基本信息:
- 专利标题： PARACHUTE CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
- 申请号：EP16856334.4 申请日：2016-10-14
- 公开(公告)号：EP3362360A1 公开(公告)日：2018-08-22
- 发明人： FATHALLAH, Michel , SWEENEY, Matthew , BASS, Tom , BADDAM, Kranthi , FOGGIA, John R.
- 申请人： Flirtey Holdings, Inc.
- 申请人地址： 1664 N. Virginia MS199 Reno, NV 89557 US
- 专利权人： Flirtey Holdings, Inc.
- 当前专利权人： FLIRTEY HOLDINGS, INC.
- 当前专利权人地址： FLIRTEY HOLDINGS, INC.
- 代理机构： EIP
- 优先权： US201562241572P 20151014; US201662344514P 20160602
- 国际公布： WO2017066662 20170420
- 主分类号： B64D17/80
- IPC分类号： B64D17/80 ; B64C9/32 ; B64C25/56 ; B64C27/08 ; B64D17/00
摘要：
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.
公开/授权文献:
- EP3362360B1 PARACHUTE CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE 公开/授权日：2023-06-14
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 |