发明名称 |
Nacelle assembly for a gas turbine engine comprising a pylon located in the fan bypass flow path with a variable area flow system |
摘要 |
<p>A turbofan engine pylon structure has a fan variable area nozzle defined by a variable area flow system between a pylon intake and a pylon exhaust to selectively adjust a bypass flow through the pylon structure. The variable area flow system changes the physical area and geometry of a pylon nozzle exit area to manipulate the bypass flow by opening and closing an additional flow area of the variable area flow system.</p> |
申请公布号 |
EP2074317(B1) |
申请公布日期 |
2012.03.07 |
申请号 |
EP20060850523 |
申请日期 |
2006.10.12 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BALTAS, CONSTANTINE |
分类号 |
F02K1/30 |
主分类号 |
F02K1/30 |
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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