公开(公告)号：US5735469A

公开(公告)日：1998-04-07

申请号：US653851

申请日：1996-05-28

申请人： Sergio E. Rodriguez ,  James P. Maddox ,  Raymond J. Netzer ,  Alan Z. Ullman

发明人： Sergio E. Rodriguez ,  James P. Maddox ,  Raymond J. Netzer ,  Alan Z. Ullman

IPC分类号： H01S3/0953 ,  B05B7/00

CPC分类号： H01S3/0953

摘要： A compact diffuser for recovering pressure from a supersonic flow with boundary layers. Sharp splicer plates near the wails form boundary layer scoops and separate the flow into an inner coreflow chapel and outer chambers containing small supersonic ejector nobles. The coreflow without boundary layers undergoes a single near-normal shock to recover pressure. The boundary layers are pumped to the recovery pressure in the outer ejector chambers. The subsonic part of the boundary layer flow to the outer chambers can be choked against boundary layer scoop inlet corners to isolate the upstream flow. The leading edge angle of the splicers may be selected to help induce coreflow shocking.

摘要翻译： 用于从具有边界层的超音速流回收压力的紧凑型扩散器。 靠近窗户的尖锐的拼接板形成边界层勺，并将流分离成内芯流道教堂和包含小超音速弹射器贵族的外室。 没有边界层的芯流经历单次接近正常的冲击以恢复压力。 边界层被泵送到外部喷射器室中的恢复压力。 流到外室的边界层的亚音速部分可以被阻塞在边界层勺入口拐角上以隔离上游流。 可以选择捻接器的前缘角以帮助引起芯流冲击。