Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing
    1.
    发明授权
    Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing 有权
    内部支撑的翼型和在制造过程中内部支撑中空翼型的方法

    公开(公告)号:US08240999B2

    公开(公告)日:2012-08-14

    申请号:US12415307

    申请日:2009-03-31

    摘要: A hollow airfoil and a method for manufacturing a hollow airfoil is provided. The method includes the steps of: providing a first airfoil portion, which first portion has a wall with an interior surface and an exterior surface, and one or more ribs extending out from the interior surface; providing a second airfoil portion having a wall with an interior surface and an exterior surface; wherein the first airfoil portion and the second airfoil portion have mating geometries in which the one or more ribs extend between the interior surfaces of the walls of the first and second airfoil portion to form at least one internal cavity defined by the interior surface of the first portion wall, one or more of the ribs, and the interior surface of the second portion wall, and wherein the airfoil includes at least one exterior port disposed in one of the first airfoil portion or the second airfoil portion, or is formed between the first and second airfoil portions, which at least one exterior port is in fluid communication with the at least one cavity; disposing a support material within the at least one internal cavity allowing the support material to be in contact with the one or more ribs, which support material is operative to structurally support the one or more ribs; attaching the first and second airfoil portions together; and removing the support material from the at least one internal cavity through the at least one exterior port.

    摘要翻译: 提供了一种中空翼型件和一种制造中空翼型件的方法。 该方法包括以下步骤:提供第一翼型部分,其第一部分具有带有内表面和外表面的壁,以及从内表面延伸出的一个或多个肋; 提供具有带有内表面和外表面的壁的第二翼型部分; 其中所述第一翼型部分和所述第二翼型部分具有配合几何形状,其中所述一个或多个肋在所述第一和第二翼型部分的壁的内表面之间延伸,以形成由所述第一翼型部分和所述第二翼型部分的内表面限定的至少一个内部空腔 部分壁,一个或多个肋和第二部分壁的内表面,并且其中所述翼型包括设置在第一翼型部分或第二翼型部分之一中的至少一个外部端口,或者形成在第一部分壁之间 和第二翼型部分,其至少一个外部端口与所述至少一个空腔流体连通; 将支撑材料设置在所述至少一个内部空腔内,以允许所述支撑材料与所述一个或多个肋接触,所述支撑材料可操作以在结构上支撑所述一个或多个肋; 将第一和第二翼面部分连接在一起; 以及通过所述至少一个外部端口从所述至少一个内部空腔移除所述支撑材料。

    INTERNALLY SUPPORTED AIRFOIL AND METHOD FOR INTERNALLY SUPPORTING A HOLLOW AIRFOIL DURING MANUFACTURING
    2.
    发明申请
    INTERNALLY SUPPORTED AIRFOIL AND METHOD FOR INTERNALLY SUPPORTING A HOLLOW AIRFOIL DURING MANUFACTURING 有权
    内部支持的空气动力和在制造过程中内部支撑空中飞行器的方法

    公开(公告)号:US20100247322A1

    公开(公告)日:2010-09-30

    申请号:US12415307

    申请日:2009-03-31

    IPC分类号: F01D5/18 B23P15/04

    摘要: A hollow airfoil and a method for manufacturing a hollow airfoil is provided. The method includes the steps of: providing a first airfoil portion, which first portion has a wall with an interior surface and an exterior surface, and one or more ribs extending out from the interior surface; providing a second airfoil portion having a wall with an interior surface and an exterior surface; wherein the first airfoil portion and the second airfoil portion have mating geometries in which the one or more ribs extend between the interior surfaces of the walls of the first and second airfoil portion to form at least one internal cavity defined by the interior surface of the first portion wall, one or more of the ribs, and the interior surface of the second portion wall, and wherein the airfoil includes at least one exterior port disposed in one of the first airfoil portion or the second airfoil portion, or is formed between the first and second airfoil portions, which at least one exterior port is in fluid communication with the at least one cavity; disposing a support material within the at least one internal cavity allowing the support material to be in contact with the one or more ribs, which support material is operative to structurally support the one or more ribs; attaching the first and second airfoil portions together; and removing the support material from the at least one internal cavity through the at least one exterior port.

    摘要翻译: 提供了一种中空翼型件和一种制造中空翼型件的方法。 该方法包括以下步骤:提供第一翼型部分,其第一部分具有带有内表面和外表面的壁,以及从内表面延伸出的一个或多个肋; 提供具有带有内表面和外表面的壁的第二翼型部分; 其中所述第一翼型部分和所述第二翼型部分具有配合几何形状,其中所述一个或多个肋在所述第一和第二翼型部分的壁的内表面之间延伸,以形成由所述第一翼型部分和所述第二翼型部分的内表面限定的至少一个内部空腔 部分壁,一个或多个肋和第二部分壁的内表面,并且其中所述翼型包括设置在第一翼型部分或第二翼型部分之一中的至少一个外部端口,或者形成在第一部分壁之间 和第二翼型部分,其至少一个外部端口与所述至少一个空腔流体连通; 将支撑材料设置在所述至少一个内部空腔内,以允许所述支撑材料与所述一个或多个肋接触,所述支撑材料可操作以在结构上支撑所述一个或多个肋; 将第一和第二翼面部分连接在一起; 以及通过所述至少一个外部端口从所述至少一个内部空腔移除所述支撑材料。

    MELTING UNIT FOR A DIE CASTING SYSTEM
    5.
    发明申请
    MELTING UNIT FOR A DIE CASTING SYSTEM 审中-公开
    炼油机组用于铸造系统

    公开(公告)号:US20120111523A1

    公开(公告)日:2012-05-10

    申请号:US12940080

    申请日:2010-11-05

    CPC分类号: B22D17/28

    摘要: A die casting system includes a die, a shot tube, a shot tube plunger and a melting unit. The die includes a plurality of die components that define a die cavity. The shot tube is in fluid communication with the die cavity. A shot tube plunger is moveable within the shot tube to communicate a charge of material into the die cavity. The melting unit is positioned relative to the die and includes a bottom portion having an opening for selectively releasing a charge of material through the bottom portion.

    摘要翻译: 压铸系统包括模具,射出管,射出管柱塞和熔化单元。 模具包括限定模腔的多个模具部件。 射出管与模腔流体连通。 喷射管柱塞可在射出管内移动以将材料的进料传送到模腔中。 熔化单元相对于模具定位,并且包括底部,其具有用于选择性地释放通过底部部分的材料的填充物的开口。