• 제목/요약/키워드: Secondary Fuel

검색결과 323건 처리시간 0.031초

통합형 연료분사장치를 통한 연소불안정 저감 (Reduction of combustion instability using flame holder integrated injector)

  • 황용석;이종근;박익수;최호진;진유인;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.432-437
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    • 2010
  • V-gutter 형 화염안정화장치를 장착한 공기흡입식 엔진의 연소기에서 발생하는 저주파 연소 불안정을 저감시키기 위해 화염안정화장치 뒤쪽에 2차 연료를 분사하는 장치를 고안하였다. 해당 장치는 모델 연소장치를 통해 성공적으로 발생된 110~120 Hz, 180dB 크기의 저주파 연소불안정을 84%까지 저감시키는 데에 성공하였다. 연소불안정의 감소는 2차 연료 공급 유량에만 의존하였으며, 특정 값 이상의 연료 공급량에서만 효과가 나타났다. 이와같은 결과는 2차 연료 공급에 의해 화염안정화장치 뒷면의 화염이 주연료 공급량의 섭동과 독립적으로 유지되어 연소 시스템과 연소기의 음향 시스템의 연계를 끊어주기 때문인 것으로 생각된다.

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이중선회 확산화염의 화염특성에 관한 실험적 연구 (An Experimental Study on Combustion Characteristics of Double Swirl Difussion Flame Burner)

  • 최원재;이진호;김세원;김경수;류태우
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.162-168
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    • 2000
  • This paper conducted experimental study of turbulent diffusion flame, equipped with a unique double swirler combustor for gas fuel. The burner has two vane swirlers which are fitted to primary, secondary air channel. Temperature, and NOx emission concentrations are measured in combustion flame region and velocity in cold flow for various primary/secondary air ratio conditions. The results showed the characteristics of swirl flame and decreasing NOx concentrations with increasing primary/secondary air ratio.

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촉매가 장착된 가솔린엔진에서 동기화된 2차공기분사에 의한 배기 탄화수소 저감 (Reducing Exhaust Hydrocarbon at Gasoline Engine with Catalytic Converter using Synchronized Secondary Air Injection)

  • 심현성;민경덕;정석호
    • 한국자동차공학회논문집
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    • 제9권2호
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    • pp.67-74
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    • 2001
  • A synchronized secondaty air injection method has been developed to hydrocarbon emission by injecting secondary air intermittently into exhaust port. The method has been tested in a single cylinder spark-ignition engine operating at cold-steady / cold-start conditions. Effects of air injection timing, intake pressure and engine air-fuel ratio have been investigated at cold-steady condition. Also, hydrocarbon emission and exhaust gas temperature with catalytic conberter are compared with a continuous SAI method and base condition at cold-start condition. Resules show that hydrocarbon reduction rate and exhaust gas temperature are sensitive to the timing of synchronized SAI. At cold-steady condition, HC emission is minimum at engine air-fuel ratio of 10. At cold-start condition, the accumulated hydrocarbon emission during the first 120 s decreases about 56% and 22% with the synchronized and continuous SAI, respectively, compared to that of base condition.

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연료 및 공기의 혼합구조가 로타리 킬른 용 버너 화염에 미치는 영향 (Mixed Structure Effect of Fuel and Air on Rotary Kiln Burner Flame)

  • 김영호;이철우;김인수;임영빈
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.339-342
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    • 2014
  • Rotary kiln produces lime from limestone through thermal decomposition. Ring formation in kiln internal wall is known issue that decreases productivity. The cause of ring formation is temperature imbalance as flame leans toward upper wall. Therefore, burner nozzle geometry was changed to improve air-fuel mixing state which leads to prevention of ring formation. CFD simulation and experimental test were performed in this study to investigate the effect of air-fuel mixing on flame structure, temperature and $NO_X$ concentration. It is shown that combustion efficiency has been enhanced and $NO_X$ concentration has been decreased by using swirl flow for secondary combustion air. It's also shown that flame has been straightened by using straight flow for secondary combustion air.

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다공스로틀밸브가 혼합기 유동과 연료 분무의 2차 미립화에 미치는 영향 (Effects of Perforated Throttle Valve on the Mixture Flow and Secondary Atomization of Fuel Spray)

  • 조병옥;조행묵;이창식
    • 한국분무공학회지
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    • 제1권3호
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    • pp.60-66
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    • 1996
  • Finely atomized fuel droplet and good mixed mixture plays very important in improving combustion efficiency in an spark ignition engine. And combustion efficiency has influence directly on the engine power, fuel consumption rate and pollutant emission. In this study, perforated throttle valve which has relatively low value of PR has been developed and studied for the purpose of improving those aims. As a result of this study, it has been verified that the perforated throttle valve makes droplet more finely, and also proved that has a function of contributing to form good mixed mixture, especially in mixture preparation system of carburetor or SPI type spark ignition engine.

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고온 고압하에서의 DME 연료 분무 및 증발 특성 (Spray and Evaporation Characteristics of DME fuel at the High pressure and temperature)

  • 김형준;서현규;이창식
    • 한국분무공학회지
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    • 제12권2호
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    • pp.101-107
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    • 2007
  • The purpose of this study is to analyze spray and evaporation characteristics of DME fuel at the high pressure and temperature. For the numerical analysis of dimethyl ether(DME) fuel spray characteristics, hybrid breakup model was applied to the DME spray and its breakup process. In order to obtain experimental results for comparison with the predicted ones, the visualization of the spray evolution process was executed by using a Nd:YAG laser. Also, the numerical investigation was conducted by the two hybrid models for primary and secondary breakup of the DME spray. The primary breakup model was used the Kelvin-Helmholtz(KH) breakup model. In the secondary breakup process, Rayleigh-Taylor(RT) and Drop Deformation Breakup(DDB) model was applied. The results of this study provide the macroscopic characteristics of the spray such as spray tip penetration and cone angle, and prediction accuracy of the two hybrid model.

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75톤급 로켓엔진용 연료펌프의 수력성능시험 (Hydraulic Tests of Fuel Pump for 75-ton class Liquid Rocket Engines)

  • 김대진;홍순삼;최창호;노준구;김진한
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.78-81
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    • 2009
  • 연료펌프에 대한 수력성능시험을 상온의 물을 매질로 하여 실시하였다. 시험된 연료펌프는 개방형 가스발생기 방식의 75톤급 액체로켓엔진에 적용할 목적으로 개발 중에 있다. 시험 결과, 연료펌프는 설계요구조건을 만족하였으며, 설계 유량에서의 양정과 효율은 수치해석에서 추정된 값보다 높았다. 또한 후방 베어링의 출구 압력이 예상보다 높았는데 이는 바이패스 배관의 입구가 좁기 때문이었다. 그리고 바이패스 곡관부의 차압 측정으로 누설 유량을 유추할 수 있었다.

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공기보조형 가솔린 연료분사기의 흡기포트내 연료분무 거동에 관한 연구 (A Study on the Spray Behavior of Air-Assist Type Gasoline Fuel Injector in Intake Port)

  • 노병준;강신재;김원태
    • 대한기계학회논문집B
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    • 제23권1호
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    • pp.92-103
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    • 1999
  • The fuel spray behavior in the intake port of an electronic control port irijection gasoline engine has a strong influence on engine performance, exhaust emission and fuel consumption. Thus, in this study, fuel spray behavior and flow characteristics of the air assist gasoline spray injected into a suction flow in a simulated rectangular intake port have boon investigated. Macro-behavior of spray characteristics was investigated by means of visualization and the measurements of SMD and velocity were made by PDPA. For analysis the flow field with droplets size, droplets are classified five droplets size groups. As a result, the normal distance of suction flow increasing, the relatively large droplets distribution and SMD increase because small droplets easily follow suction flow. Near impinging wail, after impinging against the wall, secondary atomized small droplets of D < $30{\mu}m$ bound from the wall. And the increasement of suction flow progress to the large droplets of D > $100{\mu}m$ distribution. Therefore, SMD are apparently increased near impinging wall, Z/d = 9.0.

로켓엔진용 연료펌프 전산유동해석

  • 노준구;최창호;김진한
    • 항공우주기술
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    • 제3권2호
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    • pp.183-190
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    • 2004
  • 액체로켓용 연료펌프의 설계를 검증하기 위해 상용 3차원 유동해석 소프트웨어를 이용하여 설계점 성능을 예측하였다. 연료펌프의 성능과 축추력에 영향을 미치는 누설유량에 대한 예측의 정확도를 높이기 위해 인듀서, 임펠러, 볼류트 및 2차 유로를 계산영역으로 설정하였으며 인듀서/임펠러/누설유로/볼류트 사이의 경계면에 혼합면 기법을 적용하여 계산에 소요되는 시간을 줄이고자 하였다. 유동해석을 통해 예측된 수력성능은 설계요구조건을 만족시키는 것으로 나타났으나 축추력이 허용치에 비해 크게 예측되어 이를 감소시키기 위한 설계변경이 이루어졌다. 변경된 설계안에 대한 유동해석을 수행한 결과 연료펌프의 수력성능은 유지되면서 축추력은 처음의 설계안에 비해 30% 수준으로 크게 감소하였음을 확인할 수 있었다.

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Determination of escape rate coefficients of fission products from the defective fuel rod with large defects in PWR

  • Pengtao Fu
    • Nuclear Engineering and Technology
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    • 제55권8호
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    • pp.2977-2983
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    • 2023
  • During normal operation, some parts of the fission product in the defective fuel rods can release into the primary loops in PWR and the escape rate coefficients are widely used to assess quantitatively the release behaviors of fission products in the industry. The escape rate coefficients have been standardized and have been validated by some drilling experiments before the 1970s. In the paper, the model to determine the escape rate coefficients of fission products has been established and the typical escape rate coefficients of noble gas and iodine have been deduced based on the measured radiochemical data in one operating PWR. The result shows that the apparent escape rate coefficients vary with the release-to-birth and decay constants for different fission products of the same element. In addition, it is found that the escape rate coefficients from the defective rod with large defects are much higher than the standard escape rate coefficients, i.e., averagely 4.4 times and 1.8 times for noble gas and iodine respectively. The enhanced release of fission products from the severe secondary hydriding of several defective fuel rods in one cycle may lead to the potential risk of the temporary shutdown of the operating reactors.