| 发明名称 |
Blended Wing Body Boundary Layer Ingesting Inlet Design Integration |
| 摘要 |
An inlet for a propulsion system has an upper wall and a lower wall and a throat extending between the upper wall and the lower wall. The lower wall has a bump edge located immediately after the throat. |
| 申请公布号 |
US2016144972(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201414295578 |
申请日期 |
2014.06.04 |
| 申请人 |
United Technologies Corporation |
发明人 |
Florea Razvan Virgil;Stucky Mark B. |
| 分类号 |
B64D33/02;B64C39/10 |
主分类号 |
B64D33/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An inlet for a propulsion system comprising:
an upper wall and a lower wall; a throat extending between said upper wall and said lower wall; and said lower wall having a bump edge located downstream of said throat. |
| 地址 |
Hartford CT US |
