| 发明名称 |
SCHUBDÜSENANORDNUNG FÜR EIN LUFTFAHRZEUG |
| 摘要 |
An engine nozzle arrangement for an aircraft comprises a nozzle (18) for hot exhaust gases, and a shroud (20) for the stream of hot exhaust gases emerging from the exhaust nozzle. The shroud includes an intake for a boundary layer of air for cooling the stream of exhaust gases. |
| 申请公布号 |
DE60009701(D1) |
申请公布日期 |
2004.05.13 |
| 申请号 |
DE2000609701 |
申请日期 |
2000.07.05 |
| 申请人 |
BAE SYSTEMS PLC, LONDON |
发明人 |
WHAITES, COLIN;HOUSE, PETER RICHARD;BROWN, ROBERT |
| 分类号 |
F02K1/82;B64C15/02;B64D33/04;F02K1/11;F02K1/12;F02K1/38;F02K1/60;F02K1/62;F02K1/78 |
主分类号 |
F02K1/82 |
| 代理机构 |
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代理人 |
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