Turbine component cooling holes
    51.
    发明授权

    公开(公告)号:US10443396B2

    公开(公告)日:2019-10-15

    申请号:US15180553

    申请日:2016-06-13

    Abstract: A turbine component includes an internal surface, an external surface and a cooling hole. The cooling hole includes an inlet disposed on the internal surface, an outlet disposed on the external surface and a flow passage in fluid communication between the inlet and outlet. The flow passage includes a metering section extending from the inlet to a metering end, a diffusion zone extending from the metering end to the outlet, and a hooded region defined by a portion of the diffusion zone covered by a hood. The cooling hole also includes a vane extending across the flow passage, wherein a portion of the vane is disposed within the hooded region.

    Component for a gas turbine engine with a film hole

    公开(公告)号:US10094226B2

    公开(公告)日:2018-10-09

    申请号:US14938261

    申请日:2015-11-11

    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.

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