HEAT DISSIPATION SYSTEM WITH BOUNDARY LAYER DISRUPTION
摘要
<p>A heat dissipation system that includes a structure (122) having a surface (124) with a cavity (126) recessed on the surface (124). A wing (140) or channel causes a vortex to occur in the cavity (126). Destabilizers (206), such as projections or recesses (200) are disposed on the sidewall (132) of the cavity (126) to disrupt the local surface boundary layer (180) that forms in the cavity (126). Alternatively, a plurality of freely moving bead elements (270) are disposed in the cavity to disrupt the local surface boundary layer (180). A cover (270) can be included that prevents the bead elements (270) from exiting the cavity (126).</p>
申请公布号
WO2010048058(A1)
申请公布日期
2010.04.29
申请号
WO2009US61029
申请日期
2009.10.16
申请人
NOVA RESEARCH, INC.;GOVERNMENT OF USA REPRESENTED BY THE SECRETARY OFTHE NAVY AND CHIEF OF NAVAL RESEARCH;KUCHEROV, YAN R.;HUBLER, GRAHAM