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http://dx.doi.org/10.5293/KFMA.2002.5.3.025

Investigation on the Strength and Vibration Safety of the Oxidizer Turbopump  

Jeon, Seong-Min (한국항공우주연구원 터보기계연구그룹)
Kim, Jin-han (한국항공우주연구원 터보기계연구그룹)
Yang, Soo-Seok (한국항공우주연구원 터보기계연구그룹)
Lee, Dae-Sung (한국항공우주연구원 추진기관연구부)
Publication Information
Abstract
Structural and dynamic analyses of inducer and impeller for an oxidizer turbopump are peformed to investigate the safety level of strength and vibration at a design point. Due to high rotational speed of turbopump, effects of centrifugal forces are carefully considered in the structural analysis. Hydrodynamic pressure is also considered as an external force applied to inducer and impeller blades. A three-dimensional Finite Element Method (FEM) is used for linear and nonlinear structural analyses with modified Newton-Raphson iteration method. After the nonlinear trim solution is obtained from the structural analysis, dynamic characteristics are obtained as a function of rotational speed from the linearized eigenvalue analysis at an equilibrium position. According to the results of numerical analysis, the safety margins of strength and vibration resonances are sufficient enough for safe operation within the requited life cycle.
Keywords
Turbopump; Inducer; Impeller; Finite Element Method;
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  • Reference
1 Critical Speed of Shaft/Stress Analysis of Pumps and Turbine (2D/3D) /
[ Kalmykov, G. P. ] / KeRC Report Contract No. HYSA-99-S001 Annex
2 터보펌프 Cavitation 성능시험기 개발 및 성능시험에 관한 연구 /
[ 손동기;김춘택;윤민수;차봉준;김진한;양수석 ] / 대한기계학회 춘계 학술대회
3 /
[ Kiktenko;Chumachenko ] / Experimental Turbopump Design
4 액체로켓 인듀서의 수치해석을 통한 성능예측 /
[ 최창호;이기수;김진한;양수석 ] / 대한기계학회 춘계 학술대회
5 Technical Conditions 3TH 000 000 TY Manufacture, Testing and Acceptance /
[ Kalmykov, G. P. ] / KeRC Report Contract No. HYSA-99-S001 Annex
6 Stress and Vibration Analysis of Turbopump Inducer Blades by Finite Elements /
[ Barten, H. J. ] / Journal of Spacecraft   DOI
7 임펠러/벌류트 상호작용을 이용한 원심펌프의 성능예측 /
[ 이기수;최창호;김진한;양수석 ] / 전산유체공학회 ?계 학술대회
8 High Pressure Oxidizer Turbopump(HPOTP) Inducer Dynamic Design Environment /
[ Herda, D. A.;Gross, R. S. ] / NASA TP-3589