发明名称 |
Balloon gas release flight termination system |
摘要 |
A control system for terminating flight of a balloon having a balloon envelope is provided. The control system includes a shuttle that has one or more cutting blades. The cutting blades are configured to cut open the balloon envelope. A tubular track is attached to a section of the balloon envelope. This tubular track has a guiding portion arranged to receive and guide the shuttle along the track. The control system includes a type of releasable ballast attached to the shuttle. When the ballast is released, the ballast is configured to move the shuttle along the tubular track in order to cause at least one of the cutting blades to cut open a portion of the balloon envelope. This allows lift gas to escape from the balloon envelope. |
申请公布号 |
US9346531(B1) |
申请公布日期 |
2016.05.24 |
申请号 |
US201414480848 |
申请日期 |
2014.09.09 |
申请人 |
Google Inc. |
发明人 |
Washburn Shane;Capraro Peter Isaac |
分类号 |
B64B1/62 |
主分类号 |
B64B1/62 |
代理机构 |
Lerner, David, Littenberg, Krumholz & Mentlik, LLP |
代理人 |
Lerner, David, Littenberg, Krumholz & Mentlik, LLP |
主权项 |
1. A control system, the control system comprising:
a shuttle having one or more cutting blades, the cutting blades being configured to cut open a balloon envelope; a tubular track attached to a section of the balloon envelope, the tubular track having a guiding portion arranged to receive and guide the shuttle along the tubular track; a ballast attached to the shuttle such that when the ballast is released, the ballast is configured to move the shuttle along the tubular track in order to cause at least one of the cutting blades to cut open a portion of the balloon envelope and allow lift gas to escape from the balloon envelope. |
地址 |
Mountain View CA US |