재사용 우주발사체 액체로켓엔진용 터보펌프에 적용하기 위한 하이브리드 유체 스러스트 베어링의 정하중 특성: 실험과 해석의 비교
- Title
- 재사용 우주발사체 액체로켓엔진용 터보펌프에 적용하기 위한 하이브리드 유체 스러스트 베어링의 정하중 특성: 실험과 해석의 비교
- Other Titles
- Static Load Characteristics of Hybrid Fluid Film Thrust Bearings for Liquid Rocket Engine Turbopumps in Reusable Launch Vehicles: Comparisons between Experiments and Predictions
- Author
- 류근
- Issue Date
- 2020-11
- Publisher
- 한국추진공학회
- Citation
- 한국추진공학회 학술대회논문집, Page. 516-518
- Abstract
- The present work compares the measured static load characteristics of hybrid fluid film thrust bearings for liquid rocket engine turbopumps to predictions. Static loads over 700 N are applied to the vertically installed test hybrid thrust bearing, lubricated with high pressure compressed air as a working fluid. Three displacement sensors, equally spaced, measure fluid film thickness while a strain-gauge type load cell measures the applied static load. Over the entire static load ranges, the predicted results correlate very well with the measurements.
- URI
- https://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE10546592https://repository.hanyang.ac.kr/handle/20.500.11754/165178
- ISSN
- 2234-4748
- Appears in Collections:
- COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > MECHANICAL ENGINEERING(기계공학과) > Articles
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