding box
- 455.6 × 165.6 × 106 mm
- Engine
- 3D Printing B-rep
- Parameters
- 18
- Published
- November 1, 2026
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The prompt
Draft an aerodynamic center fuselage section for a fixed-wing UAV. It must be a hollow shell printed in PA-CF. The internal cavity must be exactly 450mm long, 160mm wide, and 100mm deep. Include a flush, removable top canopy for battery access, and a dual-door bottom hatch for payload deployment. Add internal 20mm cylindrical channels running laterally through the top to accept interlocking carbon fiber wing spars. Ensure the wall thickness is optimized for 3D printing durability.
Parameters
| Name | Value | Range |
|---|---|---|
| Internal cavity length | 450 mm | 200 – 600 |
| Internal cavity width | 160 mm | 60 – 300 |
| Internal cavity depth | 100 mm | 40 – 200 |
| Wall thickness | 2.8 mm | 1.2 – 5 |
| Overall body height | 106 mm | 70 – 200 |
| Vertical corner rounding | 20 mm | 5 – 40 |
| Spar bore diameter | 20 mm | 10 – 30 |
| Spar tube wall thickness | 3.5 mm | 2 – 8 |
| Channel centre spacing | 110 mm | 40 – 200 |
| Channel centre height | 84 mm | 30 – 110 |
| Canopy length | 300 mm | 100 – 440 |
| Canopy width | 150 mm | 60 – 158 |
| Canopy total thickness | 3 mm | 1.5 – 8 |
| Canopy flange thickness | 2 mm | 1 – 6 |
| Door length | 220 mm | 100 – 440 |
| Door width | 75 mm | 30 – 78 |
| Door total thickness | 3 mm | 1.5 – 8 |
| Door flange thickness | 2 mm | 1 – 6 |
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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