A microbearing tester driven by an air turbine of 10mm diameter has been developed, and successfully used to test hydroinertia gas bearings with a shaft of 4mm diameter. The effects of bearing gas pressure conditions and bearing length to diameter ratio (LD) on the maximum achievable rotation speed were investigated. The maximum rotation speed of 890,000rpm, which corresponds to the DN number (the product of a shaft diameter in millimeter and a rotation speed in rpm) of 3,560,000, was achieved. At 890,000rpm, the tip speed of the turbine reaches approximately 470ms. Using the bearing system developed, the turbo components of a 100W class gas turbine and an air pump for 1kW class fuel cells can be tested.

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