• 제목/요약/키워드: Combustion Stability

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설계 인자에 따른 연료 과농 가스발생기의 연소 안정성 특성 연구 (A Parametric Study on Combustion Stability Characteristics of Fuel-rich Gas Generators)

  • 안규복;문일윤;서성현;한영민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.171-176
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    • 2006
  • 연료 과농 가스발생기에 대한 실험적 연구가 수행되었다. 연소 성능에 주요한 영향을 미치는 분사기 헤드에는 1.5의 리세스 수를 갖는 내부 혼합형 이중 스월 분사기 37개가 배치되었다. 본 논문에서는 연소실 길이, 직경, 그리고 교반링 등의 연소실 설계 변경에 따른 실물형 가스발생기의 연소 안정성 특성에 대하여 살펴보았다. 연소시험 결과 공진 주파수가 고주파 영역에서 생성됨에 따라 동압의 세기는 전반적으로 감소하였으나, 연소 불안정을 완전히 억제시키지는 못하는 것으로 나타났다.

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액체 로켓엔진에서 선형 연소 불안정 해석을 이용한 연소 안정한계 곡선 계산 (Calculation of Combustion Stability Limits Using Linear Stability Analysis in Liquid Rocket Engines)

  • 손채훈;문윤완;허환일
    • 한국항공우주학회지
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    • 제32권10호
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    • pp.93-101
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    • 2004
  • 액체 로켓엔진에서 발생하는 고주파 연소 불안정성을 예측하기 위해 선형 안정한계를 계산하는 방법을 연구하였다. 기존의 선형이론에 근거하여 유도된 선형 안정한계를 나타내는 안정한계 식을 채택하였으며, 그 식을 구성하는 각각의 항을 정량적으로 평가하는 방안들이 제시되었다. 안정한계 계산에 필요한 열-화학 물성치와 유동 변수를 열역학적 평형계산과 CFD 해석 및 실험 결과로부터 평가하는 구체적 절차들을 상세히 제시하였다. 실제 로켓엔진으로서 시험 데이터가 확보되어 있는 KSR-III 로켓엔진에 대해서 제시한 방법을 적용하여 안정한계 곡선을 구하였다. 계산결과는, 해당 엔진에 대해 정량적으로 타당한 안정한계 곡선을 보여주었다. 이를 토대로 해당 엔진의 안정성 특성을 분석하였다. 본 연구에서 제시된 선형 안정한계 계산 방법은 진정한 예측의 1차적 근사로서 활용할 만한 가치가 있으며, 엔진 개발 초기에 근사적으로 안정성 경향을 분석하기에 유용할 것이다.

니켈합금 Metal Foam을 적용한 예혼합 버너의 연소특성 (Combustion Characteristics of Premixed Combustor using Nickel Based Metal Foam)

  • 이필형;황상순;김종광
    • 한국연소학회지
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    • 제22권2호
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    • pp.42-49
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    • 2017
  • A premixed combustion has many advantages including low NOx and CO emission, high thermal efficiency and a small volume of combustor. This study focused on combustion characteristics in a premixed combustion burner using the nickel based metal foam. The results show that the blue flame is found to be very stable at heating load 6,300-25,200 kcal/h by implementing the proper nickel based metal foam and baffle plate. The premixed flame mode is changed into green flame, red flame, blue flame and lift off flame with decreasing equivalence ratio. NOx emission was measured 80 ppm(0% oxygen base) from 0.710 to 0.810 of equivalence ratio and CO emission is 90 ppm(0% oxygen base) under the same equivalence ratio. It is also found that the stable blue flame region in flame stability curve becomes wider with increasing the heat load.

동축형 제트 분사기의 화염 및 연소 안정성 특성에 관한 실험적 연구 (An Experimental Study On Characteristics of Flame and Combustion Stability of Coaxial Jet Injectors)

  • 손진우;민용호;손채훈
    • 한국연소학회지
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    • 제21권2호
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    • pp.15-21
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    • 2016
  • Flame characteristics and combustion stability of a swirl coaxial injector are studied experimentally. Characteristics of flame and combustion instability are analyzed with the parameter of MFR (momentum flux ratio) using hexane instead of kerosene. Flame patterns of blue and yellow are changed with variable MFR. Combustion instabilities are measured and analyzed by adopting a model chamber. Combustion instability mapping is made by evaluating damping factor at the 2 L (second longitudinal) mode with variable MFR in 63 cases for operating condition.

함침법을 이용한 금속염의 연속 억제 효과 (Combustion Retardation Effects of Metal Salts Using Impregnation Method)

  • 송영호;강민호;정국삼
    • 한국안전학회지
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    • 제19권1호
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    • pp.77-80
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    • 2004
  • The purpose of this study was to examine effects of combustion retardation for paper filter impregnated metal salts by measurement of extinguishing concentration, CO concentration, and limiting oxygen index(LOI, ASTM D 2863). And thermal stability analysis using DSC was carried out. In case of extinguishing concentration, $NH_4H_2PO_4$ showed excellent effect of combustion retardation. The result of LOI measurement showed that metal salts possessed good effect of combustion retardation. And thermal analysis using DSC showed that these metal salts possessed thermal stability. In case of CO concentration, CO concentration was increasing because of imperfect combustion process due to combustion retardation effect of metal salts.

디젤기관에서의 경유-메탄올 혼합유의 연소 안전성과 연소특성에 관한 연구 (A Study on the Combustion Stability and Characteristics for D.O - Methanol Blending Oil in Diesel Engine)

  • 김상암;왕우경
    • 동력기계공학회지
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    • 제22권1호
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    • pp.48-55
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    • 2018
  • It has recently been reported that methanol fuel has been used in the product carrier with established duel fuel engine, which has been greatly reducing emissions of $CO_2$, NOx and SOx from the engine. However, to use methanol alone as fuel oil in a general diesel engine, design modification of cylinder head is needed because the ignition aid device or the duel fuel injection system is needed. On the other hand, only if the mixer is installed on the fuel oil supply line, diesel oil - methanol blending oil can be used as fuel oil for the diesel engine, but there is a problem of the phase separation when two fuels are mixed. In this study, diesel oil and methanol were blended compulsorily in preventing the phase separation with installing agitators and a fuel oil boost pump on fuel line of a test engine. Also, cylinder pressure and fuel consumption quantity were measured according to engine load and methanol blending ratio, and indicated mean effective pressure, heat release rate and combustion temperature obtained from the single zone combustion model were analyzed to investigate the effects of latent heat of vaporization of methanol on combustion stability and characteristics. As a result, the combustion stability and characteristics of 10% methanol blending oil are closest to the those of diesel oil, and it could be used as fuel oil in existing diesel engines without deterioration of engine performance and combustion characteristics.

동축분류 확산화염에서 화염안정화와 연소특성에 관한 연구 (An Experimental Study on Flame Stability and Combustion Characteristics of Coaxial Diffusion Flame)

  • 유현석;오신규
    • 대한기계학회논문집
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    • 제19권2호
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    • pp.509-518
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    • 1995
  • A study for the flame stability and the combustion characteristics of coaxial diffusion flame was conducted. The fuel employed was natural gas. The experimental variables were rim thickness of fuel tube, blockage ratio of the outer diameter of fuel tube to the inner diameter of air tube, and momentum ratio of fuel to air. It was consequently found that the stability in the neighborhood of the fuel rim depended on the rim thickness, especially in the case of above 3 mm, and that the stable region of the flame extended remarkably due to the formation of recirculation zone above rim. The effect of the blockage ratio on the flame stability was found to be minor in the case of above 3 mm of rim thickness. Between the momentum ratio 2 and 3, the stable flame zone was widely established as well good combustion. With increasing the fuel-air momentum ratio, axial velocity, turbulence intensity, and Reynolds stress increased.

추력 30톤급 액체산소/케로신 로켓엔진 연소장치 개발(I)-연소기 (Development of 30-Tonf LOx/Kerosene Rocket Engine Combustion Devices(I) - Combustion Chamber)

  • 최환석;한영민;김영목;조광래
    • 한국항공우주학회지
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    • 제37권10호
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    • pp.1027-1037
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    • 2009
  • 우주발사체용 30톤급 액체로켓엔진 재생냉각 연소기 개발과정에 관하여 기술하였다. 이중추진제 동축 와류형 분사기 개발에서부터 시작하여 축소형 연소기를 통해 요소기술을 검증하고 개발된 기술을 실물형 연소기에 적용하였다. 총 5기의 실물형 연소기 개발시제를 사용하여 점화성능, 연소안정성, 연소성능, 냉각성능, 내구성 등의 검증을 수행하였다. 이 과정에서 총 46회의 실물형 연소기 연소시험을 실시하였고 이 중 23회는 기폭장치를 이용한 연소안정성 평가시험을 병행하였다. 시험 결과 30톤급 재생냉각 연소기는 연소 성능 및 연소안정성 요구사항을 모두 만족시켜 단품 개발이 성공적으로 완료된 것으로 평가하였다.

직접분사식 LPG 엔진의 연소전략 및 공기과잉률 변화에 따른 연소특성 비교 (Comparison of Combustion Characteristics with Combustion Strategy and Excess Air Ratio Change in a Lean-burn LPG Direct Injection Engine)

  • 조시현;박철웅;오승묵;윤준규
    • 한국자동차공학회논문집
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    • 제22권6호
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    • pp.96-103
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    • 2014
  • Liquefied Petroleum Gas(LPG) has attracted attention as a alternative fuel. The lean-burn LPG direct injection engine is a promising technology because it has an advantage of lower harmful emissions. This study aims to investigate the effect of combustion strategy and excess air ratio on combustion and emission characteristics in lean-burn LPG direct injection engine. Fuel consumption and combustion stability were measured with change of the ignition timing and injection timing at various air/fuel ratio conditions. The lean combustion characteristics were evaluated as a function of the excess air ratio with the single injection and multiple injection strategy. Furthermore, the feasibility of lean operation with stratified mixture was assessed when comparing the combustion and emission characteristics with premixed lean combustion.

저공해와 고안정성을 위한 신개념의 사이클론 제트 하이브리드 연소기의 연소특성 (The Combustion Characteristics of a New Cyclone Jet Hybrid Combustor for Low Pollutant Emission and High Flame Stability)

  • 정원석;황철홍;이규영;이창언
    • 대한기계학회논문집B
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    • 제28권2호
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    • pp.146-153
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    • 2004
  • A Promising new approach to achieve low pollutant emissions and improvement of flame stability is tested experimentally using a cyclone jet hybrid combustor employing both premixed and diffusion combustion mode. Three kinds of nozzle are tested for mixing enhancement of fuel and air. The LNG (Liquified Natural Gas) is used as a fuel. The combustor is operated by two methods. One is DC (Diffusion Combustion) mode generated swirl flow by air as general swirl combustor, and the other is HC (Hybrid Combustion) mode. The HC mode consists of diffusion jet flame of axial direction and premixed cyclone flame of tangential direction in order to stabilized the diffusion jet flame. The results showed that the flame stability of HC mode is significantly enhanced than that of DC mode through the change of mixing characteristics by modifications of fuel nozzle. In addition, the reductions of CO and NOx emission in HC mode, as compared with that for the DC mode, is large than about 50% in stable region. Also, even using the low calorific fuel as $CO_2$-blended gas, it is identified that the cyclone jet hybrid combustor has the high performance of flame stability.