发明名称 GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE
摘要 A nozzle section of a gas turbine engine includes a regulator system in fluid communication with a secondary flow duct and a tertiary flow duct to selectively regulate communication of secondary airflow into the tertiary flow duct.
申请公布号 US2010043393(A1) 申请公布日期 2010.02.25
申请号 US20080193822 申请日期 2008.08.19
申请人 ZAMORA SEAN P;MURPHY MICHAEL JOSEPH 发明人 ZAMORA SEAN P.;MURPHY MICHAEL JOSEPH
分类号 F02K3/075;F01D17/14 主分类号 F02K3/075
代理机构 代理人
主权项
地址