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산화제 터보펌프의 구조 강도 및 진동 안전성에 관한 연구

Investigation on the Strength and Vibration Safety of the Oxidizer Turbopump

  • 전성민 (한국항공우주연구원 터보기계연구그룹) ;
  • 김진한 (한국항공우주연구원 터보기계연구그룹) ;
  • 양수석 (한국항공우주연구원 터보기계연구그룹) ;
  • 이대성 (한국항공우주연구원 추진기관연구부)
  • 발행 : 2002.09.01

초록

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.

키워드

참고문헌

  1. Journal of Spacecraft v.8 no.6 Stress and Vibration Analysis of Turbopump Inducer Blades by Finite Elements Barten, H. J. https://doi.org/10.2514/3.59707
  2. NASA TP-3589 High Pressure Oxidizer Turbopump(HPOTP) Inducer Dynamic Design Environment Herda, D. A.;Gross, R. S.
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  4. 대한기계학회 춘계 학술대회 액체로켓 인듀서의 수치해석을 통한 성능예측 최창호;이기수;김진한;양수석
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  6. Experimental Turbopump Design Kiktenko;Chumachenko
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