The invention relates to a pure radial
supersonic speed micro
turbine structure with an
air bearing. The structure is characterized in that air flow enters a
turbine stator runner (5) from the radial direction, and then the flowing direction of the air flow in a
turbine is always kept in the radial direction; according to a
stator part,
stator blades (2), an upper casing (1) and a lower casing (4) form a contraction and release flow channel, and the cross section area of a
throat part of the flow channel is equal to the critical area of designed flow, so that
airflow is accelerated to
supersonic speed; an inlet blade of a rotor
impeller (3) is in a blunt end shape to block part of the flow area so as to adapt to the small flow design requirement of the micro turbine; and
dynamic pressure grooves (7) are engraved in the back face and the edge of the rotor
impeller (3) and matched with the lower casing (4) to form a
dynamic pressure air bearing runner (6), and when the rotating speed of the turbine reaches a design value, air in the
dynamic pressure grooves provides supporting force due to the
viscous effect, and the thrust and radial bearing effects are achieved. The structure can realize expansion acting of small-flow high-pressure gas and has the characteristics of being compact in structure, extremely high in rotating speed, small in required flow, capable of acting by using
cold air, high in
expansion ratio and strong in acting capacity.