发明名称 |
ENGINE PYLON COMPRISING A VORTEX GENERATOR, AND METHOD FOR THE PRODUCTION THEREOF |
摘要 |
<p>The invention relates to a method for manufacturing an engine pylon (7) to be mounted between an engine (1) and an aircraft wing (6), said method comprising: mounting a pylon box (8) around a main structure (9), the box having a substantially oblong shape along which an air boundary layer (C) is formed while in flight; mounting at least one vortex generator (2) onto the pylon box such that a thickness (e) of the boundary layer is changed; and previously determining the shape of the pylon on the basis of the changed thickness of the boundary layer and the position of the vortex generators.</p> |
申请公布号 |
EP2496472(B1) |
申请公布日期 |
2014.03.05 |
申请号 |
EP20100787857 |
申请日期 |
2010.10.27 |
申请人 |
AIRBUS OPERATIONS (S.A.S.) |
发明人 |
BEDOIN, STEVE;BONNAUD, CYRIL |
分类号 |
B64C7/02;B64C23/06;B64D29/02 |
主分类号 |
B64C7/02 |
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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