发明名称 |
AIRCRAFT PROPULSION SYSTEM PROVIDED WITH REVERSE THRUST MEANS |
摘要 |
<p>The invention relates to a propulsion system including a nacelle and, inside said nacelle, a dual flow turbojet engine that itself includes a fan casing (10) in which a fan and a flow-rectifying vane assembly (15) are located. Said propulsion system includes a reverse thrust means (17) that is located between said fan and said vane assembly (15).</p> |
申请公布号 |
WO2011124793(A1) |
申请公布日期 |
2011.10.13 |
申请号 |
WO2011FR50483 |
申请日期 |
2011.03.10 |
申请人 |
AIRCELLE;PITIOT, INGRID;DEZEUSTRE, NICOLAS |
发明人 |
PITIOT, INGRID;DEZEUSTRE, NICOLAS |
分类号 |
F02K1/70 |
主分类号 |
F02K1/70 |
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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