发明名称 Passively driven acoustic jet controlling boundary layers
摘要 Existing pressure oscillations created by axial or centrifugal fans in a diverging shroud are utilized to power a passive, acoustic jet, the nozzle of which directs high momentum flux gas particles essentially tangentially into the boundary layer of the flow in a diffuser, or a duct, the fluid particles in the resonant chamber of the passive acoustic jet being replenished with low momentum flux particles drawn from the fluid flow in a direction normal to the surface, thereby to provide a net time averaged flow of increased momentum flux particles to defer, even eliminate, the onset of boundary layer separation in the diffuser or duct. The passive acoustic jet is used in the vicinity of fan blade tips to alleviate undesirable flow effects in the tip region, such as leakage.
申请公布号 US6379110(B1) 申请公布日期 2002.04.30
申请号 US19990257563 申请日期 1999.02.25
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MCCORMICK DUANE C.;LORD WESLEY K.
分类号 B64C23/00;F01D11/08;F01D11/10;(IPC1-7):F01D25/04 主分类号 B64C23/00
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