| 发明名称 |
DUAL FLOW TURBOSHAFT ENGINE AND IMPROVED HOT FLOW NOZZLE |
| 摘要 |
According to the invention, the hot flow nozzle includes a single skin (14s) conformed for promoting the cold flow (10) circulation when the aircraft including said turboshaft engine is in a cruise flight mode. |
| 申请公布号 |
WO2009004143(A3) |
申请公布日期 |
2009.06.25 |
| 申请号 |
WO2008FR00706 |
申请日期 |
2008.05.22 |
| 申请人 |
AIRBUS FRANCE;CROSTA, FRANCK;PRAT, DAMIEN |
发明人 |
CROSTA, FRANCK;PRAT, DAMIEN |
| 分类号 |
F01D17/10;F01D25/26;F02C9/52;F02K1/38;F02K1/46;F02K3/06;F02K3/075 |
主分类号 |
F01D17/10 |
| 代理机构 |
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代理人 |
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