- 专利标题: Multistage turbine with single blade row, and gas turbine using same
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申请号: US11395169申请日: 2006-04-03
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公开(公告)号: US20060222484A1公开(公告)日: 2006-10-05
- 发明人: Shiki Iwase , Yoshio Saito
- 申请人: Shiki Iwase , Yoshio Saito
- 申请人地址: JP Chofu-shi
- 专利权人: JAPAN AEROSPACE EXPLORATION AGENCY
- 当前专利权人: JAPAN AEROSPACE EXPLORATION AGENCY
- 当前专利权人地址: JP Chofu-shi
- 优先权: JP2005-107211 20050404
- 主分类号: F01D1/12
- IPC分类号: F01D1/12
摘要:
In order to desirably prevent leakage of a working fluid from the tip clearance to reduce loss of a heat drop of the working fluid, a first corresponding blade of a second stationary blade row, which corresponds to a first reference blade of a first stationary blade row, is disposed in a position distant by 2L from the position of a lower end of a rotor blade in the direction of movement of the rotor blades when the rotor blade makes the closest approach to a lower end of the first reference blade. It should be noted that L is a value obtained by multiplying the average time T required for the high-pressure working fluid to pass through the rotor blade by the traveling speed U of the rotor blade. On the other hand, a second corresponding blade of the second stationary blade row, which corresponds to a second reference blade of the first stationary blade row, is disposed in a position of a lower end of a rotor blade when the rotor blade makes the closest approach to a lower end of the first reference blade.
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