发明名称 |
CHEVRON-TYPE PRIMARY EXHAUST NOZZLE FOR AIRCRAFT TURBOFAN ENGINE, AND AIRCRAFT COMPRISING SUCH A NOZZLE |
摘要 |
A primary exhaust nozzle for a turbofan engine of the double, separated air-flow type for aircraft comprises: an inner coat, within which there circulates a primary air flow (FP), comprising chevrons at an external end and an outer coat at least partially surrounding the inner coat and along which there flo ws a secondary air flow (FS), the outer coat being mobile along the inner coat. Also disclosed is an aircraft comprising such an exhaust nozzle.</SDOAB >
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申请公布号 |
CA2501766(C) |
申请公布日期 |
2008.06.10 |
申请号 |
CA20052501766 |
申请日期 |
2005.03.21 |
申请人 |
AIRBUS FRANCE |
发明人 |
HEMEURY, PHILIPPE;GERRI, CHRISTIAN;FEUILLARD, PHILIPPE |
分类号 |
F02K1/09;B64D33/04;F02K1/34;F02K1/38;F02K1/40;F02K1/48 |
主分类号 |
F02K1/09 |
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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