• 제목/요약/키워드: 화염가시화

검색결과 114건 처리시간 0.021초

파일럿분사에 의한 바이오디젤유의 연소과정에 관한 연구 (A Study on Combustion Process of Biodiesel Fuel with Pilot Injection in a Common-rail Diesel Engine)

  • 방중철;김성훈
    • 한국자동차공학회논문집
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    • 제19권3호
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    • pp.146-153
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    • 2011
  • American NREL (National Renewable Energy Laboratory) reported that BDF20 could reduce PM, CO, SOx, and cancerogenic matters by 13.6%, 9.3%, 17.6%, and 13% respectively, compared to diesel fuel. BDF20 has been being tested on garbage trucks and official vehicles at Seoul City, which is positive on air environment, but negative on combustion by higher viscosity in winter season. This study investigated the combustion characteristics by applying pilot injection for improving the deterioration of combustibility caused by the higher viscosity of the BDF20 with the combustion flames taken by a high-speed camera and the cylinder pressure diagram. A 4-cycle single-cylinder diesel engine was remodeled to a visible 2-cycle engine taking the flame photographs, which has a common-rail injection system. The test was done laboratory temperature at $5{\sim}6^{\circ}C$. The results obtained are summarized as follows, (1) In the case of without pilot injection, the flame propagation speed was slowed and the maximum combustion pressure became lower. The phenomena became further aggravated as the fuel viscosity gets higher. (2) In the case of with pilot injection, early stage of combustion such as rapid ignition timing and flame propagation was activated since intermediate products formed by pilot injection act as a catalyst for combustion of main fuel.

Swirl Groove Piston에 의한 바이오 디젤연료의 연소과정에 관한 연구 (A Study on Combustion Process of Biodiesel Fuel using Swirl Groove Piston)

  • 방중철;김성훈
    • 한국자동차공학회논문집
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    • 제17권1호
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    • pp.105-113
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    • 2009
  • The performance of a direct-injection type diesel engine often depends on the strength of swirl or squish, shape of combustion chamber, the number of nozzle holes, etc. This is of course because the combustion in the cylinder was affected by the mixture formation process. In this paper, combustion process of biodiesel fuel was studied by employing the piston which has several grooves with inclined plane on the piston crown to generate swirl during the compression stroke in the cylinder in order to improve the atomization of high viscosity fuel such as biodiesel fuel and toroidal type piston generally used in high speed diesel engine. To take a photograph of flame, single cylinder, four stroke diesel engine was remodeled into two stroke visible engine and high speed video camera was used. The results obtained are summarized as follows; (1) In the case of toroidal piston, when biodiesel fuel was supplied to plunger type injection system which has very low injection pressure as compared with common-rail injection system, the flame propagation speed was slowed and the maximum combustion pressure became lower. These phenomena became further aggravated as the fuel viscosity gets higher. (2) In the case of swirl groove piston, early stage of combustion such as rapid ignition timing and flame propagation was activated by intensifying the air flow in the cylinder. (3) Combustion process of biodiesel fuel was improved by the reason mentioned in paragraph (2) above. Consequently, the swirl grooves would also function to improve the combustion of high viscosity fuel.

저압 분사조건에 따른 직접분사 LPG의 분무 및 연소특성 연구 (An Study on Spray and Combustion Characteristics of Direct Injection LPG under Low Pressure Injection Condition)

  • 황성일;정성식;염정국;이진현
    • 한국가스학회지
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    • 제20권1호
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    • pp.52-61
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    • 2016
  • 액화석유가스는 환경 친화적이며 에너지 효율성과 출력성능이 뛰어나 실용성이 높고, 경쟁연료에 비해 가격 경쟁력이 우수하기 때문에 촉망받는 대체연료 중 하나로 간주된다. 스파크점화 엔진에서 직분식 기술은 엔진 체적효율을 눈에 띄게 증가시키며, 상대적으로 더 높은 연소효율이 가능한 성층급기를 이용해 엔진을 작동시킨다. 본 연구에서는 가솔린직접분사 엔진의 원리를 적용하여 가시화 시스템을 장착한 연소실을 설계하였다. 이를 통해 스파크점화직분식 LPG의 점화성과 화염전파 과정을 디지털 방식으로 기록하고 분석하였다. 이러한 연구의 결과는 스파크점화직분식 LPG 엔진의 설계 및 최적화를 위한 광범위한 기초 자료로서 기여하고자 한다.

실기체급 비행체 모델에 대한 M4 준자유류 시험 (M4 Semi-Freejet Test with Full-scale Vehicle Model)

  • 배주현;임창원;최호진;진상욱;김정우
    • 한국추진공학회지
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    • 제26권5호
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    • pp.63-73
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    • 2022
  • 국내 설비를 활용하여 실기체급 비행체 모델에 대한 M4 준자유류 시험을 수행하였다. 시험장치 및 비행체 모델은 반복적인 전산유체해석을 통해 통합적으로 설계/제작되었고, 해당 설비를 목표 시험 조건까지 가동하여 시험장치의 M4 노즐이 완전히 팽창하는 것을 확인하였다. 비행체 모델의 흡입구 주변의 가시화 영상을 획득하여 경사충격파가 생성되면서 비행체의 흡입구가 시동하는 것을 관측하였다. 비행체의 가변노즐을 구동하여 배압을 조절하면서 비행체 내부 유로의 벽면 압력 분포를 획득하였고, 연소기 내 화염안정화장치에서 점화용 토치 점화 및 점화보조제의 연소 현상을 관측하였다.