• 제목/요약/키워드: Gaseous Hydrogen & Oxygen

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초임계 압력상태에서 기체수소/액체산소 국소화염구조 해석 (Analysis for Local Structure of Gaseous Hydrogen/liquid Oxygen Flame at Supercritical Pressures)

  • 김태훈;김성구;김용모
    • 한국분무공학회지
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    • 제15권4호
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    • pp.182-188
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    • 2010
  • Significant real fluid behaviors including rapid property changes take place where high pressure combustion devices such as rocket engines. The flamelet model is the reliable approach to account for the real fluid effects. In the present study, the flamelet equations are extended to treat the general fluids over transcritical and supercritical states. The real fluid flamelet model is carried out for the gaseous hydrogen and cryogenic liquid oxygen flames at the wide range of thermodynamic conditions. Based on numerical results, the precise discussions are made for effects of real fluid, pressure, and differential diffusion on the local flame structure.

Nonlinear Acoustic-Pressure Responses of Oxygen Droplet Flames Burning in Gaseous Hydrogen

  • Chung, Suk-Ho;Kim, Hong-Jip;Sohn, Chae-Hoon;Kim, Jong-Soo
    • Journal of Mechanical Science and Technology
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    • 제15권4호
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    • pp.510-521
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    • 2001
  • A nonlinear acoustic instability of subcritical liquid-oxygen droplet flames burning in gaseous hydrogen environment are investigated numerically. Emphases are focused on the effects of finite-rate kinetics by employing a detailed hydrogen-oxygen chemistry and of the phase change of liquid oxygen. Results show that if nonlinear harmonic pressure oscillations are imposed, larger flame responses occur during the period that the pressure passes its temporal minimum, at which point flames are closer to extinction condition. Consequently, the flame response function, normalized during one cycle of pressure oscillation, increases nonlinearly with the amplitude of pressure perturbation. This nonlinear response behavior can be explained as a possible mechanism to produce the threshold phenomena for acoustic instability, often observed during rocket-engine tests.

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수소-산소 동축 분사기에 대한 리세스 효과 수치해석 (Numerical Analysis of Recess Effects on Gaseous Hydrogen/Liquid Oxygen Coaxial Injector)

  • 이기범;박태선
    • 한국추진공학회지
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    • 제20권3호
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    • pp.17-24
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    • 2016
  • 본 연구에서 리세스가 있는 기체수소/액체산소 2차원 동축 전단 분사기에 대해 연소해석을 수행하였다. 이상기체와 실제기체 상태방정식을 이용한 정상상태 난류연소에 대해 표준 ${\kappa}-e$ 모델과 층류 화염편 모델이 선택되었다. 리세스 길이가 증가할수록 연소실 내 재순환의 크기가 커지고 와도가 강해졌다. 또한, 온도, 연소생성물, 압력의 변화가 리세스 길이에 큰 영향을 받았다. 해석된 결과들은 리세스가 있는 분사기에 의해서 효과적인 연소기를 얻을 수 있음을 보여주었다.

압력섭동에 따른 비정상 화염편 응답특성 해석 (Flamelet Analysis for Transient Response to Pressure Oscillations)

  • 배준경;김용모;김성구
    • 한국연소학회지
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    • 제16권1호
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    • pp.30-35
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    • 2011
  • This study has been mainly motivated to numerically investigate the transient flame response to pressure oscillations in the gaseous hydrogen - liquid oxygen flames at supercritical pressures. The present analysis is based on the real-fluid transient flamlet model and the flame field is acoustically perturbed only by the sinewave oscillations in the frequency range from 1,000 Hz to 5,000 Hz. Based on numerical results, the detailed discussions are made for the flame response characteristics and the transient flamelet response associated with the high-frequency combustion instability in the liquid propellant rocket engines.

초임계 압력에서 기체수소/액체산소의 연소과정 해석 (Analysis of Gaseous Hydrogen/liquid Oxygen Combustion Processes at Supercritical State)

  • 김태훈;김성구;김용모
    • 한국분무공학회지
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    • 제15권4호
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    • pp.189-194
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    • 2010
  • This study has been mainly motivated to numerically model the transcritical mixing and reacting flow processes encountered in the liquid propellant rocket engines. In the present approach, turbulence is represented by the extended k-$\varepsilon$ turbulence model. To account for the real fluid effects, the propellant mixture properties are calculated by using SRK (Souve-Redlich-Kwong) equation of state model. In order to realistically represent the turbulence-chemistry interaction in the turbulent non-premixed flames, the flamelet approach based on the real fluid flamelet library has been adopted. Based on numerical results, the detailed discussions are made for the real fluid effects and the precise structure of the transcritical cryogenic liquid nitrogen jet and gaseous hydrogen/liquid oxygen coaxial jet flame.

인공조도를 이용한 수소발생량과의 상관성에 관한 연구 (A Study for Correlativity of Hydrogen Production Using Artificial Luminous Intensity)

  • 정유라;홍창우;최용성;이경섭
    • 전기학회논문지P
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    • 제59권2호
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    • pp.218-221
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    • 2010
  • This paper presents energy efficiency about an electrolyser which is related with the hybrid system of solar cell and fuel cell for using the system more fully. The water electrolyser is the exact reverse of a hydrogen fuel cell; it produces gaseous hydrogen and oxygen from water. Electrolyser technology may be implemented at a variety of scales wherever there is an electricity supply to provide hydrogen and/or oxygen for virtually any requirement. Also, this paper shows optimum operating point in the electrolyser for saving cost of the electrical energy with hybrid system.

O2/H2 화염의 초임계 조건 연소 특성 연구를 위한 모델 연소기 설계 (Design of a Model Combustor for Studying the Combustion Characteristics of O2/H2 Flames at Supercritical Conditions)

  • 안영종;김영후;권오채
    • 한국수소및신에너지학회논문집
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    • 제31권1호
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    • pp.96-104
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    • 2020
  • A model combustor has been designed and fabricated for studying the combustion characteristics of oxygen (O2)/hydrogen (H2) flames under supercritical conditions. The combustor is designed to allow combustion experiments up to 60 bar, the supercritical pressure condition of O2 and H2. Injectors can be replaced to study various types of flames and the combustion chamber is designed to visualize flames by installing optical windows. Through the preliminary tests, including a high-pressure (up to 60 bar) test using air and combustion tests for coaxial jet flames of liquid oxygen (LO2)/gaseous hydrogen (GH2) at elevated pressure, the reliability of the combustor has been demonstrated.

초임계 압력하의 기체수소-액체산소 화염에 대한 난류모델을 이용한 해석에서 수치기법 평가 (An Evaluation of Numerical Schemes in a RANS-based Simulation for Gaseous Hydrogen/Liquid Oxygen Flames at Supercritical Pressure)

  • 김원현;박태선
    • 한국추진공학회지
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    • 제17권3호
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    • pp.21-29
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    • 2013
  • 초임계조건의 기체수소/액체산소 화염의 난류유동 및 온도장에 대해 난류모델을 이용한 해석이 수행되었다. 실제유체의 연소유동을 해석하기 위하여 화염편모델에 SRK 상태방정식이 도입되었다. 수정된 압력-속도-밀도 연계알고리듬이 초임계유동에 적용되었다. 수정된 알고리듬을 토대로 6개의 대류항 차분법과 4개의 난류모델의 상대적인 성능비교가 이루어졌다. 선택된 난류모델들은 실제유체 연소유동의 다양한 특징을 고려하기 위해서 수정이 필요함을 나타내었다.

Design and Combustion Tests of 1[N] Micro-Thruster with $H_2/O_2$ Propellants

  • Fujii, Masaya;Seki, Lssei;Yuasa, Saburo
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.628-633
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    • 2004
  • 초소형위성은 개발기간의 단축에 따른 발사 비용의 저감과 업무와 기능의 분산화에 따른 발사 실패의 리스크 저감 등 여러 장점이 있기 때문에 그 필요성이 높아지고 있다.(중략)

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연료용 합성가스 생산을 위한 바이오매스와 폐플라스틱의 혼합가스화 (Co-Gasification of Woodchip and Plastic Waste for Producing Fuel Gas)

  • 홍성구
    • 한국농공학회논문집
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    • 제54권3호
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    • pp.75-80
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    • 2012
  • Gasification is a therm-chemical conversion process to convert various solid fuels into gaseous fuels under limited supply of oxygen in high temperature environment. Considering current availability of biomass resources in this country, the gasification is more attractive than any other technologies in that the process can accept various combustible solid fuels including plastic wastes. Mixed fuels of biomass and polyethylene pellets were used in gasification experiments in this study in order to assess their potential for synthesis gas production. The results showed that higher reaction temperatures were observed in mixed fuel compared to woodchip experiments. In addition, carbon monoxide, hydrogen, and methane concentrations were increased in the synthesis gas. Heating values of the synthesis gas were also higher than those from woodchip gasification. There are hundred thousand tons of agricultural plastic wastes generated in Korea every year. Co-gasification of biomass and agricultural plastic waste would provide affordable gaseous fuels in rural society.