发明名称 Methods and apparatus for controlling air flow within a pulse detonation engine
摘要 A flow control device for use with a pulse detonation chamber including an inlet coupled in flow communication with a source of compressed air. The inlet extends at least partially into the chamber to facilitate controlling air flow into the chamber. The device also includes a body portion extending downstream from and circumferentially around the inlet, wherein the body portion is positioned in flow communication with the inlet.
申请公布号 US2007180833(A1) 申请公布日期 2007.08.09
申请号 US20060348869 申请日期 2006.02.07
申请人 GENERAL ELECTRIC COMPANY 发明人 RASHEED ADAM;DEAN ANTHONY J.
分类号 F02C5/00 主分类号 F02C5/00
代理机构 代理人
主权项
地址