• Title/Summary/Keyword: High pressure gas

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Numerical Analysis for Evaluation of Ejection Capacity Relationship of Safety Valves in Pressure Regulating Station(I) - Flow Analysis and Mass Flow Rate Verification of Pressure Regulator - (정압기지내의 안전밸브 분출용량 관계식 검증을 위한 유동해석(I) - 정압기 유동 해석 및 질량 유량 검증 -)

  • Gwon, Hyuk-Rok;Roh, Kyung-Chul;Kim, Young-Seop;Lee, Seong-Hyuk
    • Journal of the Korean Institute of Gas
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    • v.12 no.2
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    • pp.99-104
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    • 2008
  • Gas pressure regulators in pressure regulating station reduce high-pressure gas in a process line to a lower. Gas pressure regulators are not flow control devices, they are used to control delivery pressure only. For the safety of pressure regulating station, it is essential to study flow regime and characteristics of a safety valves that is connected to a pressure regulator. For this, it is necessary to understand flow characteristics and the flow rate of upstream component part such as gas pressure regulators in regulating station. In the present study, numerical analysis of flow characteristics and the mass flow rate of a pressure regulator is conducted under the several inlet, outlet conditions and open rates. Then, the numerical result of the mass flow rate is verified with experimental equation from manufacture of pressure regulator. Consequently, the numerical result is comparatively good agreement with values from experimental equation.

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Effect of Operating Conditions on the Residual Gas Fraction in an SI Engine (스파크 점화 기관에서 밸브오버랩이 잔류가스율 변화에 미치는 영향)

  • 장진영;박용국;배충식;김우태
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.6
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    • pp.11-18
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    • 2002
  • Residual gas fraction in an engine cylinder affects engine performance, efficiency and emission characteristics. With high residual gas fractions, a flame speed and maximum combustion temperature are decreased and these are deeply related with combustion stability especially at idle and NOx emission at relatively high engine load. In this work, the residual gas fraction was calculated by an engine simulation code, which was validated by the experimental data (cylinder pressure and emissions) obtained from 4-cyliner spark ignition engine. A comparison between experimental and computational calculation results was made. The residual gas is generated mostly at low engine speed by the larger pressure difference between the intake and exhaust port. As the valve overlap duration was increased, the amount of residual gas in the cylinder, the amount of HC emission in the exhaust gas and the variation of power output increased.

Densification of $Si_3N_4$ Cera,ocs by Two Step Gas Pressure Sintering (2단계 가스압 소결에 의한 질화규소의 치밀화)

  • 이상호
    • Journal of the Korean Ceramic Society
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    • v.35 no.7
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    • pp.659-664
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    • 1998
  • Densification behavior of $Si_3N_4$ ceramics by two step gas pressure sintering was compared with pres-sureless sintering one step gas pressure sintering or hot isostatic pressing. While it was difficult to get the highly interlocked ${\beta}-Si_3N_4$ microstructure during the pressureless sintering due to decomposition above $1800^{\circ}C$ gas pressure sintering could solve this problem by increasing the densification temperature 2MPa of nitrogen pressure was enough to inhibit the decomposition up to $1890^{\circ}C$ and especially two step gas pres-sure sintering applying comparatively low pressure(2MPa) until the closed pore stage and then high pres-sure(10MPa) after pore closure could increase the hardness and the toughness.

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Thermo-Mechanical Analysis of Continuous-Adjustment Thruster using Explosion Pressure (폭압을 사용하는 연속조정 추진구조체의 열-구조해석)

  • Kim, Kyung-Sik;Kwon, Young-Doo;Kwon, Soon-Bum;Gil, Hyuck-Moon
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.24 no.6
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    • pp.699-705
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    • 2011
  • High-maneuver missile is a projectile which demands a strong momentum at short time. To produce a necessary thrust for the flight, the gas of high temperature and pressure is generated through explosive combustion of solid propellant, and a great thrust can be obtained by expanding this high temperature and pressure gas. Although the operating time of a rocket motor is less than a few seconds, a failure of part or ablation near the throat of nozzle may take place during the expansion of high temperature and pressure gas for great thrust. In other words, for the precise control of a missile an exact stress analysis considering both, the thermal stress caused by the heat transfer between combustion gas and wall, and the mechanical stress caused by the pressure change in the flow, should be considered first. In this connection, this study investigated the safety, as a point of view of stress and melting point of the material, of the pre-designed thrust generating structure which is subjected to high temperature and pressure as a function of motor operating time.

Analysis of Cold Gas Flow in Puffer Type GCB Considering the Real Gas Property of $SF_6$ ($SF_6$ 가스의 실제 기체특성을 고려한 파퍼식 가스차단기 내의 냉가스 유동해석)

  • 김홍규;정진교;박경엽
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.53 no.3
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    • pp.129-134
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    • 2004
  • To analyze the performance of the gas circuit breaker(GCB), the flow field variables such as temperature, pressure and density should be evaluated accurately In the puffer chamber of puffer type GCB, the pressure rise may Exceed 20 bar and in this range of high pressure, $SF_6$ gas deviates the ideal gas property. Therefore, the real gas property of $SF_6$ should be taken into consideration for the accurate analysis of flow field. This paper presents the analysis technique of cold gas flow in GCB employing the real gas state equation of SF6. The FVFLIC method is Employed to solve the axisymmetric Euler equation. To reduce the computational effort of real gas state equation, the relationship between density and pressure is approximated by the polynomial at the temperature of 300K. The proposed method is applied to the test GCB model and simulation results show good agreement with the experimental ones.

Numerical Study on the Production of Methane Hydrate by Depressurization Method (감압법을 이용한 메탄하이드레이트 생산에 대한 수치적 연구)

  • Kim, Jin-Hong;Chun, Won-Gee;Kim, Nam-Jin
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.06a
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    • pp.519-523
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    • 2007
  • Gas(or methane) hydrates are solid solutions when water molecules are linked through hydrogen bonding and create host lattice cavities that can enclose a large variety of guest gas molecules. The natural gas hydrate crystal may exist at low temperature above the normal freezing point of water and high pressure greater than about 30 bars. A lot of quantities of natural gas hydrates exists in the earth and many production schemes are being studied. In the present investigation, depressurization method was considered to predict the production of gas and the simulation of the two phase flow - gas and water - in porous media is being carried out. The simulation show about the fluid flow in porous media have a variety of applications in industry. Results provide the appearance of gas and water production, the pressure profile, the saturation of gas/ water/ hydrates profiles and the location of the pressure front.

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Diffusion Range and Pool Formation in the Leakage of Liquid Hydrogen Storage Tank Using CFD Tools

  • Kim, Soohyeon;Lee, Minkyung;Kim, Junghwan;Lee, Jaehun
    • Applied Chemistry for Engineering
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    • v.33 no.6
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    • pp.653-660
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    • 2022
  • In liquid hydrogen storage tanks, tank damage or leakage in the surrounding pipes possess a major risk. Since these tanks store huge amounts of the fluid among all the liquid hydrogen process facilities, there is a high risk of leakage-related accidents. Therefore, in this study, we conducted a risk assessment of liquid hydrogen leakage for a grid-type liquid hydrogen storage tank (lattice-type pressure vessel (LPV): 18 m3) that overcame the low space efficiency of the existing pressure vessel shape. Through a commercially developed three-dimensional computational fluid dynamics program, the geometry of the site, where the liquid hydrogen storage tank will be installed, was obtained and simulations of the leakage scenarios for each situation were performed. From the computational flow analysis results, the pool formation behavior in the event of liquid hydrogen leakage was identified, and the resulting damage range was predicted.

A Study on the Effect of Turbulent Combustion upon Soot Formation in Premixed Constant-Volume Propane Flames (정적 예혼합 프로판 화염의 매연생성에 미치는 난류연소 영향에 관한 연구)

  • 배명환;안수환
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.7
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    • pp.889-898
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    • 2003
  • The soot yield is studied by a premixed propane-oxygen-inert gas combustion in a specially designed disk-type constant-volume combustion chamber to investigate the effect of turbulence on soot formation. Premixtures are simultaneously ignited by eight spark plugs located on the circumference of chamber at 45 degree intervals in order to observe the soot formation under high pressures and high temperatures. The eight flames converged compress the end gases to a high pressure. The laser schlieren and direct flame photographs for observation field with 10 mm in diameter are taken to examine into the behaviors of flame front and gas flow in laminar and turbulent combustion. The soot volume fraction in the chamber center during the final stage of combustion at the highest pressure is measured by the in situ laser extinction technique and simultaneously the corresponding burnt gas temperature by the two-color pyrometry method. It is found that the soot yield of turbulent combustion decreases in comparison with that of laminar combustion because the burnt gas temperature increases with the drop of heat loss.

A Numerical Analysis of the NO Emission Characteristics in $CH_4/Air$ Counterflow Premix Flame (메탄/공기 대향류 예혼합화염의 NO 발생특성에 관한 수치해석)

  • Cho, Eun-Seong;Chung, Suk-Ho
    • Journal of the Korean Society of Combustion
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    • v.9 no.4
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    • pp.22-27
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    • 2004
  • Lean premix combustion is a best method in low $NO_x$ gas turbine combustor and we must know the characteristics of NO emission in high temperature and pressure condition in premix flame. Numerical analysis was performed to investigate the NO emission characteristics by adopting a counterflow as a model problem using detailed chemical kinetics. Methane $(CH_4)$ was used as a test fuel which is the main fuel of natural gas. The tested parameters were stretch rate, equivalence ratio, initial temperature, and pressure in premix flame. Results showed that NO emission was high in low stretch rate, near stoichiometric equivalence ratio, high initial temperature, and high pressure. Also, the pressure effect was sensitive in high temperature condition.

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A Study on Spark Ignition Natural Gas Engines

  • Cho Haeng-Muk
    • Journal of Advanced Marine Engineering and Technology
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    • v.30 no.4
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    • pp.455-462
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    • 2006
  • Natural gas is a promising alternative fuel to meet strict engine emission regulations in many countries. Natural gas engines can operate at lean burn and stoichiometric burn conditions with different combustion and emission characteristics. In this paper, the fuel economy, emissions, misfire, knock and cycle-to-cycle variations in indicated mean effective pressure of lean burn natural gas engines are highlighted. Stoichiometric burn natural gas engines are briefly reviewed. To keep the output power and torque of natural gas engines comparable to that of gasoline engines, high boosting pressure should be used. High activity catalyst for methane oxidation and lean deNOx system or three way catalyst with precisely control strategies should be developed to meet stringent emission standards.