| 发明名称 |
AIRCRAFT |
| 摘要 |
An aircraft including trailing edge flaps, a wing mounted propulsor positioned such that the flaps are located in a slipstream of the first propulsor in use when deployed. The aircraft further including a thrust vectorable propulsor configured to selectively vary the exhaust efflux vector of the propulsor in at least one plane. The thrust vectorable propulsor includes a ducted fan configurable between a first mode, in which the fan provides net forward thrust to the aircraft, and a second mode in which the fan provides net drag to the aircraft. The fan is positioned to ingest a boundary layer airflow in use when operating in the first mode. |
| 申请公布号 |
US2016332741(A1) |
申请公布日期 |
2016.11.17 |
| 申请号 |
US201615135040 |
申请日期 |
2016.04.21 |
| 申请人 |
ROLLS-ROYCE plc |
发明人 |
MOXON Matthew |
| 分类号 |
B64D33/02;B64C11/00;B64D33/04;B64D27/10;B64D29/04;B64C3/50;B64D27/24 |
主分类号 |
B64D33/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising:
a thrust vectorable propulsor configured to selectively vary the exhaust efflux vector of the propulsor in at least one plane and configurable between a first mode, in which the thrust vectorable propulsor provides net forward thrust to the aircraft, and a second mode in which the thrust vectorable propulsor provides net drag to the aircraft, the thrust vectorable propulsor being positioned to ingest a boundary layer airflow in use when operating in the first mode. |
| 地址 |
London GB |
