The invention belongs to the technical field of aero-engines, and discloses a centrifugal
impeller and an aero-engine rotor. The centrifugal
impeller comprises an
impeller body, a centrifugal switching section and a
fastener; a connecting part is arranged on the side, close to the gas
turbine disc, of the impeller body, the centrifugal switching section comprises an impeller switching part and a
turbine switching part which are fixedly connected, an annular spigot is formed in the side, close to the impeller body, of the impeller switching part, and outer teeth are arranged on the outer side of the impeller switching part in the circumferential direction; the connecting part is fixedly connected with the impeller switching part through a
fastener, the connecting part is located in the spigot, a positioning surface for radially positioning the impeller body is arranged in the spigot, and end teeth are arranged at the end, away from the impeller body, of the
turbine switching part. The centrifugal impeller is provided with the centrifugal switching section, the impeller body and the centrifugal switching section can be made of different materials, the centrifugal switching section is made of high-temperature
alloy, the abrasion resistance of the rear end teeth of the centrifugal impeller can be effectively improved, end tooth bonding is prevented or relieved, and the problems of end tooth bonding and disc body abrasion of the centrifugal impeller are solved.