터보펌프용 연료펌프의 평균유선 성능해석

다국어 초록 (Multilingual Abstract)

Low NPSH and high pressure pumps are widely used for turbopump systems, which have an inducer and operate at high rotating speeds. In this paper, a meanline method has been established for the preliminary design and performance prediction of pumps having an inducer for cavitating or non-cavitating conditions and at design or off-design points. The method was applied for the performance prediction of a fuel pump, which had been developed by Hyundai Mobis in collaboration with KeRC for a liquid rocket engine. The engine uses liquid methane and liquid oxygen as working fluids and rotates at 50,000 rpm. KeRC carried out a model testing of the fuel pump with water as a working fluid at the reduced speed (10,000~15,000 rpm). Predicted performances by the method are shown to be in good agreement with experimental results for cavitating and non-cavitating conditions. The established meanline method can be used for the performance prediction and preliminary design of high speed pumps which have a inducer, impeller and volute.

목차 (Table of Contents)

• ABSTRACT
  
• 1. 서론
  
• 2. 펌프의 평균경 성능예측기법
  
• 3. 연료 펌프의 해석 결과
  
• 4. 결론
  
• 후기
  
• 참고문헌