Mold core and method of forming internal passages in an airfoil
    2.
    发明授权
    Mold core and method of forming internal passages in an airfoil 失效
    模具芯和在翼型中形成内部通道的方法

    公开(公告)号:US4596281A

    公开(公告)日:1986-06-24

    申请号:US414041

    申请日:1982-09-02

    申请人: Thomas H. Bishop

    发明人: Thomas H. Bishop

    CPC分类号: B22C21/14 B22C9/10 B22C9/106

    摘要: An improved core is adapted to extend axially through the central portion of a mold cavity in which an airfoil or other article is formed. The core is used to form cooling passages as the airfoil is cast in the mold cavity. The core has an elongated cantilevered center section which is disposed within a main or base section. A metallic pin member extends from a free end portion of the cantilevered center section of the core to the main section of the core to hold the free end portion of the cantilevered center section against movement relative to the main section.

    摘要翻译: 改进的芯适于轴向延伸穿过其中形成有翼型或其它制品的模腔的中心部分。 当机翼被铸造在模腔中时,芯用于形成冷却通道。 芯部具有细长的悬臂中心部分,其设置在主部分或基部部分内。 金属销构件从芯的悬臂中心部分的自由端部延伸到芯的主要部分,以保持悬臂中心部分的自由端部相对于主要部分的运动。