| 发明名称 |
Gas turbine engine system and corresponding method for controlling a bypass airflow |
| 摘要 |
<p>A variable fan nozzle for use in a gas turbine engine includes a nozzle section, such as an inflatable bladder, associated with a fan bypass passage for conveying a bypass airflow. The nozzle section has an internal fluid pressure that is selectively variable to influence the bypass airflow.</p> |
| 申请公布号 |
EP2064433(B1) |
申请公布日期 |
2013.11.20 |
| 申请号 |
EP20060816750 |
申请日期 |
2006.10.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LEVASSEUR, GLENN |
| 分类号 |
F02K1/08;F02K1/10;F02K1/12 |
主分类号 |
F02K1/08 |
| 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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