| 发明名称 |
Spoiler for an Aircraft Bay |
| 摘要 |
A method for managing an airflow of an aircraft. A spoiler is moved into the airflow passing a bay of the aircraft when the bay is open. The airflow moving relative to the bay is changed to form a desired airflow using louvers physically associated with a frame system in the spoiler. |
| 申请公布号 |
US2016121996(A1) |
申请公布日期 |
2016.05.05 |
| 申请号 |
US201414203636 |
申请日期 |
2014.03.11 |
| 申请人 |
The Boeing Company |
发明人 |
Eveker James Vincent;Huhman Patrick Dale;Crites Cindy Lee |
| 分类号 |
B64C5/12;B64C23/00 |
主分类号 |
B64C5/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus comprising:
a frame system configured to move relative to a bay in an aircraft; and louvers physically associated with the frame system, wherein the louvers are configured to change an airflow moving relative to the bay when the bay is open to form a desired airflow. |
| 地址 |
Chicago IL US |
