A payload drone structure
By designing a heavy-load clamping mechanism, a replacement latching mechanism, and a latching auxiliary mechanism, the problems of unstable clamping of heavy-duty UAVs and inconvenient installation of lifting components are solved, achieving efficient and reliable heavy-load transportation and component replacement.
CN224528982UActive Publication Date: 2026-07-21ORDOS INST OF APPLIED TECH
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- ORDOS INST OF APPLIED TECH
- Filing Date
- 2025-09-26
- Publication Date
- 2026-07-21
Smart Images
Figure CN224528982U_ABST
Abstract
The utility model discloses a kind of heavy-duty unmanned aerial vehicle structures, including unmanned aerial vehicle assembly, hoisting assembly, weight clamping mechanism, replacement clamping mechanism and clamping auxiliary mechanism, the weight clamping mechanism includes driving motor and installation frame, the replacement clamping mechanism includes clamping pipe and clamping rod, the clamping auxiliary mechanism includes outer swivel ring and double-layer clamping ring, weight clamping mechanism is driven gear transmission system by driving motor control, so that the pair of clamping frame can accurately clamp different shape weights, replacement clamping mechanism uses the design of clamping pipe and clamping rod cooperation, by limit swivel ring rotation drives clamping block to embed or away from clamping rod, the quick connection and disassembly of component are realized, ratchet ring prevents limit swivel ring accidental reverse, make connection more reliable, greatly improve the efficiency and flexibility of unmanned aerial vehicle function conversion.
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