Development ofsmall-sized high speed aerodynamic bearings for micro turbo-machines
| Project/Area Number |
23760140
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| Research Category |
Grant-in-Aid for Young Scientists (B)
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| Allocation Type | Multi-year Fund |
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| Research Field |
Design engineering/Machine functional elements/Tribology
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| Research Institution | Tokyo University of Science |
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Principal Investigator |
SOMAYA Kei 東京理科大学, 工学部, 助教 (70581429)
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| Project Period (FY) |
2011 – 2012
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| Project Status |
Completed (Fiscal Year 2012)
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| Budget Amount *help |
¥3,120,000 (Direct Cost: ¥2,400,000、Indirect Cost: ¥720,000)
Fiscal Year 2012: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2011: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000)
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| Keywords | 機械要素 / 設計工学 / 動圧軸受 / 気体軸受 / フォイル軸受 / 高速安定性 / 動圧気体軸受 |
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| Research Abstract |
In order to realize aerodynamic bearings which can stably operate at more than 1Mrpm, we proposed new-type aerodynamic foil journal bearings. We investigated the high-speed stability of the proposed foil bearings, and it was confirmed that the rotor supported by the proposed foil bearings can rotate at more than 700krpm. In addition, The foil thrust bearing was manufactured and we investigated the static characteristics of the foil thrust bearing. As a result, we confirmed that the foil thrust bearing has the maximum load capacity of 4.9N at 350krpm.
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Report
(3 results)
Research Products
(6 results)
