发明名称 BOUNDARY LAYER SEPARATION CONTROL DEVICE, FUEL INJECTOR, AND CONTROL METHOD
摘要 PROBLEM TO BE SOLVED: To provide a stable combustor with high thrust and a combustor control method by providing a backward acute-angle protruding matter on the inner wall of an engine, and turning the recirculating flow (counterflow) from the rear backward by this protruding matter to reduce the interference between the recirculating flow and a main boundary layer to suppress the extension of separation region and improving the thrust by the pressure rise in the back surface of the protruding matter. SOLUTION: A surface A inclined to the downstream side at an angleΘ1 to the main flow is formed in the boundary inter layer (wall surface) that is the subject of separation control and suppression of upstream extension of counterflow region so that the angles of the front and rear walls B and C of a stepped part having the surface A to the main flow areΘ2 andΘ3, respectively. The relation among the anglesΘ1,Θ2 andΘ3 is set and controlled to 0°<1<90°and -90°<Θ2. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004084516(A) 申请公布日期 2004.03.18
申请号 JP20020244834 申请日期 2002.08.26
申请人 JAPAN SCIENCE & TECHNOLOGY CORP;NATIONAL AEROSPACE LABORATORY OF JAPAN 发明人 SUNAMI TETSUHARU;MURAKAMI JUNRO;KUDO KENJI;KODERA MASATOSHI;NISHIOKA MICHIO
分类号 F02K7/14;(IPC1-7):F02K7/14 主分类号 F02K7/14
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