发明名称 |
A gas turbine engine assembly with a variable area nozzle and a method of controlling this nozzle |
摘要 |
A gas turbine engine system includes a first nozzle section (40a) associated with a gas turbine engine bypass passage (32) and a second nozzle section (40b) that includes a plurality of positions relative to the first nozzle section (40a). In at least one of the positions, there is a gap (64) between the first nozzle section (40a) and the second nozzle section (40b). A movable door (52) between the first nozzle section (40a) and the second nozzle section (40b) selectively opens or closes the gap (64). |
申请公布号 |
EP2050948(A3) |
申请公布日期 |
2012.01.18 |
申请号 |
EP20080253283 |
申请日期 |
2008.10.08 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
STERN, ALFRED M. |
分类号 |
F02K1/72;B64D33/04;F02K1/09;F02K1/62;F02K3/06 |
主分类号 |
F02K1/72 |
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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