REFRACTORY METAL CORE
    6.
    发明专利

    公开(公告)号:CA2484570A1

    公开(公告)日:2005-04-15

    申请号:CA2484570

    申请日:2004-10-13

    Abstract: A casting system for forming a gas turbine engine component is provided. T he casting system, in a first embodiment, comprises a shaped refractory metal sheet having a plurality of features for forming a plurality of film cooling passages, whic h features are formed from refractory metal material bent out of the sheet. The casting system for forming a gas turbine engine component in a second embodiment comprises a metal wall having an airfoil shape and a refractory metal core adjacent the metal wall and having a shape corresponding to the shape of the metal wall.

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