Q-UAV
Dual-Use heavy lift multirotor drone.
Pushing the envelope.
Developed by a team of aerospace research engineers backed by The Levyne Group (R&D), this project pushes the boundaries of lift, and payload enablement. Built as a showcase of our technical capabilities, it embodies the innovation and intelligence that define The Levyne Group.
Key Data
97.2KG
Thrust produced @100% power
6.4KG
Total carbon fibre airframe weight
1.42m
Maximum length
1.60m
Maximum width
Design & Engineering
Composite Construction
By using aerospace-grade carbon fiber composites, we engineered an ultralight 6.4 kg structural airframe that maximizes thrust-to-weight efficiency, enabling a >15:1 airframe-to-thrust ratio and leaving remaining mass dedicated purely to propulsion and payload capacity.
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CAD/CAM
Through advanced CAD and CAM, we translated theoretical designs and simulations into precision-engineered, modular components, streamlining production, eliminating manufacturing difficulties, and enabling the carbon-fiber airframe to be realized with structural integrity.
Powertrain
The fully electric powertrain, built around four high-performance ESCs, was engineered to minimise back-EMF and signal interference through careful design, including braided power distribution wiring, resulting in cleaner control signals, higher efficiency, and more reliable motor response under load.
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PACKAGING/ASSEMBLY
This was engineered with simplicity and serviceability in mind, balancing repairability, fault detection, and inspection with efficient construction and repeatable manufacturing, while carefully managing constraints such as interference reduction and battery integration to ensure function, cost-effectiveness and long-term product longevity.
