发明名称 |
Turbojet nacelle and method for controlling separation in a turbojet nacelle |
摘要 |
An aircraft turbojet nacelle comprising blowing means intended to inject a tangential airflow (Ft) into the internal volume (V) of the nacelle, said blowing means being provided in a wall of the air intake of the nacelle in the supersonic area of said air intake. The invention also concerns a method for controlling separation in an aircraft nacelle, wherein a tangential airflow is injected (Ft) into the internal volume (V) of the nacelle in the locally supersonic area of the air intake so as to pull the main airflow (F) into the extension of the inner wall of the nacelle. |
申请公布号 |
US8640986(B2) |
申请公布日期 |
2014.02.04 |
申请号 |
US20080326604 |
申请日期 |
2008.12.02 |
申请人 |
SURPLY THIERRY;BOURDEAU CHRISTOPHE;AIRBUS OPERATIONS SAS |
发明人 |
SURPLY THIERRY;BOURDEAU CHRISTOPHE |
分类号 |
B64D33/02;B64C21/04 |
主分类号 |
B64D33/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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