发明名称 STRUCTURE OF OUTPUT SECTION OF JET PROPULSION ENGINE OR GAS TURBINE
摘要 A tandem blade lattice having characteristics enhanced is provided. In a high pressure ratio blade lattice, inevitable generation of an shock wave is shifted, as much as possible, toward a rear portion of an upper surface of a front bl ade to inhibit separation from a blade surface from being caused by interference of theshock wave and a boundary layer, and boundary layer control is performed such that a speed, a momentum and the like of a jet flowing from a trailing edge of alower surface of the front blade onto an upper surfa ce of a rear blade are regulated to obtain a flow along the upper surface of the rear blade, so that separati on of the boundary layer on the upper surface of the rear blade is restricted to a vic inity of a trailing edge.
申请公布号 CA2208113(C) 申请公布日期 2001.07.10
申请号 CA19972208113 申请日期 1997.06.18
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 HASHIMOTO, KEISUKE
分类号 F01D5/14;F01D9/04;F02K3/04 主分类号 F01D5/14
代理机构 代理人
主权项
地址
您可能感兴趣的专利