发明名称 Gas turbine engine with variable area fan nozzle
摘要 <p>A nozzle section of a gas turbine engine includes a regulator system (50) in fluid communication with a secondary flow duct (40) and a tertiary flow duct (60) to selectively regulate communication of secondary airflow (B) into the tertiary flow duct (60).</p>
申请公布号 EP2157305(A2) 申请公布日期 2010.02.24
申请号 EP20090251654 申请日期 2009.06.26
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ZAMORA, SEAN P.;MURPHY, MICHAEL JOSEPH
分类号 F02K1/42;F02K1/46;F02K1/82;F02K3/075;F02K3/077 主分类号 F02K1/42
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