| 发明名称 |
PASSIVE CONTROL FIN STOPS FOR AIR LAUNCHED BOOSTED (TWO STAGE) HIGH SPEED VEHICLES |
| 摘要 |
A temporary control fin stop system employs a housing coupled to a vehicle. At least one tang is coupled to the housing and positioned to engage a trailing edge of a fin. The tang is ablatively erodible at a predetermined temperature induced by a flight profile of the vehicle to allow unconstrained motion of the fin. |
| 申请公布号 |
US2015247712(A1) |
申请公布日期 |
2015.09.03 |
| 申请号 |
US201414170143 |
申请日期 |
2014.01.31 |
| 申请人 |
The Boeing Company |
发明人 |
Won Ben YoungSon;Luke Marvin;Ortega Daniel Madrid;Blevins Creed E. |
| 分类号 |
F42B10/02;F42B15/10;F42B33/00;F42B15/01 |
主分类号 |
F42B10/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A temporary control fin stop comprising:
a housing coupled to a vehicle; at least one tang coupled to the housing and positioned to engage a trailing edge of a fin, said tang ablatively erodible at a predetermined temperature induced by a flight profile of the vehicle. |
| 地址 |
Chicago IL US |
