发明授权
US09194241B2 CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact 有权
CMC涡轮喷嘴适于通过径向接触来支撑金属涡轮内部壳体

CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact
摘要:
A composite material turbine nozzle blade including an airfoil adapted to have a cooling fluid flow through it and extending between a shroud and a root is provided. The shroud is shaped to be attached to one or more turbine casings of a turbomachine and the root is shaped to provide a junction with a turbine internal casing. The root is produced with a loosened texture and includes an external upstream side loosened texture lug and an external downstream side loosened texture lug. The ends of the two external side lugs extend radially relative to the rotation axis of the turbomachine to form a device for supporting and centering the internal casing.
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