一种用于扑翼微飞行器的电磁式可折叠翼机构及微飞行器
By using an electromagnetic foldable wing mechanism to drive the folding and unfolding of the flapping-wing micro-aircraft's wings, the problems of large wing space occupation and easy damage are solved, achieving portability and lightweight effect.
CN118270268BActive Publication Date: 2026-07-17SUZHOU UNIV
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- SUZHOU UNIV
- Filing Date
- 2024-04-23
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
Existing flapping-wing aircraft typically have a one-piece wing structure, which is long, takes up a lot of space, is inconvenient to carry, and is easily damaged.
Method used
The system employs an electromagnetic folding wing mechanism, including a wing frame, wing membrane, and drive assembly. The folding and unfolding of the wing are driven by electromagnetic force, and the automatic locking of the wing is achieved using a friction self-locking structure.
Benefits of technology
The aircraft automatically folds after landing or when it is no longer in use, reducing space occupation, improving portability, reducing the risk of damage, and has a simple structure, low failure rate, and meets the requirements for lightweight design.
✦ Generated by Eureka AI based on patent content.
Smart Images
Figure CN118270268B_ABST
Abstract
本发明涉及一种用于扑翼微飞行器的电磁式可折叠翼机构及微飞行器，包括机翼架，其包括主支撑杆、副支撑杆和翼骨，主支撑杆的一端与副支撑杆的一端转动连接，翼骨连接于主支撑杆上；翅膜，其覆盖于机翼架上并分别与主支撑杆、副支撑杆及翼骨相连；驱动组件，其包括第一线圈和第二线圈，第一线圈连接于主支撑杆上，第二线圈连接于副支撑杆上。本可折叠翼机构可在飞行器使用完毕后进行机翼的自动折叠收拢，使整个飞行器占用的空间变的更小，提高了整机的便携性，且在飞行器转运的过程中，折叠起来的机翼也更不易发生损坏；同时，整个可折叠翼机构的构造简单，故障率低，安装及维护都较为方便，整体重量轻，能够满足微型飞行器轻量化的要求。
Need to check novelty before this filing date? Find Prior Art