The invention discloses a kernel rotor device of an exhaust-gas
turbocharger, comprising a middle casing, a thrust sleeve, a
thrust bearing, an oil baffle, and a shaft gland, wherein a blade wheel is arranged on a
turbine shaft on one end of the shaft gland, the middle casing on the one end of the blade wheel is provided with a chamber, a sealing ring sleeve base is arranged in the chamber, and the sealing ring sleeve base comprises a ring-shaped component which is sealed with the inner walls of the chamber and a
lantern ring which is dynamically sealed by the shaft gland and is arranged on the
turbine shaft. A ring-shaped connecting member is fixedly connected between the ring-shaped component and the
lantern ring, one lateral side of the ring-shaped connecting member which faces the blade wheel is provided with an arc-shaped end face which is relative to the shape of the blade wheel. The original connection between a linking disk and the middle casing is changed into the connection of the middle casing and the sealing ring sleeve to remove the linking disk with
large size, thereby avoiding deformation of the product. The original projection sealing is changed into notch sealing to enlarge the oil return space of the product, and the original screw pressing is changed into a
circlip pressing, thereby providing conveniences for
assembly, easily adopting an automatic
assembly line, and reducing the cost of the product.