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A Study on the Turbopump Rotordynamic Characteristics due to Bearing Housing Structural Flexibility
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베어링 하우징의 구조 유연성에 따른 터보펌프 회전체동역학 특성 연구

논문 기본 정보

Type
Proceeding
Author
Seong Min Jeon (한국항공우주연구원) Suk-Hwan Yoon (한국항공우주연구원) Jinhan Kim (한국항공우주연구원)
Journal
The Korean Society of Propulsion Engineers 한국추진공학회 학술대회논문집 한국추진공학회 2013년도 제40회 춘계학술대회 논문집
Published
2013.5
Pages
388 - 394 (7page)

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A Study on the Turbopump Rotordynamic Characteristics due to Bearing Housing Structural Flexibility
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Abstract· Keywords

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A rotordynamic analysis is performed for a turbopump of 7 ton class liquid rocket engine considering bearing housing structural flexibility. Stiffness and damping characteristics of ball bearings and pump noncontact seals are reflected in a rotordynamic model. A dynamic model of bearing housing with lumped mass and stiffness is also applied to the rotordynamic analysis. Rotor critical speed and onset speed of instability are predicted from synchronous rotor mass unbalance response and complex eigenvalue analyses. The bearing housing structural flexibility effect on rotordynamic characteristics is investigated for the both of bearing loaded and unloaded conditions respectively. From the numerical analysis, it is found that the effect of the housing structural flexibility significantly reduces the rotor critical speed and onset speed of instability.

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ABSTRACT
초록
1. 서론
2. 회전체동역학 모델
3. 수치해석
4. 결론
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UCI(KEPA) : I410-ECN-0101-2014-570-002551071