| 发明名称 |
S-DUCT FOR A TURBO-JET AIRCRAFT ENGINE |
| 摘要 |
An improved S-duct (10c) for turbo-jet engined aircraft. The present invention allows a high volume of high energy air to traverse the S-duct (10c) at a high pressure recovery ratio. |
| 申请公布号 |
WO9401735(A1) |
申请公布日期 |
1994.01.20 |
| 申请号 |
WO1993US05928 |
申请日期 |
1993.06.21 |
| 申请人 |
THE DEE HOWARD COMPANY |
发明人 |
FINCH, THOMAS, E.;CAVATORTA, ENRICO;PASCHAL, WILLIAM |
| 分类号 |
B64D33/02;(IPC1-7):F64D33/02 |
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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