发明名称 Integrated fluidic CD nozzle for gas turbine engine
摘要 An exhaust nozzle for a gas turbine engine includes converging and diverging nozzles joined together at a throat and attached to a frame. An injection slot is disposed at the throat in flow communication with a transition duct for channeling injection air therethrough as controlled by an injection valve for fluidically varying throat area for exhaust gases discharged through the exhaust nozzle.
申请公布号 US6021637(A) 申请公布日期 2000.02.08
申请号 US19970939799 申请日期 1997.09.29
申请人 GENERAL ELECTRIC COMPANY 发明人 SCAVO, STEVEN
分类号 F02K1/30;(IPC1-7):F02K1/30 主分类号 F02K1/30
代理机构 代理人
主权项
地址