Gears and transmission
Futuristic VTOL Aircraft – Exploded View
- Bounding box
- 17400.0 × 1900.0 × 1500.0 mm
- Engine
- Precision B-rep
- Parameters
- 32
- Published
- August 10, 2026
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The prompt
Design a futuristic two-seat electric VTOL aircraft with a sleek aerospace-inspired appearance. The aircraft has a lightweight carbon-fiber monocoque fuselage with a glossy black and silver finish, featuring a large panoramic tinted glass cockpit canopy. The cabin seats two people side by side with minimalist controls and digital displays. The aircraft uses six large ductless propellers mounted on carbon-fiber arms. Four primary lift motors are positioned symmetrically around the cabin—front-left, front-right, rear-left, and rear-right. Two additional high-thrust motors are mounted beneath the center section to provide extra vertical lift during takeoff and landing. The rear motors are installed on tilt mechanisms that rotate up to 90 degrees, allowing the aircraft to transition from vertical flight to forward flight. The design includes aerodynamic fairings over the motor mounts and integrated cooling vents. Under the cabin is a streamlined battery compartment forming the belly of the aircraft. Retractable carbon-fiber landing skids extend below the fuselage. Navigation lights are integrated into the arm tips, with red lights on the left, green on the right, and white rear position lights. The aircraft includes roof-mounted GPS antennas, LiDAR sensors, forward stereo cameras, and obstacle-detection sensors integrated into the nose and sides. The central avionics compartment houses the flight controller, AI computer, communication systems, and redundant power electronics. The body has smooth aerodynamic curves with sharp futuristic styling inspired by next-generation air taxis. Show exposed carbon-fiber textures, titanium structural joints, and high-tech engineering details. Render the model in a professional CAD style with front, side, top, rear, and isometric views on a white engineering background. Include exploded views showing the fuselage, motors, battery pack, landing gear, avionics, and propeller assemblies.
Parameters
| Name | Value | Range |
|---|---|---|
| Layout Gap | 1500 mm | 500 – 5000 |
| Fuselage Length | 4200 mm | 3000 – 6000 |
| Fuselage Width | 1800 mm | 1000 – 3000 |
| Fuselage Height | 1500 mm | 1000 – 2500 |
| Canopy Length | 1600 mm | 1000 – 2500 |
| Canopy Width | 900 mm | 500 – 1500 |
| Canopy Height | 700 mm | 300 – 1000 |
| Main Propeller Diameter | 1200 mm | 800 – 2000 |
| Main Motor Housing Diameter | 150 mm | 100 – 300 |
| Main Motor Housing Height | 100 mm | 50 – 200 |
| Main Hub Diameter | 80 mm | 50 – 150 |
| Main Hub Height | 30 mm | 10 – 50 |
| Main Arm Diameter | 60 mm | 30 – 100 |
| Main Arm Length | 800 mm | 500 – 1500 |
| Rear Tilt Angle (deg) | 30 deg | 0 – 90 |
| Center Propeller Diameter | 1000 mm | 700 – 1500 |
| Center Motor Housing Diameter | 300 mm | 200 – 500 |
| Center Motor Housing Height | 150 mm | 100 – 300 |
| Center Hub Diameter | 100 mm | 50 – 150 |
| Center Hub Height | 30 mm | 10 – 50 |
| Center Arm Diameter | 50 mm | 30 – 80 |
| Center Arm Length | 300 mm | 200 – 600 |
| Battery Length | 2400 mm | 1500 – 3500 |
| Battery Width | 1100 mm | 500 – 1500 |
| Battery Height | 500 mm | 200 – 800 |
| Skid Length | 1800 mm | 1000 – 2500 |
| Skid Width | 20 mm | 10 – 50 |
| Skid Height | 20 mm | 10 – 50 |
| Skid Spacing | 800 mm | 400 – 1200 |
| Avionics Length | 600 mm | 300 – 1000 |
| Avionics Width | 400 mm | 200 – 600 |
| Avionics Height | 300 mm | 200 – 500 |
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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