发明名称 |
Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion |
摘要 |
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. |
申请公布号 |
US8109466(B2) |
申请公布日期 |
2012.02.07 |
申请号 |
US20080144368 |
申请日期 |
2008.06.23 |
申请人 |
ATEN MICHAEL RAY;CRAWFORD SARA CHRISTINE;ROHR, INC. |
发明人 |
ATEN MICHAEL RAY;CRAWFORD SARA CHRISTINE |
分类号 |
F02K1/54 |
主分类号 |
F02K1/54 |
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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