A bearing device for a turbocharger, comprising: a bearing housing interposed between a turbine housing and a compressor housing of a turbocharger for pressurizing supply air to a combustion chamber of an internal combustion engine; a rotor shaft of a turbine rotor arranged to pass through the bearing housing; and a first floating bush bearing interposed between the bearing housing and the rotor shaft, comprising a first floating bush (19, 35) and being disposed on a compressor housing side, the first floating bush (19, 35) having an oil supply hole (19a, 35c) which interconnects an outer peripheral surface (19b, 27b, 30a, 35a) and an inner peripheral surface (19c, 35b) and being configured to supply lubricating oil from the bearing housing to the outer peripheral surface (19b, 35a) and the inner peripheral surface (19c, 35b); a second floating bush bearing having the same configuration as the first floating bush bearing, comprising a second floating bush and being disposed on a turbine housing side, wherein each of the first (19, 35) and second floating bushes is configured so that an inner bearing width Li is formed smaller than an outer bearing width Lo at the same ratio, wherein the outer peripheral surface (19b, 35a) of the first and second floating bushes (19, 35; 20) has a low friction treatment, characterized in that the low friction treatment is formed by a pair of edge grooves (35d, 35d) formed over the entire circumference of the outer peripheral surface on both sides of the oil supply hole of the outer peripheral surface in the bearing width direction, and a transverse groove provided for each oil supply hole so that the pair of edge grooves (35d, 35d) communicate with the oil supply hole, the oil supply hole being provided at the center of the outer peripheral surface of the first and second floating bushes in the bearing width direction. a bearing housing interposed between a turbine housing and a compressor housing of a turbocharger for pressurizing supply air to a combustion chamber of an internal combustion engine; a rotor shaft of a turbine rotor arranged to pass through the bearing housing; and a first floating bush bearing interposed between the bearing housing and the rotor shaft, comprising a first floating bush (19, 35) and being disposed on a compressor housing side, the first floating bush (19, 35) having an oil supply hole (19a, 35c) which interconnects an outer peripheral surface (19b, 27b, 30a, 35a) and an inner peripheral surface (19c, 35b) and being configured to supply lubricating oil from the bearing housing to the outer peripheral surface (19b, 35a) and the inner peripheral surface (19c, 35b); a second floating bush bearing having the same configuration as the first floating bush bearing, comprising a second floating bush and being disposed on a turbine housing side, wherein each of the first (19, 35) and second floating bushes is configured so that an inner bearing width Li is formed smaller than an outer bearing width Lo at the same ratio, wherein the outer peripheral surface (19b, 35a) of the first and second floating bushes (19, 35; 20) has a low friction treatment, characterized in that the low friction treatment is formed by a pair of edge grooves (35d, 35d) formed over the entire circumference of the outer peripheral surface on both sides of the oil supply hole of the outer peripheral surface in the bearing width direction, and a transverse groove provided for each oil supply hole so that the pair of edge grooves (35d, 35d) communicate with the oil supply hole, the oil supply hole being provided at the center of the outer peripheral surface of the first and second floating bushes in the bearing width direction.