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    • 5. 发明公开
    • Method and apparatus for as-cast seal on turbine blades
    • urb ung ung ung ung ung ung ung ung ung ung ung ung ung
    • EP2092996A1
    • 2009-08-26
    • EP09250238.4
    • 2009-01-29
    • United Technologies Corporation
    • Verner, Carl R.Bullied, Steven J.
    • B22C7/02B22C9/04C30B29/52F01D5/00
    • F01D5/14B22C7/02B22C9/04C30B11/002C30B29/52F01D5/147F05D2230/21Y10T428/12
    • Disclosed is an investment casting mold article (22) comprising a wall for retaining casting material, a cavity defined by the wall, the cavity comprising an airfoil portion (30), a root portion (32) adjacent to the airfoil portion and a labyrinth seal portion (34) extending from the root portion. Disclosed is also a method of casting a gas turbine engine component, the method comprising providing an investment casting mold having a cavity with an airfoil portion, a root portion adjacent to the airfoil portion, and a labyrinth seal portion extending from the root portion, supplying a metallic casting material to the cavity of the investment casting mold, solidifying the metallic casting material to form the gas turbine engine component with a single crystal grain structure, wherein a first feature of the gas turbine engine component defined by the labyrinth seal portion of the investment casting mold has a dimension and a true position defined as-cast.
    • 公开了一种熔模铸造模具制品(22),其包括用于保持铸造材料的壁,由壁限定的空腔,空腔包括翼型部分(30),邻近翼型部分的根部部分(32)和迷宫式密封件 部分(34)从根部延伸。 还公开了一种铸造燃气涡轮发动机部件的方法,该方法包括提供具有翼型部分的空腔的熔模铸造模具,与翼型部分相邻的根部,以及从根部延伸的迷宫式密封部分, 将熔融铸造模具的腔体的金属铸造材料固化成金属铸造材料以形成具有单晶粒结构的燃气涡轮发动机部件,其中由所述熔模铸造模具的迷宫式密封部分限定的燃气涡轮发动机部件的第一特征 熔模铸造模具具有定义为铸造的尺寸和真实位置。