A rotor blade for an axial flow turbine is provided to improve efficiency of a turbine and thrust by enhancing the shape of a leading edge of a blade. A rotor blade for an axial flow turbine, comprises an intrados(2) for producing positive pressure between a leading edge and a trailing edge; and an extrados(1) for producing negative pressure between the leading edge and the trailing edge. The intrados and the extrados at the leading edge are chamfered so that the intrados and the extrados are connected through a plane(3). The angle between the chamfered intrados and the chamfered extrados is smaller than the angle between the chamfered intrados and a vertical plane including the leading edge.
申请公布号
KR20070006341(A)
申请公布日期
2007.01.11
申请号
KR20050061596
申请日期
2005.07.08
申请人
PUSAN NATIONAL UNIVERSITY INDUSTRY-UNIVERSITY COOPERATION FOUNDATION
发明人
KIM, KUI SOON;JEONG, SOO IN;CHO, JONG JAE;SHIN, BONG GUN;YUN, WON GEUN;KWAK, YOUNG JAE