A small, separate flapping wing vehicle for reconnaissance

Through modular design and biomimetic structural optimization, the problems of complex assembly and disassembly and low flight efficiency of flapping-wing aircraft have been solved, enabling high-efficiency flight and long-term reconnaissance, making it suitable for scientific research, teaching and multi-scenario missions.

CN122354822APending Publication Date: 2026-07-10廖羽洁
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2026-05-18
Publication Date
2026-07-10

AI Technical Summary

Technical Problem

Existing flapping-wing aircraft are complex to assemble and disassemble, have low flight efficiency, short endurance, limited reconnaissance functions, poor portability and deployment capabilities, and cannot simulate the opening and closing mechanism of bird flight feathers, resulting in high air resistance and low lift-to-drag ratio.

Method used

It features a modular fuselage, quick-release wing components, and a detachable tail fin, connected by a tool-less snap-fit ​​structure. The wings adopt a fence-like biomimetic structure, and the fuselage has a biomimetic bird-like streamlined shape. It is equipped with flexible skin and a carbon fiber frame, a detachable tail fin and servo motors, an integrated control system and solar panels, and supports quick replacement and self-destruct functions.

Benefits of technology

It achieves miniaturization, modularization, quick assembly and disassembly, high-efficiency flight, and long-term reconnaissance, improving lift-to-drag ratio and endurance. It is suitable for scientific research, teaching, and rapid deployment in the field, and has high biomimetic stealth and multi-scenario mission adaptability.

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Abstract

The application provides a small-sized separated flapping-wing aircraft for reconnaissance, and relates to the technical field of bionic flapping-wing aircrafts, characterized in that the small-sized separated flapping-wing aircraft comprises a modular fuselage, a quick-detachable wing assembly and a detachable tail wing, and the components are connected through a tool-free buckle type quick-assembly structure; the modular fuselage comprises two left-right split housings and a core cabin, the housings are internally provided with mounting slots, and the core cabin is arranged in the mounting slots; the quick-detachable wing assembly is arranged above the modular fuselage, and the detachable tail wing is arranged behind the modular fuselage; the quick-detachable wing assembly comprises a wing, and the wing root is provided with a quick-assembly buckle. The application has the advantages of compact structure, mature manufacturing process, low cost and convenient batch production. The module interfaces are standardized, and the supply chain can be divided for production. The application can be used for military individual reconnaissance and special operations, and is also applicable to the fields of scientific research and teaching, education and outdoor entertainment, and has wide market prospects and practical value.
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