发明名称 |
Aft cascade ring with flow deflector portion, corresponding thrust reverser cascade assembly and aircraft engine nacelle |
摘要 |
<p>An aircraft engine thrust reverser cascade assembly includes a plurality of circumferentially spaced cascade segments, each cascade segment including a plurality of spaced vanes including an aft-most vane, and an aft end. The cascade assembly also includes an aft cascade ring removably attached to the aft ends of the cascade segments. The aft cascade ring includes a deflector portion that at least partially extends forward of the aft ends of the cascade segments. The deflector portion is configured to at least partially redirect at least a portion of a volume of air as the air outwardly passes between the aft-most vanes and the aft ends of the cascade segments.
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申请公布号 |
EP2138697(A3) |
申请公布日期 |
2011.04.27 |
申请号 |
EP20090007905 |
申请日期 |
2009.06.16 |
申请人 |
ROHR, INC. |
发明人 |
ATEN, MICHAEL RAY;CRAWFORD, SARA CHRISTINE |
分类号 |
F02K1/72;F02K1/62 |
主分类号 |
F02K1/72 |
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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