H-Quad Tilt-Rotor UAV

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Bounding box: 2150.0 × 1810.0 × 220.0 mm
Engine: Precision B-rep
Parameters: 27
Published: August 9, 2026

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The prompt

i want you to design a fuselage of quad wing with tilt rotor mechanism uav (h shaped), with appropriate dimesnions

Parameters

Name	Value	Range
Fuselage Length	700 mm	200 – 1500
Fuselage Width	180 mm	50 – 500
Fuselage Height	220 mm	50 – 500
Boom Length	1600 mm	500 – 3000
Boom Outer Diameter	45 mm	10 – 100
Boom Wall Thickness	2.5 mm	0.5 – 10
Wing Span	500 mm	100 – 1000
Wing Chord	220 mm	50 – 500
Wing Max Thickness	15 mm	5 – 50
Wing Camber (fraction)	0.02	0 – 0.04
Camber Position (fraction)	0.4	0.1 – 0.6
Nacelle Length (X)	100 mm	30 – 200
Nacelle Width (Y)	80 mm	20 – 200
Nacelle Height (Z)	70 mm	20 – 150
Propeller Diameter	500 mm	200 – 1000
Hub Diameter	30 mm	10 – 80
Blade Width (chord)	30 mm	10 – 60
Blade Thickness	3 mm	1 – 8
Front Wing Root X	500 mm	200 – 1000
Rear Wing Root X	-500 mm	-1000 – -200
Boom Y Offset	300 mm	100 – 600
Wing Tip \|Y\|	800 mm	400 – 1200
Nacelle Inboard Offset	20 mm	5 – 50
Nacelle Z Position	60 mm	30 – 100
Boom Z Position	20 mm	0 – 60
Wing Root Z Position	40 mm	10 – 80
Fuselage Z Position	0 mm	-20 – 50

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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