• 제목/요약/키워드: Natural Gas Combustion

검색결과 266건 처리시간 0.026초

모형 가스터빈 연소기에서 화염구조와 연소불안정 특성에 대한 실험적 연구 (An Experimental Study on Flame Structure and Combustion Instability Characteristics in Model Gas Turbine Combustor)

  • 박성순;김민기;윤지수;윤영빈
    • 한국추진공학회지
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    • 제15권4호
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    • pp.26-34
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    • 2011
  • 스월러를 가진 천연가스 연료분사기가 장착된 희박 예혼합 연소기에서 화염구조의 일부분인 재순환 영역의 형성이 연소불안정에 미치는 영향에 대하여 실험적으로 연구를 진행하였다. PIV 계측기법으로 연소장에서의 화염의 안정화 그리고 불안정한 영역에서 유동장을 확인해본 결과 스월러에 의한 재순환 영역은 화염의 안정화 및 난류의 강도뿐만 아니라 재순환영역 형성의 크기에 따른 화염 재점화에도 영향을 미쳐 연소불안정 발생의 원인이 되는 열방출 섭동과 매우 밀접한 관계가 있음을 확인하였다.

모형 가스터빈 연소기에서 화염구조와 연소불안정 특성에 대한 실험적 연구 (An Experimental Study on Flame Structure and Combustion Instability Characteristics in Model Gas Turbine Combustor)

  • 박성순;김민기;윤지수;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.445-452
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    • 2011
  • 스월러를 가진 천연가스 연료분사기가 장착된 희박 예혼합 연소기에서 화염구조의 일부분인 재순환 영역의 형성이 연소불안정에 미치는 영향에 대하여 실험적으로 연구를 진행하였다. PIV 계측기법으로 연소장에서의 화염의 안정화 그리고 불안정한 영역에서 유동장을 확인해본 결과 스월러에 의한 재순환영역은 화염의 안정화 및 난류의 강도뿐만 아니라 재순환영혁 형성의 크기에 따른 화염 재점화에도 영향을 미쳐 연소불안정 발생의 원인이 되는 열방출 섭동과 매우 밀접한 관계가 있음을 확인하였다.

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

  • 조은성;정석호
    • 한국연소학회지
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    • 제9권4호
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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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연료전지 시스템을 적용한 하이브리드 굴삭기 해석 모델 개발 (Development of Simulation Model for PEMFC Hybrid Excavator)

  • 이세영
    • 드라이브 ㆍ 컨트롤
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    • 제16권3호
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    • pp.16-22
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    • 2019
  • Due to the rise in energy consumption and natural resource prices, the demand to improve energy efficiency in the construction machine has been highlighted. Even though many researchers have contributed to the development of the technology, CO2 gas emissions of heavy machinery remains high. One of the most significant problems of the novel excavator with internal combustion engines is the emission of harmful gas. To reduce emissions in the construction machine, it is necessary to replace the internal combustion engines with the alternative one. To overcome those problems, this paper focuses on the adoption of PEMFC hybrid engine for the excavator system. An internal combustion engine is replaced by new structures with fuel cell, battery and ultra capacitor. The proposed system has been designed and modeled using Simcenter Amesim software and compared with the conventional one through simulation results.

희박 예혼합 모형 가스터빈 연소기의 화염구조와 배기특성에 관한 실험적 연구 (Experimental Investigation on Flame Structure and Emission Characteristics in a Lean Premixed Model Gas Turbine Combustor)

  • 이종호;김대현;전충환;장영준
    • 대한기계학회논문집B
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    • 제28권4호
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    • pp.425-432
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    • 2004
  • The objective of this study is a qualitative comparison between line-integrated OH chemiluminescence(OH$\^$*/) image and its Abel inverted image to investigate the flame structure at different phase of the oscillating pressure field. PIV(Particle Image Velocimetry) measurements were conducted under non-reacting conditions to see the global flow structure and NOx emission was measured to investigate the effect of fuel-air premixing on combustion instability and emission characteristics. Experiments were carried out in an atmospheric pressure, laboratory-scale dump combustor operating on natural gas. Combustion instabilities in present study exhibited a longitudinal mode with a dominant frequency of ∼341.8㎐, which corresponded to a quarter wave mode of combustor. Heat release and pressure waves were in-phase when instability occurred. Results gave an insight about the location where the strong coherence of pressure and heat release existed. Also an additional information on active control to suppress the combustion instabilities was obtained. For lean premixed combustion, strong correlation between OH$\^$*/ and NOx emissions was expected largely due to the exponential dependence of thermal NOx mechanism on flame temperature.

희박 예혼합 모형 가스터빈 연소기의 화염구조와 배기특성에 관한 실험적 연구 (Experimental Investigation on Flame Structure and Emission Characteristics in a Lean Premixed Model Gas Turbine Combustor)

  • 문건필;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.356-361
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    • 2003
  • The objective of this study is a qualitative comparison between line-integrated OH chemiluminescence ($OH{\ast}$) image and its Abel inversion image at different phase of the oscillating pressure field. PIV(Particle Image Velocimetry) measurements were conducted under non-reacting conditions to see the global flow structure. Also NOx emission was measured to investigate the effect of fuel-air premixing on combustion instability and emission characteristics. Experiments were carried out in an atmospheric pressure, laboratory-scale dump combustor operating on natural gas. Combustion instabilities in present study exhibited a longitudinal mode with a dominant frequency of ${\sim}341.8$ Hz, which corresponded to a quarter wave mode of combustor. Heat release and pressure waves were in-phase when instability occurred. Results gave an insight about the location where the strong coherence of pressure and heat release existed. Also an additional information on active control to suppress the combustion instabilities was obtained. For lean premixed combustion, strong correlation between $OH{\ast}$ and NOx emissions was expected largely due to the exponential dependence of thermal NOx mechanism on flame temperature.

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고압 천연 가스 인젝터의 분무 특성에 관한 연구 (An Investigation on the Spray Characteristics of a Compressed Natural Gas Injector)

  • 삭다 통차이;강유진;임옥택
    • 한국수소및신에너지학회논문집
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    • 제29권2호
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    • pp.219-225
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    • 2018
  • This study was carried out to investigate the injection characteristics of 800 kPa compressed natural gas compressed natural gas (CNG) injector developed in Korea. The CNG injector with multi-holes, employed in this experiment, was designed to inject CNG in the manifold at high pressure of 800 kPa. The spray macroscopic visualization test was carried out via Schlieren photography to study fuel-air mixing process. The fundamental spray characteristics, such as spray penetration, spray cone angle and spray velocity, were evaluated in the constant volume combustion chamber (CVCC) with varying the constant back pressure in CVCC from 0 to 1.8 bar. For the safety reason, nitrogen ($N_2$) and an acetone tracer were utilized as a surrogate gas fuel instead of CNG. The surrogate gas fuel pressures were controlled at 3, 5.5, and 8 bar, respectively. Injection durations were set at 5 ms throughout the experiment. The simulating events of the low engine speed were arranged at 1,000 rpm. The spray images were recorded by using a high-speed camera with a frame rate of 10,000 f/s at $512{\times}256pixels$. The spray characteristics were analyzed by using the image processing (Matlab). The results showed the significant difference that higher injection pressure had more effect on the spray shape than the lower injection pressure. When the injection pressure was increased, the longer spray penetration occurred. Moreover, the linear relation between speed and time are dependent on the injection pressure as well.

선박용 가솔린/CNG Bi-fuel 엔진개조 기술 개발 (A Development of Converting Technology for the Marine Gasoline/CNG Bi-fuel Engine)

  • 박명호
    • Journal of Advanced Marine Engineering and Technology
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    • 제34권5호
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    • pp.632-637
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    • 2010
  • 천연가스는 메탄을 주성분으로 하는 청정한 대체연료로 자동차나 트럭 등에 압축천연가스와 액화천연가스 형태로 사용할 수 있다. 그리고, 천연가스만을 사용하는 전소엔진과 가솔린 및 천연가스를 동시에 사용할 수 있는 겸용엔진이 있으며, 특히, 겸용엔진의 경우 두가지 연료를 동시에 사용할 수 있는 것으로 정의할 수 있다. 본 연구에서는 선박용 가솔린 시스템을 인젝터, 레귤레이터, 연료탱크 및 전자제어장치로 구성된 압축 천연가스 겸용시스템으로 전환시켜 연료시스템과 동력값을 비교하였다. 그 결과, 천연가스엔진의 경우 적은 배출가스를 나타내었으며 최대동력은 가솔린엔진과 비교 약 7%정도 감소함을 확인할 수 있었다.

5MW 발전용 가스터빈 엔진 연소기 성능시험 (Performance Test of 5MW Gas Turbine Engine Combustor)

  • 박부민;김형모;최영호;양수석;천무환
    • 한국연소학회지
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    • 제13권4호
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    • pp.37-46
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    • 2008
  • Performance test of 5MW class gasturbine combustor was carried out at combustor test facility of KARI(Korea Aerospace Research Institute). The combustor is dry low NOx type premixed combustor and fuel is natural gas. The characteristics of combustor were measured including emission, pressure pulsation and exit temperature distribution. Optimum operation point of combustor was found by changing parameters like fuel ratio between pilot and main burner. The test result showed that the combustor performance is sufficient to satisfy the gasturbine system requirement.

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산지별 천연가스의 화염 안정영역에 관한 실험적 연구 (Experimental Study on the Flame Stable Region of Natural Gases from Various Producing Districts)

  • 이창언;홍성창;정영식;유현석;이승준;허재영;황철홍
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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    • pp.69-75
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    • 2007
  • In this study, the difference of flame stability zone for natural gases from producing districts was studied experimentally using a new type of flame stability diagram. The similarity of stable flame zone between a domestic appliance and an interchangeability test(IT) burner is also examined. As a result, the stable flame zones expressed by limits curves of flame lifting and yellow tipping show the similar results in a domestic gas range and IT burner. Furthermore, IT burner can reproduce the flash back phenomena and show the distinct difference of fuel type as the burner diameter is increased. To suggest the new type of flame stability diagram in the respect of fuel interchangeability, the air flowrate and Wobbe fuel flowrate were adopted as axis coordinates. It can be identified that the new diagram can provide the useful information on the difference of flame stability zone, heat input rate and air-fuel ratio when a fuel is altered to other fuels under the identical operating conditions. Finally, the stable flame zones for natural gas of 6 type are compared, and the detailed information to use as the interchangeability fuels of standard natural gas is provided using the new type of flame stability diagram.

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