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전성민,윤석환,최창호,Jeon, Seong Min,Yoon, Suk-Hwan,Choi, Chang-Ho 항공우주시스템공학회 2015 항공우주시스템공학회지 Vol.9 No.1
A critical speed analysis of oxidizer pump was peformed for a 7 ton class liquid rocket engine as the third stage engine of the Korea Space Launch Vehicle II. Based on the previously developed experimental 30 ton class turbopump and presently developing 75 ton class turbopump for the first and second stage rocket engine of Korea Space Launch Vehicle II, a layout and configuration of the 7 ton class turbopump rotor assembly are determined. A ball bearing stiffness analysis and rotordynamic analysis are performed for both of the bearing unloaded condition and loaded condition. Structural flexibility of the oxidizer pump casing is also included to predict critical speeds. From the numerical analysis, it is confirmed that the rotor system acquires sufficient separate margin of critical speed as a sub-critical rotor even though decrease of critical speed due to the casing structural flexibility.
전성민,이강산,이재랑,김광득,박영옥,Jeon, Seong-Min,Hasolli, Naim,Lee, Kang-San,Lee, Jea-Rang,Kim, Kwang-Deuk,Park, Young-Ok Korean Society for Atmospheric Environment 2016 한국대기환경학회지 Vol.14 No.5
In this study, two kinds of industrial filter bags were tested for their filtration performance to apply the existing bag filter systems. Experimental variables were examined for pressure drop, cleaning interval, residual pressure drop, cleaning efficiency, fractional grade efficiency, total collection efficiency according to the filter bag structure. According to these results, the filter bags tested in this study demonstrated good performance in dust collection. This was also true for the double surface filter bag. The lifetime was longer than the round type filter bag because the filtration area was more than 1.6 times wider and the filter quality factor was much higher. Therefore, double surface filter bags are suggested to be used in order to increase filtration performance of the bag filter systems.
방사선(학)과의 작업종사자와 수시출입자의 교내 실습에 따른 피폭선량에 대한 고찰
전성민(Seong-Min Jeon),이용기(Yong-Ki Lee),안성민(Sung-Min Ahn) 한국방사선학회 2021 한국방사선학회 논문지 Vol.15 No.3
본 연구에서는 교내 실습 중 방사선(학)과 에 지정된 방사선작업종사자 및 수시출입자의 피폭 정도를 분석하여 방사선(학)과에 대한 원자력안전법의 방사선 방호에 대한 타당성과 최적화에 대한 기초 연구에 목적을 두었다. 연도별 작업종사자의 평균 피폭선량 2014년과 2016년에 0.01 mSv로 가장 낮은 수치가 나타났으며. 가장 높은 수치는 2018년도로 0.12 mSv이다. 연도별 수시출입자의 평균 피폭선량은 2018년 0.013 mSv로 가장 낮은 수치를 보였으며, 2016년 0.022 mSv로 가장 높은 수치가 나타났다. 본 연구를 통하여 방사선발생장치만을 사용하는 대학의 담당교수, 실습 조교 및 방사선(학)과의 학생들은 교내실습 과정에서 받는 연간 피폭선량은 일반인의 선량한도인 1mSv에도 미치지 못하는 수준이다. 그러므로 방사선(학)과 학생들의 피폭선량이 일반인의 선량한도 보다 낮게 나오는 시점에서 현재 원자력안전법의 안전규제는 과도한 규제라고 판단된다. 따라서 현재의 원자력안전법에서 방사선 발생장치의 규정을 개정하거나 대학의 재학생에 대한 방사선안전관리 체계를 수정하는 것은 필요하다고 사료된다. In this study, the purpose of this study was to analyze the degree of exposure of radiation workers assigned to the Department of Radiology and frequent visitors during on-campus practice, and to conduct a basic study on the feasibility and optimization of the radiation protection of the Nuclear Safety Act for the Department of Radiology. . The average exposure dose of occupational workers by year was 0.01 mSv, the lowest in 2014 and 2016. The highest figure was 0.12 mSv in 2018. The average exposure dose of frequent visitors by year was the lowest at 0.013 mSv in 2018, and the highest at 0.022 mSv in 2016. According to this study, the annual exposure dose received by professors, practical assistants, and students in the department of radiology (department) who use only radiation generators in the course of in-school practice is less than 1 mSv, which is the dose limit for the general public. Therefore, at the time when the radiation dose of students in the Department of Radiology is lower than the dose limit of the general public, the current safety regulation of the Nuclear Safety law is judged to be excessive regulation. Therefore, it is considered necessary to revise the regulations for radiation generators in the current Nuclear Safety law or to revise the radiation safety management system for university students.
전성민(Seong Min Jeon),곽현덕(Hyun Duck Kwak),박민주(Min Joo Park),김진한(Jinhan Kim) 한국추진공학회 2010 한국추진공학회 학술대회논문집 Vol.2010 No.5
75톤급 터보펌프용 추진제 혼합 방지 실의 누설 성능 및 내구 성능을 평가하기 위한 수류환경 성능 시험을 수행하였다. 추진제 혼합 방지 실 시제품은 연료펌프 부와 산화제펌프 부 각각 누적 시험시간 2,100초 동안 수류환경에서 내구 성능 시험이 이루어 졌다. 1단의 카본 플로팅 링 실로 구성된 연료펌프 부는 성능 시험 동안 평균 실 차압 9.4 bar에서 평균 누설 유량 13.7 gram/sec의 결과를 얻었다. 반면, 2단의 카본 플로팅 링 실로 구성된 산화제펌프 부는 성능 시험 동안 평균 실 차압 9.5bar에서 평균 누설 유량 7.3 gram/sec의 결과를 얻었다. 내구 성능 시험 후, 추진제 혼합 방지 실은 양호한 상태를 보였다. 향후 액체 질소를 시험 매질로 하는 극저온 환경에서 추진제 혼합 방지 실누설 성능 시험이 수행될 예정이다. A performance test of a 75 ton class turbopump inter propellant seal is conducted using water to evaluate leakage and endurance performance. Each fuel pump side part and oxidizer pump side part of a prototype inter propellant seal has been tested for verifying endurance performance during total accumulated test time 2,100 sec in water. The fuel pump side part with 1 stage carbon floating ring seal shows average leakage rate 13.7 gram/sec under average seal differential pressure 9.4 bar. On the other hand, the LOx pump side part with 2 stage carbon floating ring seal shows average leakage rate 7.3 gram/sec under average seal differential pressure 9.5 bar. After the endurance performance test, the inter propellant seal shows good physical condition. A cryogenic leakage performance test of the inter propellant seal will be performed using LN2 in the near future.
산화제 터보펌프의 구조 강도 및 진동 안전성에 관한 연구
전성민(Seong Min Jeon),김진한(Jinhan Kim),양수석(Soo-Seok Yang),이대성(Dae-Sung Lee) 한국유체기계학회 2001 유체기계 연구개발 발표회 논문집 Vol.- No.-
Structural and dynamic analyses of inducer and impeller for a oxidizer turbopump are peformed to investigate the safety level of strength and vibration at 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 to be operated safely within the required life cycle.