• Title/Summary/Keyword: 가스분사 시스템

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Measurements and Calculation of Injection Mass Rate of LFG for Intake Injection in Spark Ignition Engines (불꽃점화 엔진의 흡기관 분사를 위한 매립지가스 분사량의 측정 및 계산)

  • Kim, Kyoungsu;Choi, Kyungho;Jeon, Wonil;Kim, Bada;Lee, Daeyup
    • Journal of the Korean Institute of Gas
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    • v.25 no.4
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    • pp.36-42
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    • 2021
  • When the landfill gas generated at the landfill site is released into the atmosphere, methane gas with a high global warming potential is emitted, which adversely affects climate change. When methane contained in landfill gas is used as fuel for internal combustion engines and burned to generate electricity, it is emitted into the atmosphere in the form of carbon dioxide, which can contribute to lowering the global warming potential. Therefore, in order to use the landfill gas as fuel for power generation using an internal combustion engine, it is important to increase the thermal efficiency of the engine. Thus, it is necessary to use a fuel supply system in which gas is injected using an electronically controlled injector at an intake port for each cylinder rather than a fuel supply technology using the conventional mixer technology. In order to use the electronically controlled gas injection method, it is important to accurately measure the mass flow rate according to the conditions of using landfill gas. For this, a study was conducted to measure the injection amount and calculate them in order for the intake port gas injection of landfill gas.

대형 디젤대체용 LPG 엔진개발

  • Gang, Geon-Yong
    • LP가스
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    • s.71
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    • pp.49-53
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    • 2000
  • 대형디젤엔진의 대체용으로 LPG 엔진을 개발함에 있어서 차세대 연료공급방식인 LPG 연료의 액상분사방식을 채택하여 기존의 믹서방식의 연료공급시스템을 가진 LPG 엔진보다 고출력, 고효율, 저공해성을 추구하고자 하였다. 이를 위한 기초연구로서 먼저 단기통 연소엔진을 이용하여 대형엔진에 LPG 연료 적용 가능성, 액상분사 시스템을 포함한 여러 가지 연료공급방식에 따른 엔진의 성능파악, 대형엔진에 적합한 최적 선회비의 결정, 연료조성에 따른 엔진성능의 변화 등을 알아보았다. 실험결과, 대형엔진에 LPG 연료의 적용은 아무런 문제점이 없었으며 LPi 연료공급방식은 다른 방식에 비해서 10%정도의 체적효율 및 출력의 증가를 확인할 수 있었다. 최적의 선회비는 2.0 부근에서 형성되었고, 연료 조성은 프로판 대 부탄의 비율이 60 : 40에서도 정상적으로 운전됨을 확인하였다. 시제품 엔진의 경우, 과급방식의 KL6i 엔진을 개발하기 앞서 좀더 기술적 접근이 용이한 자연흡입방식의 K-1엔진의 개발이 선행되었으며 현재 개발 진행중인 K-1엔진의 성능평가 결과, 기존의 디젤엔진에 비해 출력성능이 20% 정도 향상됨을 확인할 수 있었다. 특히 대형차량에서 중요시 생각되는 저속토크 성능이 매우 우수한 것으로 파악되었다. 이러한 결과를 바탕으로 단기통 연소엔진에서 확인된 최적화된 연료조성과 선회비를 향후 K-1엔진에 적용할 예정이다. 최근 열린 가스학회 추계발표회와 LPG자동차세미나의 주요내용을 게재한다.

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Study on Development of High-Speed Small Engine Controlled by EFI (Electronic Fuel Injection) (소형 고속 전자제어 연료분사 엔진 개발에 관한 연구)

  • Lee Seungjin;Ryu Jeongin;Choi Kyonam;Jeong Dongsoo
    • Journal of Energy Engineering
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    • v.14 no.3 s.43
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    • pp.173-179
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    • 2005
  • Fuel injection system has more benefits in power, fuel consumption and emission than carburetor system even in high speed small engine. Up to date fuel injection system is used in motor car but is not used in motorcycles in Korea. EFI (Electronic fuel injection) system which has ECU can control precise fuel supply to variable RPM in engine. The purpose of this study is the investigation of effects of fuel injection system to improve the engine performance and efficiency in variable revolution of high speed small engine which is 4 Valves SOHC single cylinder engine used in motorcycle.

Comparison Study on System Design Parameters of Gas Generator Cycle Liquid Rocket Engine (가스발생기 사이클 액체로켓엔진의 시스템 설계 인자 비교)

  • Nam Chang-Ho;Park Soon-Young;Moon Yoon-Wan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.220-223
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    • 2005
  • System design parameters of gas generator cycle liquid rocket engines were investigated and compared in the present study. Characteristic velocity of combustor, pressure drop of combustor injector, exit pressure of pump, pump efficiency and specific power of turbine were considered as a system design parameter. The result shows the characteristic velocity is in the range of 1700-1770 m/s, pressure drop of combustor injector, 4-10 bar, pump exit pressure ratio to combustion pressure, 120-230%, pump efficiency, 60-80%, specific power of turbine, $0.28-0.58MW{\cdot}s/kg$.

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Performance evaluation of a steam injected gas turbine CHP system using biogas as fuel (바이오 가스를 연료로 사용하는 증기분사 가스터빈 열병합발전 시스템의 성능분석)

  • Kang, Do-Won;Kang, Soo-Young;Kim, Tong-Seop;Hur, Kwang-Beom
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.6
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    • pp.57-62
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    • 2010
  • MW-class gas turbines are suitable for distributed generation systems such as community energy systems(CES). Recently, biogas is acknowledged as an alternative energy source, and its use in gas turbines is expected to increase. Steam injection is an effective way to improve performance of gas turbines. This study intended to examine the influence of injecting steam and using biogas as the fuel on the operation and performance a gas turbine combined heat and power (CHP) system. A commercial gas turbine of 6 MW class was used for this study. The primary concern of this study is a comparative analysis of system performance in a wide biogas composition range. In addition, the effect of steam temperature and injected steam rate on gas turbine and CHP performance was investigated.

CFD Analysis on Gas Injection System of Solid SCR for NOx Reduction of Exhaust Emissions in Diesel Engine (디젤엔진 배출가스의 질소산화물 저감을 위한 Solid SCR용 가스분사 시스템의 전산유체해석 연구)

  • Lee, Hoyeol;Yoon, Cheon Seog;Kim, Hongsuk
    • Transactions of the Korean Society of Automotive Engineers
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    • v.22 no.5
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    • pp.73-83
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    • 2014
  • CFD(computational fluid dynamics) model is developed to simulate direct injection of ammonia gas phase from ammonia transporting materials into the SCR catalyst in the exhaust pipe of the engine with solid SCR. Configurations of one-hole and four-hole nozzle, circumferential type, porous tube type, and the effect of mixer configurations which commonly used in liquid injection of AdBlue are considered for complex geometries. Mal-distribution index related to concentration of ammonia gas, flow uniformity index related to velocity distribution, and pressure drop related to flow resistance are compared for different configurations of complex geometries at the front section of SCR catalyst. These results are used to design the injection system of ammonia gas phase for solid SCR of target vehicle.

Effect of the distance between the adjacent injectors on penetration and mixing characteristics of the jet in supersonic crossflow (수평 배치된 분사구의 배치 간격에 따른 초음속 유동장 내 분사 유동의 침투 및 혼합 특성)

  • Kim, Sei Hwan;Lee, Hyoung Jin
    • Journal of Aerospace System Engineering
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    • v.12 no.4
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    • pp.81-89
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    • 2018
  • In the present study, a numerical investigation was conducted to analyze the effect of the distance between the adjacent injectors on the characteristics of flow structure, fuel penetration, and air/fuel mixing. Numerical results were validated with experimental data using a single injection. Subsequently, the same injector geometry and properties were applied on a non-reacting flow simulation with multiple injectors. Total pressure loss, penetration height, and mixing efficiency were compared with the distance between the injectors. The results showed that each injected gas merged into a single stream, resulting in the 2D-like flow fields under the condition of short distance and lower mixing efficiency along with higher total pressure loss. When the distance between the injectors increased, total pressure loss reduced and mixing efficiency increased due to the weakening of interactions between the injected gases.

Structural Analysis of Snap Ring in Thrust Cut-Off System (Thrust Cut-Off 시스템에서의 스냅링 구조해석)

  • 김경희
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2000.11a
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    • pp.21-21
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    • 2000
  • Thrust Cut-Off 시스템은 로켓 발사체의 분리시의 충격에 의한 비행방향오차 및 비행거리를 감소하고 Pay-Load 부에 추진력을 증가시키고 분리된 추진 기관부의 낙하위치 예측을 용이하게 한다. 이와 같이 중요한 역할을 하게되는 Thrust Cut-Off 시스템에서 스냅링은 핵심적인 역할을 하게 된다. 정상적인 추진체의 작동 시에는 고압의 연소가스를 지탱하고 분리 시에는 쉽게 분리되어 연소가스를 역 분사 시켜야한다.(중략)

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Effects of Swirl and Combustion Parameters on the Performance and Emission in a Turbocharged D.1. Diesel Engine (선회유동 및 연소인자가 터보과급 디젤엔진의 성능 및 배기가스특성에 미치는 영향)

  • 윤준규;차경옥
    • Journal of Energy Engineering
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    • v.11 no.2
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    • pp.90-98
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    • 2002
  • The effects of swirl and combustion parameters on the performance and emission in a turbo-charged D.I. diesel engine of the displacement 9.4L were studied experimentally in this paper. Generally the swirl in the combustion process of diesel engine promotes mixing of the injection fuel and the intake air. It is a major factor to improve the engine performance because the fuel consumption and NO$_{x}$ is trade-off according to the high temperature and high pressure of combustion gas in a turbocharged D.I. diesel engine, it's necessary to thinking over the intake and exhaust system, the design of combustion bowl and so on. In order to choose a turbocharger of appropriate capacity. As a result of steady flow test, when the swirl ratio is increased, the mean flow coefficient is decreased, whereas the gulf factor is increased. Also, through engine test its can be expected to meet performance and emissions by optimizing the main parameter's; the swirl ratio is 2.43, injection timing is BTDC 13$^{\circ}$ CA, compression ratio is 16, combustion bowl is re-entrant 5$^{\circ}$, nozzle hole diameter is $\Phi$0.28*6, turbocharger is GT40 model which are compressor A/R 0.58 and turbine A/R 1.19.

A Study on the Effects of Fuel Rail Pressure and Engine Speed on Gas Fuel System (연료레일 압력과 엔진 속도가 가스연료 시스템에 미치는 영향에 관한 연구)

  • Kwak, Youn-Ki
    • The Journal of Korea Institute of Information, Electronics, and Communication Technology
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    • v.11 no.5
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    • pp.579-585
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    • 2018
  • This study is to figure out the fuel injection characteristics according to the injection pressure and engine speed in the fuel supply system for gas fuel. The fuel rail pressure was from 1.5 to 6.0 bar by 1.5 bar increment and engine speed was set 1,000 ~ 6,000 RPM at interval of 1000 RPM. Considering the real engine operation, the injection pulse width was set 2.5ms, 5.0ms, and 13.0ms which correspond low, mid and high load condition respectively. In conclusion, in case of 100cc fuel rail, 4.5 bar of injection pressure showed best performance and the minimum required injection quantity 53cc which guarantees engine output can be obtained in each 1000~ 6000 rpm engine speed.