发明名称 Multistage turbine with single rotor blade row, and gas turbine using same
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.
申请公布号 EP1710396(A2) 申请公布日期 2006.10.11
申请号 EP20060006647 申请日期 2006.03.30
申请人 JAPAN AEROSPACE EXPLORATION AGENCY 发明人 IWASE, SHIKI;SAITO, YOSHIO
分类号 F01D1/12 主分类号 F01D1/12
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