Gas compressor end sealing structure of turbocharger

The utility model discloses a gas compressor end sealing structure of a turbocharger. The gas compressor end sealing structure comprises a bearing body, a turbine rotating shaft which is transversely distributed is arranged in the bearing body; a gas compressor impeller, a shaft sealing sleeve and a thrust spacer sleeve are mounted on the radial outer wall of the turbine rotating shaft; an oil sealing cover and an oil baffle plate are mounted on the radial outer side of the sealing sleeve in a surrounding manner; a thrust bearing plate is mounted on the radial outer side of the left end of the thrust spacer sleeve; the radial outer side face of the left end of the shaft sealing sleeve is provided with a plurality of pressing end sealing ring arrangement grooves used for installing pressing end sealing rings. A first oil storage space is formed between the right side of the upper part of the oil baffle plate and the left side of the upper part of the thrust bearing plate; a second oil storage space is arranged