Clock turbine airfoil cooling
    112.
    发明授权
    Clock turbine airfoil cooling 失效
    时钟涡轮机翼型冷却

    公开(公告)号:US06402458B1

    公开(公告)日:2002-06-11

    申请号:US09640357

    申请日:2000-08-16

    CPC classification number: F01D25/12 F01D5/142 Y02T50/673 Y02T50/675

    Abstract: A turbine includes three rows of airfoils which receive in sequence hot combustion gases during operation. The third row airfoils are clocked circumferentially relative to the first row airfoils for bathing the third row airfoils with relatively cool wakes discharged from the first row airfoils during the hottest running condition of the gas turbine engine being powered. The third row airfoils therefore avoid the hottest temperature of the combustion gases for reducing the cooling requirements thereof.

    Abstract translation: 涡轮机包括三排机翼,其在操作期间依次接受热燃烧气体。 第三排翼型件相对于第一排翼型件周向地进行计时,用于在燃气涡轮发动机供电的最热的运行状态期间洗涤第三排翼型件,其具有从第一排翼型件排出的相对较冷的骤冷件。 因此,第三排翼型件避免了燃烧气体的最高温度以降低其冷却要求。

Patent Agency Ranking