| 摘要 |
Cast dual alloy turbine rotor disk and method of forming the same are provided. The disk includes a ring (104) and a blade (106). The ring (104) comprises a superalloy that includes a plurality of elements, and the blade (106) extends from the ring. The blade (106) comprises a non-metallic ceramic matrix composite, and at least one element from the superalloy of the ring (104) is diffused into the non-metallic ceramic matrix composite of the blade. |
