发明名称 |
Gas turbine engine with variable area fan nozzle and method of operating a variable area fan nozzle |
摘要 |
A nacelle assembly (N) for a bypass gas turbine engine includes a variable area fan nozzle (42) having a first fan nacelle section (52) and a second fan nacelle section (54). The variable area fan nozzle (42) is in communication with a fan bypass flow path (40). The first fan nacelle section (52) defines an intermittent trailing edge (60) which defines a multiple of ports (62) and the second fan nacelle section (54) defines a multiple of doors (66). Each of the multiple of doors (66) matches each of the multiple of ports (62) such that a fan nacelle trailing edge (34S) is continuous when the second fan nacelle section (54) is selectively translated to a closed position relative to the first fan nacelle section (52). |
申请公布号 |
EP2444645(B1) |
申请公布日期 |
2016.05.04 |
申请号 |
EP20110186217 |
申请日期 |
2011.10.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DO, LOGAN H.;KRYSTOWSKI, EDWARD A. |
分类号 |
F02K1/06;F02K1/09;F02K1/38;F02K1/48;F02K1/76;F02K3/06 |
主分类号 |
F02K1/06 |
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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