• Title/Summary/Keyword: 시동성능

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The performance effect of shroud split for turbopump turbine rotor (터보펌프 터빈 로터의 슈라우드 스플릿이 성능에 미치는 영향)

  • Lee, Hang-Gi;Jung, Eun-Hwan;Yoon, Suk-Hwan;Park, Pyun-Gu;Kim, Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.117-122
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    • 2012
  • A blisk with rotor shroud is usually adopted in LRE turbine to maximize its performance. However it experiences severe thermal load and resulting damage during engine stating and stop. Shroud splitting is devised to relieve thermal stress on the turbine rotor. Structural analysis confirmed the reduction of plastic strain at the blade hub and tip. However, split gap at the rotor shroud entails additional tip leakage and results performance degradation. In order to assess the effect of shroud split on the turbine performance, tests have been performed for various settings of shroud split. For the maximum number of shroud splitting, measured efficiency reduction ratio was 2.65% to the value of original shape rotor.

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A Study on Performance Characteristics of Second Throat Exhaust Diffuser with Back Pressure (고공환경 모사용 이차목 디퓨저의 배압에 따른 성능 특성)

  • Kim, Wan Chan;Yu, I Sang;Kim, Tae Woan;Park, Jin Soo;Ko, Young Sung;Kim, Min Sang
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.9
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    • pp.563-570
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    • 2017
  • Experimental and numerical studies were performed to investigate the performance and internal flow characteristics of a supersonic second throat exhaust diffuser (STED) with back pressure ($P_a$). An ejector system was used to vary the back pressure ($P_a$) conditions. The operating gas for the STED and the ejector was high pressure nitrogen at room temperature. When the back pressure ($P_a$) at a constant nozzle inlet pressure $P_0$) decreases, the pressure recovery location moves downstream. If the pressure ratio $P_0/P_a$) is the same, even if the nozzle inlet pressures $P_0$) are different, the diffuser's internal flow pattern and starting pressure ratio ($(P_0/P_a)_{st}$) are almost the same.

Experimental Study on Heat Transfer Characteristics of Binary Working Fluid for Clean Large Cauldron Using Liquid-Vapor Phase Change Heat (기-액 상변화 열전달을 이용한 대형 조리용기 개발을 위한 2 성분 작동유체의 열전달 특성실험)

  • Jung, Tae Sung;Kang, Hwan Kook
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.11
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    • pp.899-905
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    • 2014
  • This paper describes preliminary research conducted for developing a high-efficiency clean large cauldron using the liquid-vapor phase change heat transfer. To improve the isothermal environment of the cauldron, naphthalene and FC-40 were selected as the working fluids to operate well in the temperature range of $100-200^{\circ}C$ and used in experimental investigations of the heat transfer characteristics. A two-phase closed thermosyphon was designed and built to demonstrate the functionality of the working fluids. Startup, boiling, and condensation tests were performed, and the test results were used to examine the possibility of complementary effects of the startup and heat transfer characteristics of the two-phase closed thermosyphon using a mixture of naphthalene and FC-40.

Management of Test Facility for Tests of Liquid Rocket Engine on Off-Design Condition (액체로켓엔진 탈설계 조건 시험을 위한 시험설비 운용)

  • Yu, Byungil;Kim, Hongjip;Han, Yeongmin
    • Journal of Aerospace System Engineering
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    • v.14 no.5
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    • pp.91-99
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    • 2020
  • A liquid rocket engine goes through many tests to prove its performance before liftoff. It means the tests for setting ignition and start-up conditions or a test on design condition, which verifies the design performance. However, the development process requires verification of performance under off-design conditions through tests involving different operating conditions, which affects the duration of engine development. The off-design performance test is performed by altering the conditions of the propellant supplied to the engine in conjunction with the engine performance test that varies the opening of the control valves in the engine. This paper is based on the results of the engine tests performed at the KSLV-II engine test facilities in the Naro Space Center and describes the operations of the test facility for off-design condition test that changes the inlet conditions of the turbo-pump due to changes in the pressure and temperature of the propellant supplied to the test engines.

Present Status of Hydrogen Refueling Station in KIER (KIER 수소충전소 구축 현황)

  • Seo, Dong-Joo;Seo, Yu-Taek;Seo, Yong-Seog;Park, Sang-Ho;Roh, Hyun-Seog;Jeong, Jin-Hyeok;Yoon, Wang-Lai
    • 한국신재생에너지학회:학술대회논문집
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    • 2006.06a
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    • pp.21-24
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    • 2006
  • 수소의 소규모 분산 생산 기술은 본격 적 인 수소 인프라가 도입되기 전에 연료전지 자동차의 수소 충전용이나 분산 발전형 연료전지의 수소 공급을 위해 필요하다. 생산 용량은 수소 기준으로 $20{\sim}100 Nm^3/hr$ 정도로 현재로선 천연가스의 수증기 개 질법이 가장 경제적인 공정으로 알려져 있다. 소규모 생산에 따른 열효율 저하를 줄이 기 위해 단위 공정들이 통합된 컴팩트 개질 시스템의 개발이 필요하다. 연료전지 자동차용 수소 인프라 조기 구축을 위하여 수소충전소 구축과 국산화 천연가스 수증기 개질기 개발을 병행하여 진행하였다. 수소 충전소 구축 부분은 충전소 부지 확보, 건물 건축, 각종 유틸리 티 설치의 토목 부분과 천연가스 개질형 수소 제조 유닛 설치, 수소 압축, 저장, 디스펜싱 시스템 설치를 포함하고 있으며 고압 설비에 대한 인허가 대응 및 안전대책 작업도 진행하였다. 구축된 수소충전소는 향후 연료전지 자동차 연계 실증 프로그램에 활용할 수 있다. 국산화 핵심 기술 개발을 위하여 열 및 시스템 통합 설계에 의 해 천연가스 수증기 개질기를 제작하고 내부 열교환 구조에 따른 개질기의 성능을 평가하였다. 개발된 개질기는 개질온도 $720^{\circ}C$, 수증기 대 카본 비 2.7의 운전조건에서 $23Nm^3/h$ 이상의 수소 생산이 가능하였으며 73% 이상의 개질 효율을 나타내었다. 개발된 천연가스 수증기 개질기는 향후 수소 정제용 PSA(Pressure Swing Adsorption) 시스템과 연계하여 수소충전소 국산화 엔지니어링 설계 패키지 개발의 핵심 기 술로 사용할 계획이다.시간 정도 운전한 후 시스템을 정지하였다 메탄 전환율과 일산화 탄소 농도, 열효율을 모니터링 하고 있으며, 현재까지 초기 성능을 그대로 유지하고 있다. 앞으로 일일시동-정지 운전 시험을 지속하면서 초기 시동 특성 및 부하 변동에 따른 응답 특성 개선, 그리고 연료전지와의 연계 운전을 실시할 예정이다 한다. 단위 전지 운전 온도 $130^{\circ}C$, 상대습도 37%의 운전 조건에서도 상당히 우수한 전지 성능을 보임에 따라 고온/저가습 조건에서 상용 Nafion 112 막보다 우수한 막 특성을 나타냄을 확인하였다.소/배후방사능비는 각각 $2.18{\pm}0.03,\;2.56{\pm}0.11,\;3.08{\pm}0.18,\;3.77{\pm}0.17,\;4.70{\pm}0.45$ 그리고 $5.59{\pm}0.40$이었고, $^{67}Ga$-citrate의 경우 2시간, 24시간, 48시간에 $3.06{\pm}0.84,\;4.12{\pm}0.54\;4.55{\pm}0.74 $이었다. 결론 : Transferrin에 $^{99m}Tc$을 이용한 방사성표지가 성공적으로 이루어졌고, $^{99m}Tc$-transferrin의 표지효율은 8시간까지 95% 이상의 안정된 방사성표지효율을 보였다. $^{99m}Tc$-transferrin을 이용한 감염영상을 성공적으로 얻을 수 있었으며, $^{67}Ga$-citrate 영상과 비교하여 더 빠른 시간 안에 우수한 영상을 얻을 수 있었다. 그러므로 $^{

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An Experimental Study of Synthesis and Characterization of Vanadium Oxide Thin Films Coated on Metallic Bipolar Plates for Cold-Start Enhancement of Fuel Cell Vehicles (연료전지 차량의 냉시동성 개선을 위한 금속 분리판 표면의 바나듐 산화물 박막 제조 및 특성 분석에 관한 연구)

  • Jung, Hye-Mi;Noh, Jung-Hun;Im, Se-Joon;Lee, Jong-Hyun;Ahn, Byung-Ki;Um, Suk-Kee
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.6
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    • pp.585-592
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    • 2011
  • The enhancement of the cold-start capability of polymer electrolyte fuel cells is of great importance in terms of the durability and reliability of fuel-cell vehicles. In this study, vanadium oxide films deposited onto the flat surface of metallic bipolar plates were synthesized to investigate the feasibility of their use as an efficient self-heating source to expedite the temperature rise during startup at subzero temperatures. Samples were prepared through the dip-coating technique using the hydrolytic sol-gel route, and the chemical compositions and microstructures of the films were characterized by X-ray diffraction, X-ray photoelectron spectroscopy, and field-emission scanning electron microscopy. In addition, the electrical resistance hysteresis loop of the films was measured over a temperature range from -20 to $80^{\circ}C$ using a four-terminal technique. Experimentally, it was found that the thermal energy (Joule heating) resulting from self-heating of the films was sufficient to provide the substantial amount of energy required for thawing at subzero temperatures.

Comparison of Performance on Hypersonic Intakes in Off-Design Conditions Through Numerical Simulations (전산해석을 통한 탈설계점에서의 극초음속 흡입구 성능 비교)

  • Cha, Seung-Won;Roh, Tae-Seong;Lee, Hyoung Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.3
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    • pp.195-203
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    • 2019
  • Since the hypersonic intake is directly related to the overall performance of the engine, it is essential to analyze performance characteristics under various off-design conditions. In this paper, Busemann intake and conical intake with external compression were designed, and numerical simulations were performed at on/off-design conditions. Based on the results, the overall performance characteristics of two types of intake were analyzed in various Mach numbers and angle of attacks. The results showed that performance degradation of Busemann intake with truncation angle of 2 degrees was minimal. Also, the performance of Busemann intake was higher than external compression intake at various Mach numbers, however, the starting characteristics were significantly reduced with an angle of attack.

Development of Tucson Fuel Cell Hybrid Electric Vehicle (투싼 연료전지 하이브리드 차량 개발)

  • Jeon Soonil;Choi Seoho;Kwon Soonwoo;Lee Kyuil;Jeong Sungjin;Yun Seong Gon
    • 한국신재생에너지학회:학술대회논문집
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    • 2005.06a
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    • pp.357-360
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    • 2005
  • Hyundai Motor Company developed the second generation of fuel cell hybrid electric vehicle based on Tucson SUV in 2004. This vehicle has cold start capability below -10C and its driving performances including maximum speed and accelerating time are almost similar to conventional Tucson SUV's performances without any sacrifice in terms of cabin space. Especially. the cold start capability was realized by utilizing only internal power sources such as fuel cell power and high voltage lithium ion polymer battery. In this paper, we will briefly introduce specifications of Tucson FCEV and its driving performances based on field test and simulations.

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Static and Dynamic Characteristics of Aerostatic Gas Bearing (공기정압 베어링의 정 동특성에 관한 연구)

  • 전경석;한동철
    • Tribology and Lubricants
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    • v.6 no.2
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    • pp.60-67
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    • 1990
  • 최근 전자 및 광학 분야에 있어서의 눈부신 발전은 다면경 가공기나 초정밀 연삭기와 같은 초정밀 가공기계의 개발과 실용화에 힘입은 바 크다. 이러한 초정밀 가공기의 성능을 좌우하는 핵심 요소로서 추축계를 들수 있으며, 비교적 소형 경량의 공박물을 가공하는 기계의 주축용 베어링으로는 오일 베어링을 대신하여 공기 베어링이 점차 널리 사용되고 있다. 이러한 가공기에 많이 사용되는 외부 가압 공기 베어링은 동압 공기 베어링과는 달리, 외부에서 가압된 압축공기에 의하여 공기막을 형성하므로, 시동과 정지시 마멸이 없고 저속에서도 비교적 높은 하중 지지력을 얻을 수 있으며, 오일 베어링과 비교하여서는 발열이 적고 윤활제의 유출에 의한 오염의 위험이 없다는 특성외에 공기막에 의한 평균화 효과에 의하여 고정도의 운전이 가능하다는 장점이 있다. 본 연구에서는 점급기원의 가정하게 직접 수치해법을 사용하는 해석 프로그램을 작성하여, 무차원화된 설계 변수들에 대한 외부가압 공기베어링의 정$\cdot$동특성수들을 구하고자 한다.

Experimental Evaluation of HDD's Non-Contact Start/Stop Motion Using Shape Memory Alloy Actuator (SMA 작동기를 이용한 HDD의 비접촉 시동 및 정지 기구의 실험적 성능 고찰)

  • 임수철;박종성;최승복;박영필
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.05a
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    • pp.1122-1129
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    • 2001
  • In this work, we propose a new type of HDD suspension featuring shape memory ally (SMA) actuator in order to prevent the contact between the slider and disk. The principal design parameters are obtained from the modal analysis using finite element analysis, and then the dynamic model is established to formulate the control scheme for Non-Contact Start/Stop mode drive. Subsequently, a robust Η$_{\infty}$, control algorithm is designed by integrating experimentally-obtained SMA actuator dynamics to the proposed suspension system. The controller is empirically realized and control results for different load/unload profiles are presented in time domain. In addition, the contact signal between the slider and disk is measured by the electrical resistance method.istance method.

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