
基本信息:
- 专利标题: 无人机与降落伞的延时分离机构
- 专利标题(英):Unmanned aerial vehicle and parachute delayed separation mechanism
- 申请号:CN201420574756.2 申请日:2014-09-30
- 公开(公告)号:CN204124372U 公开(公告)日:2015-01-28
- 发明人: 杨友东 , 童月堂 , 钱少明 , 王吉国 , 胡文杰
- 申请人: 浙江工业大学之江学院 , 浙江中杭电子有限公司
- 申请人地址: 浙江省绍兴市柯桥区柯华路958号
- 专利权人: 浙江工业大学之江学院,浙江中杭电子有限公司
- 当前专利权人: 浙江工业大学之江学院,浙江中杭电子有限公司
- 当前专利权人地址: 浙江省绍兴市柯桥区柯华路958号
- 代理机构: 杭州九洲专利事务所有限公司
- 代理人: 张羽振
- 主分类号: B64D17/80
- IPC分类号: B64D17/80
The utility model discloses an unmanned aerial vehicle and parachute delayed separation mechanism which comprises an electromagnet and a locking device. When the locking device is in a locked state, the electromagnet is not electrified, an armature of the electromagnet does not extend outwards, a driving rod and a connecting rod are located on the same straight line, dead point positions of a hinge four-bar mechanism are utilized, and a driven rod bearing the tension of a parachute can not rotate; when the locking device is unlocked, the armature of the electromagnet extends outwards, the driving rod of the hinge four-bar mechanism is pushed to rotate, the dead point positions of the hinge four-bar mechanism are broken, and the joints of an unmanned vehicle and the recycled parachute are switched. The unmanned aerial vehicle and parachute delayed separation mechanism has the advantages that the large tension of the parachute is borne by the driving rod, the connecting rod, the driven rod and other components of the hinge four-bar mechanism, and the bearing capacity is high; the value of thrust outputted by the electromagnet is small, and therefore the appearance sizes and masses of the electromagnet and the delayed separation mechanism can be effectively decreased; the mechanism is simple and practical in structural principle and high in reliability and has large application value.
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64D | 用于与飞机配合或装到飞机上的设备;飞行衣;降落伞;动力装置或推进传动装置的配置或安装 |
------B64D17/00 | 降落伞 |
--------B64D17/80 | .与飞机结合的,例如用于飞机制动的 |