A high-speed rotor shaft structure comprises a rotor, radial foil bearings, thrust foil bearings, support end covers, a shell and
clutch bearing assemblies, the rotor is connected with the support end covers through the radial foil bearings, the thrust foil bearings and the
clutch bearing assemblies, and the rotor is provided with radial
foil bearing mounting shaft sections, thrust
foil bearing mounting grooves and
clutch bearing
assembly mounting seats at both ends; the support end covers are provided with radial
foil bearing mounting holes, thrust foil bearing mounting end faces and clutch bearing
assembly mounting shaft sections. The application can be used for high-speed motor rotors or
aviation high-speed shafts, and is supported by ball bearings at
low speed and supported by foil bearings at high speed, so that starting is stable, friction is not generated at high speed,
heat generation is reduced,
lubrication system requirements are lowered, and environmental
pollution is reduced; the application is used in frequent start-stop occasions, reduces friction
heat generation and
coating wear of the foil bearings, and prolongs service life.