Hydroinertia Gas Bearing System to Achieve 470m∕s Tip Speed of 10mm-Diameter Impellers

Author:

Tanaka Shuji1,Esashi Masayoshi1,Isomura Kousuke2,Hikichi Kousuke3,Endo Yuki3,Togo Shinichi3

Affiliation:

1. Department of Nanomechanics, Tohoku University, 6-6-01 Aza Aoba, Aramaki, Aoba-ku, Sendai, Miyagi 980-8579, Japan

2. Research & Engineering Division, Engine Technology Department, Aero-Engine & Space Operations, Ishikawajima-Harima Heavy Industries Co. Ltd., 3-5-1 Mukodai-cho, Nishi-Tokyo, Tokyo 188-8555, Japan

3. Department of Mechanical Engineering, Tohoku-Gakuin University, 1-13-1 Chuo, Tagajo, Miyagi 985-0873, Japan

Abstract

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 (L∕D) 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 470m∕s. 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.

Publisher

ASME International

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

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