• Title/Summary/Keyword: pressurization system

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Performance Test of PSD Oxidizer Drain Valve for KSLV-II (한국형발사체 PSD 산화제 배출밸브 성능시험)

  • Chung, Yonggahp;Han, Sangyeop;Kim, Suengik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1171-1175
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    • 2017
  • Cryogenic helium gas is used as the pressurant for the oxidizer pressurization of DR(Damper Receiver) sphere in the PSD(Pogo Suppression Device) system and liquid oxygen is used as the oxidizer for the propellant in Korea Space Launch Vehicle-II. The helium gas is stored in pressurant cylinders inside the cryogenic liquid oxygen tank and liquid oxygen is stored in the oxidizer tank. In this study, the performance test of PSD liquid oxygen drain valve for KSLV-II was considered.

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Pre-service Acoustic Emission Testing for Metal Pressure Vessel (금속압력용기의 사용 전 음향방출시험)

  • Lee, Jong-O;Yoon, Woon-Ha;Lee, Tae-Hee;Lee, Jong-Kyu
    • Journal of the Korean Society for Nondestructive Testing
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    • v.23 no.3
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    • pp.280-284
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    • 2003
  • The field application of acoustic emission(AE) testing for brand-new metal pressure vessel were performed. We will introduce the test procedure for acoustic emission test such as instrument check distance between sensors, sensor location, whole system calibration, pressurization sequence, noise reduction and evaluation. The data of acoustic emission test contain many noise signal, these noise can be reduced by time filtering which based on the description of observation during AE test.

Effect of pressurization on dissolution of a supercooled aqueous solution with a stationary state (가압조건이 정지상태 과냉각 수용액의 해소에 미치는 영향)

  • Kim, Byung-Seon;Peck, Jong-Hyun;Hong, Hi-Ki;Kang, Chae-Dong
    • Proceedings of the SAREK Conference
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    • 2006.06a
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    • pp.132-137
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    • 2006
  • Supercooled type ice slurry system is hard to keep a proper supercooling degree when solution becomes supercooling state. This is the reason of the ice blockage in pipe or cooling part due to an unstable cooling state. In this study, a cooling experiment was performed to pressurized solution in a stationary state. The behaviors during the supercooled aqueous solution were investigated at fixed flow rate of brine and aqueous solution of ethylene glycol 7 mass%. Also the effect to the freezing point of supercooled aqueous solution was investigated to the different pressure 101, 202, 303, and 404 kPa. At results, the pressure of the aqueous solution in the cylinder increased the supercooling degree increased and dissolution of supercooled point decreased.

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Life-Time Prediction of HNBR Diaphragm in Oil Reservoir (유압구동장치 동력원용 고무 다이아프램 저유기의 수명 예측 연구)

  • Kim, Sol A
    • Journal of Drive and Control
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    • v.18 no.2
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    • pp.32-37
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    • 2021
  • The piston reservoir is mainly used in hydraulic blow-down system for aerospace engineering. The reservoir is heavy due to both hydraulic cylinder and piston in pressurization. The positive expulsion tank with rubber diaphragm has been mostly applied propellant and fuel tank at low pressure to satellites. To reduce weight, the reservoir that can be used at high pressure with rubber diaphragm was developed. In this research, the prediction of life-time for the rubber diaphragm was implemented through an accelerated life test, as a part of development of new reservoir. Also, the diaphragm was stored in an temperature chamber at the same condition as and operation with hydraulic oil. As a result, the life-time for a rubber diaphragm was successfully evaluated via Arrhenius law and Time-Temperature Superposition based on failure times over temperatures in the accelerated test.

Helium Quantity Estimation for LOx Tank Pressurization of a Restartable Pressure-fed Propulsion System (재 점화가 있는 가압식 추진기관의 액체산소 탱크 가압 헬륨량 산정)

  • Cho, Gyu-Sik;Jung, Young-Suk;Oh, Seung-Hyub
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.3
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    • pp.77-81
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    • 2012
  • In a cryogenic propellant tank the pressurant is contracted due to heat loss and the propellant itself evaporates. On a restartable propulsion system such phenomena are more intensive because the propellant contacts with the pressurant on the larger surface during the coast flight. Such heat and mass transfer phenomena should be considered for estimating the amount of pressurant. On the hypothesis that the heat and mass transfer quasi-equilibrium is achieved during the coast flight, the calculation process of the equilibrium pressure is presented. On the process the amount of loaded helium on the Falcon-1 second stage is calculated.

Helium Quantity Estimation for LOx Tank Pressurization of a Restartable Pressure-fed Propulsion System (재 점화가 있는 가압식 추진기관의 액체산소 탱크 가압 헬륨량 산정)

  • Cho, Gyu-Sik;Jung, Young-Suk;Oh, Seung-Hyub
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.201-205
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    • 2011
  • In a cryogenic propellant tank the pressurant is contracted due to heat loss and the propellant itself evaporates. On a restartable propulsion system such phenomena are more intensive because the propellant contacts with the pressurant on the larger surface during the coast flight. Such heat and mass transfer phenomena should be considered for estimating the amount of pressurant. On the hypothesis that the heat and mass transfer quasi-equilibrium is achieved during the coast flight, the calculation process of the equilibrium pressure is presented. On the process the amount of loaded helium on the Falcon-1 second stage is calculated.

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Review of Steam Jet Condensation in a Water Pool (수조내 증기제트 응축현상 제고찰)

  • 김연식;송철화;박춘경
    • Journal of Energy Engineering
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    • v.12 no.2
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    • pp.74-83
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    • 2003
  • In the advanced nuclear power plants including APR1400, the SDVS (Safety Depressurization and Vent System) is adopted to increase the plant safety using the concept of feed-and-bleed operation. In the case of the TLOFW (Total Loss of Feedwater), the POSRV (Power Operated Safety Relief Value) located at the top of the pressurizer is expected to open due to the pressurization of the reactor coolant system and discharges steam and/or water mixture into the water pool, where the mixture is condensed. During the condensation of the mixture, thermal-hydraulic loads such as pressure and temperature variations are induced to the pool structure. For the pool structure design, such thermal-hydraulic aspects should be considered. Understanding the phenomena of the submerged steam jet condensation in a water pool is helpful for system designers to design proper pool structure, sparger, and supports etc. This paper reviews and evaluates the steam jet condensation in a water pool on the physical phenomena of the steam condensation including condensation regime map, heat transfer coefficient, steam plume, steam jet condensation load, and steam jet induced flow.

Basic Model for Propellant Tank Ullage Calculation (추진제탱크 얼리지 해석을 위한 기본모델)

  • Kwon, Oh-Sung;Cho, Nam-Kyung;Cho, In-Hyun
    • Aerospace Engineering and Technology
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    • v.9 no.1
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    • pp.125-132
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    • 2010
  • Estimation of pressurant mass flowrate and its total mass required to maintain propellant tank pressure during propellant outflow is very important for design of pressurization control system and pressurant storage tank. Especially, more pressurant mass is required to maintain pressure in cryogenic propellant tank, because of reduced specific volume of pressurant due to heat transfer between pressurant and tank wall. So, basic model for propellant tank ullage calculation was proposed to estimate ullage and tank wall temperature distribution, required pressurant mass, and energy distribution of pressurant in ullage. Both test and theoretical analysis have been conducted, but only theoretical modeling method was addressed in this paper.

The Development of a Functional Pressure Controller in Smoke Management Systems for the Fire Safety of Buildings (화재시 제연 및 피난을 위한 기능성 차압 조절장치 개발에 관한 연구)

  • Jung, Ki-Chang;Kim, Jeong-Hun;Lee, Jung-Yun
    • Journal of the Korean Society of Safety
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    • v.19 no.1
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    • pp.44-48
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    • 2004
  • The smoke and toxic gases generated from the building fires are proved to cause human death. Therefore, the necessity and significance of smoke control have been emphasized, and lots of studies for developing improved smoke management system have been carried out. In this study, the experiments were conducted to evaluated a function and performance in newly developed smoke management system using mechanical pressurization. As a result of this experiment, the differential pressure was 40Pa${\sim}$60Pa and the air velocity through the door was 0.7m/s between safety zone and fire zone. The functional pressure control equipment which could make proper pressure and maintain differential pressure between safety zone and fire zone was developed. And it will give a lot of helps to evacuation activity for peoples in building and fire fighting.

Study on the Cleaning Screen Printing using Alternative Cleaning Solvent of 1,1,1-TCE, CFC-113 (1,1,1-TCE, CFC-113 대체세정제를 이용한 스크린인쇄 세정연구)

  • Lee, Ki-Chang;Yoon, Cheol-Hun;Hwang, Sung-Kwy;Oh, Se-Young;Lee, Seok-Woo;Ryu, Jung-Wok
    • Journal of the Korean Applied Science and Technology
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    • v.14 no.2
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    • pp.115-122
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    • 1997
  • The field of printing use to pressurization ink using screen gassamer that is called screen printing. Existing cleaning solvent using screen printing are the organic solvents including aromatic compounds carried with poisonous and stench. Besides, cleaning method of current screen printing are for the most part mixed cleaning method of dipping and polish. Using 1,1,1-TCE, CFC-113 alternative system cleaning solvent be substituted for existing cleaning solvent against screen printing ink measured the cleaning efficiency according to gravimetric analysis method and property change of gassamer according to Image Analyzer. Also, Cleaning process system carry with excellent cleaning efficiency studied which was proposed new cleaning process including ultrasonic and vibration cleaning process be substituted for existing mixed cleaning method of dipping and polish.