发明名称 STRUCTURE OF RADIAL TURBINE SCROLL AND BLADES
摘要 PURPOSE: Structure of a radial turbine scroll and blades is provided to improve the turbine efficiency by reducing flow loss of the turbine blade and suppressing increase in a loss of a scroll passage. CONSTITUTION: In structure of a radial turbine scroll(4) and turbine blades(3), an actuating gas flows in the radial direction into the blades of a turbine rotor disposed inside the scroll through the scroll formed in a turbine casing(1), and the actuating gas is exhausted in the axial direction after rotating the turbine rotor. A scroll width ratio between the width(delta R) in the radial direction and the width(B) in the direction of the rotating axial core(20) ranges from delta R/B=0.3 to 0.7.
申请公布号 KR20030032899(A) 申请公布日期 2003.04.26
申请号 KR20020063963 申请日期 2002.10.18
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 OSAKO KATSUYUKI;MAEKAWA SHOZO;EBISU MOTOKI;UTSUMI RYOJI;MIKOGAMI TAKASHI
分类号 F01D9/06;F01D5/04;F01D5/14;F01D9/02;F01D25/24;F02B39/00;(IPC1-7):F01D9/06 主分类号 F01D9/06
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