Composite Airfoil Assembly for a Turbine Engine

    公开(公告)号:US20240401482A1

    公开(公告)日:2024-12-05

    申请号:US18327172

    申请日:2023-06-01

    Abstract: A composite airfoil assembly for a gas turbine engine. The composite airfoil assembly includes a composite airfoil having opposite pressure and suction sides and opposite leading and trailing edges. The pressure side and the suction side extend axially between the leading edge and the trailing edge. The composite airfoil has a laminate skin that is applied to at least a portion of a core. A first cladding and a second cladding, having adjacent segments, are located on the pressure side or the suction side of the composite airfoil.

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