書誌事項
- タイトル別名
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- J1030101 Rotordynamic Characteristics of Segmented Seal under Whirling Motion
説明
Rocket turbopump is high-speed, high-power turbomachinery that has often suffered from rotor vibration problems. A circumferential hydrodynamic segmented seal (segment seal) is often applied to completely separate the turbine from the pump in the rocket turbopump. It is important to elucidate the effect of the rotordynamic fluid force of the segment seal on the rotor vibration. However, the effect has never been examined. The purpose of this study is to clarify the rotordynamic characteristics of the segment seal and the impact of this force on rotor vibration. The experimental results of the rotordynamic fluid force of the segment seal under whirling motion of the rotor are reported in this paper. Experiments were conducted by using the rotordynamic test stand of JAXA (JARTS) with active magnetic bearings. It was found that the rotordynamic fluid force of the segment seal has positive influence for stability of the rotor because the radial forces had a restoring effect and the tangential forces had a damping effect. The damping effect will be generated by the friction force on the secondary sealing surface and the squeeze effect.
収録刊行物
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- 年次大会
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年次大会 2015 (0), _J1030101--_J1030101-, 2015
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001205844196736
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- NII論文ID
- 110010049011
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- ISSN
- 24242667
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
- OpenAIRE
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- 抄録ライセンスフラグ
- 使用不可