发明名称 |
Primary nozzle with chevrons for bypass turboreactor engine of an aircraft and aircraft with such a nozzle |
摘要 |
<p>The pipe has an internal skin (2) inside which circulates a primary air flow (FP) and which comprises chevrons (4), at an external end. An external skin (3) partially surrounds the internal skin and along which flows a secondary air flow (FS). The external skin is movable along the internal skin. A sliding device (5) is placed between the internal skin and the external skin. An independent claim is also included for an aircraft with turbofan engine.</p> |
申请公布号 |
EP1580419(A1) |
申请公布日期 |
2005.09.28 |
申请号 |
EP20050300221 |
申请日期 |
2005.03.24 |
申请人 |
AIRBUS FRANCE |
发明人 |
FEUILLARD, PHILIPPE;HEMEURY, PHILIPPE;GERRI, CHRISTIAN |
分类号 |
F02K1/48;(IPC1-7):F02K1/48 |
主分类号 |
F02K1/48 |
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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