• Title/Summary/Keyword: combustion performance test

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[ NOX ] Emission Characteristics in Radiant Tube Burner with Oscillating Combustion Technology (맥동연소기술이 접목된 복사관 버너에서의 NOX 배출 특성)

  • Cho, Han-Chang;Cho, Kil-Won;Kim, Hoo-Joong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.32 no.2
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    • pp.100-106
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    • 2008
  • An experimental study was carried out in a small-scale test furnace to investigate the performance, such as $NO_X$ emission, enhancement of heat transfer, uniformity of temperature, and etc, of oscillating combustion applied in radiant tube burner system. A premixed type burner and a cyclic oscillating control valve were designed and used. The fuel, used commercial LPG in this study, was only oscillated using the cyclic oscillating control valve. As oscillating combustion was applied in radiant tube burner system, it is found that $NO_X$ emission, compared to no oscillation, could be reduced by 38% at $90{\sim}120rpm\;(1.5{\sim}2.0Hz)$. However, as oscillating frequency was increased, effect of abatement of $NO_X$ emission is gradually reduced. From the measurement of furnace heating time from $100^{\circ}C$ to $720^{\circ}C$, heat transfer is increased by 11.5% at the oscillation of 120rpm. Temperature distribution of radiant tube surface is more uniform at oscillation of 120rpm with decrease of the peak temperature and increase of low temperature. From these results, it is confirmed that oscillating combustion is useful in radiant tube burner system.

The Effect of Air and Spray Turbulence on the Progress in a D.I. Diesel Engine(II)-Combustion Chamber Design for the Use of Emulsified Diesel Oil with Water Particles- (직접분사식 디젤기관의 연소실 형상과 화염의 발달 (2)-유화액연료용 연소실의 형상-)

  • ;;Ohta, Motoo
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.11
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    • pp.3054-3062
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    • 1995
  • Recently, the improvement of fuel economy and the reduction of exhaust smoke and NOx have been successfully achieved by supplying diesel engines with emulsified diesel oil with water particles. In the present paper, the difference between the combustion of injected emulsified fuel and that of diesel oil spray is clarified by means of taking high-speed and color photographs of the flames in the engine cylinder. As the results, the two kinds of fuels show different combustion behavior each other in the growth of initial flame and in the termination of combustion process in the cylinder. Then, suitable combustion chamber design for the use of emulsified fuel is discussed on the basis of experimental data for various distribution of spray in different kinds of piston cavities. Some methods of clearing troubles caused by emulsified fuel injection are also discussed on the basis of performance tests with a remodeling test engine.

DRASTIC IMPROVEMENT OF THERMAL EFFICIENCY BY RAPID PISTON-MOVEMENT NEAR TDC

  • Moriyoshi, Y.;Sano, M.;Morikawa, K.;Kaneko, M.
    • International Journal of Automotive Technology
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    • v.7 no.3
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    • pp.295-301
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    • 2006
  • A new combustion method of high compression ratio SI engine was studied and proposed in order to achieve high thermal efficiency, comparable to that of CI engine. Compression ratio of SI engine is generally restricted by the knocking phenomena. A combustion chamber profile and a cranking mechanism were studied to avoid knocking with high compression ratio. Because reducing the end-gas temperature will suppress knocking, a combustion chamber was considered to have a wide surface at the end-gas region. However, wide surface will lead to large heat loss, which may cancel the gain of higher compression ratio operation. Thereby, a special cranking mechanism was adapted which allowed the piston to move rapidly near TDC. Numerical simulations were performed to optimize the cranking mechanism for achieving high thermal efficiency. An elliptic gear system and a leaf-shape gear system were employed in numerical simulations. Livengood-Wu integral, which is widely used to judge knocking occurrence, was calculated to verify the effect for the new concept. As a result, this concept can be operated at compression ratio of fourteen using a regular gasoline. A new single cylinder engine with compression ratio of twelve and TGV(Tumble Generation Valve) to enhance the turbulence and combustion speed was designed and built for proving its performance. The test results verified the predictions. Thermal efficiency was improve over 10% with compression ratio of twelve compared to an original engine with compression ratio of ten when strong turbulence was generated using TGV, leading to a fast combustion speed and reduced heat loss.

A Study on Combustion Characteristics of a Multi Injector Rocket Engine using $H_2O_2$/Kerosene as propellants (과산화수소/케로신 다중 인젝터의 혼합비에 따른 연소 특성 연구)

  • Yu, I-Sang;Jeon, Jun-Su;kim, Jai-Ho;Kim, Wan-Chan;Ko, Yung-Sung;Kim, Sun-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.129-132
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    • 2012
  • In this study, combustion performance tests of a multi coaxial-swirl injector engine using hydrogen peroxide and kerosene as propellants were performed to evaluate combustion characteristic according to mixture ratio between 6.0 and 9.0 by criterion of designed(7.6). Combustion characteristics were evaluated by calculated characteristic exhaust velocity($c^*$) and pressure fluctuation. Test results showed that the combustion efficiency was over 90% and the pressure fluctuation was within 1%.

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Comparison of Combustion Efficiency of Multi Hole Pintle Injector and Continuous Pintle Injector (다중 홀 핀틀 인젝터와 연속형 핀틀 인젝터의 연소성능 비교)

  • Nam, JeongSoo;Lee, KeonWoong;Koo, JaYe
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.3
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    • pp.165-172
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    • 2022
  • Pintle injector is the most suitable injector for thrust control because it can control the area of propellant injection. Accordingly, the combustion test of multiple hole pintle injector and continuous type pintle injector was carried out in this paper using liquid oxygen and gas methane. The combustion performance of the two pintles was verified with the characteristic speed efficiency, and the experimental results were compared according to the O/F and combustion chamber pressure and under similar conditions. The efficiency of the multi hole pintle was generally somewhat higher than continuous pintle when pintle opening distance(the area of dispensing oxidizer) was in a 100% thrust condition.

Configuration Design, Hot-firing Test and Performance Evaluation of 200 N-Class GCH4/LOx Small Rocket Engine (Part II: Steady State-mode Ground Hot-firing Test) (200 N급 GCH4/LOx 소형로켓엔진의 형상설계와 성능시험평가 (Part II: 정상상태 지상연소시험))

  • Kim, Min Cheol;Kim, Young Jin;Kim, Jeong Soo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.24 no.1
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    • pp.9-16
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    • 2020
  • A performance evaluation of the 200 N-class GCH4/LOx small rocket engine was performed through ground hot-firing test. As a result, the combustion pressure and thrust raised with the increase of the oxidizer supply pressure, and thus the specific impulse, characteristic velocity, and their efficiency increased. The characteristic velocity was measured at about 90% performance efficiency. The change of chamber aspect ratio did not affect the performance of the rocket engine in the test condition specified. In addition, uncertainty evaluation was conducted to ensure the reliability of the test results.

Emission Characteristics of NO2 in Diesel Oxidation Catalyst according to the Content of Precious Metal (귀금속 함량에 따른 디젤산화촉매의 이산화질소 배출 특성)

  • Kim, Hoonmyung;Park, Yongsung;Lee, Gwang G.
    • 한국연소학회:학술대회논문집
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    • 2012.11a
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    • pp.37-38
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    • 2012
  • Two catalyst systems with different content of precious metal coated on DOC are carefully tested in a diesel engine to investigate the emission characteristics of $NO_2$. Three types of experiment methods ($NO_2$ conversion test, ETC mode test, and BPT test) are applied to compare the performance of the two catalyst systems. All the experimental results consistently indicate that it is possible to satisfy $NO_x$ regulation by properly lowering the content of precious metal without the loss of PM removal performance.

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Heat transfer characteristics around a circular combustion chamber of kerosene fan heater (석유 팬 히터의 연소실 주변 열전달 특성)

  • Kim, Jang-Gwon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.22 no.4
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    • pp.551-561
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    • 1998
  • This paper was studied to understand the characteristics of heat transfer coefficients and surface temperature distributions around a circular combustion chamber within the heat-intercept duct of kerosene fan heater. The experiment was carried out in the heat-intercept duct of kerosene fan heater attached to the blow-down-type subsonic wind tunnel with a test section of 240 mm * 240 mm * 1200 mm. The purpose of this paper was to obtain the basic data related with normal combustion for new design from conventional kerosene fan heater, and to investigate the effect of surface temperature, local and mean heat transfer coefficients versus flow-rate of convection axial fan according to the variations of heat release conditions from kerosene fan heater during normal combustion. Consequently it was found that (i) the revolution of convection axial fan during combustion had a smaller value than that of non-combustion because of the thermal resistance due to the high temperature in the heat-intercept duct, (ii) the pressure ratio P$_{2}$/P$_{1}$ had a comparatively constant value of 0.844 according to the revolution increase of turbo fan and the heating performance of kerosene fan heater had a range of 1,494 ~ 3,852 kcal/hr, (iii) the local heat transfer coefficient around a circular combustion chamber had a comparatively larger scale in the range of 315 deg. < .theta. < 45 deg. than that in the range of 90 deg. < .theta. < 270 deg. as a result of heat transfer difference between front and back of a circular combustion chamber, and (iv) the mean heat transfer coefficient around a circular combustion chamber increased linearly like a H$_{m}$=95.196Q+104.019 in condition of high heat release according to the increase of flow-rate of axial fan.n.

Incineration of Waste Water Sludge and Coal In a Circulating Fluidized Bed Combustor (순환유동층에서 폐수슬러지와 석탄의 혼소 특성)

  • Bae, Dal-Hee;Shun, Do-Won;Park, Jae-Hyeon;Ryu, Ho-Jung;Park, Do-Hyun
    • 한국연소학회:학술대회논문집
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    • 2004.06a
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    • pp.165-172
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    • 2004
  • Co-incineration of coal and wastewater sludge was r;erfonn:rl in a O.lMWth bench scale circulating fluidized bed combustor(CFBC) Sludge was received from a wastewater treatment plant in a dye industrial complex in Busan. Metropolis. Moisture content of received sludge was 80%. Coal and sludge mixture was prepared with weight ratio of 90/10, 85/15 and 80/20. Co-combustion characteristics of the coal and sludge mixture demonstrated stable combustion conditions. Component analysis, incineration characteristics, boiler performance was measured before and after the test and application for commercial 59MWth CFBC boiler. The release of hazardous components such as $SO_2$ and Cl was suppressed by the presence of inherent minerals of Ca, Na, K in coal and sludge mixture. Pre-drying was not essential but it was recommended for the benefits of manageability of sludge.

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A Review of Development for DHI's Industrial Gas Turbine Combustor (2) (두산중공업 발전용 가스터빈 연소기 개발 현황 (2))

  • Lee, Donghun;Lee, Sangeon;Chon, Muhwan;Nam, Samsik;Lee, Kwangyeol
    • 한국연소학회:학술대회논문집
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    • 2015.12a
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    • pp.269-269
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    • 2015
  • 두산중공업이 국책과제로 개발 중인 한국형 대형 가스터빈의 연소기 개발현황 및 결과에 대해 기술하였다. 압력손실 5%, 연소효율 99.9%, 15ppm NOx 배출 성능을 가지는 14개의 캔형 연소기로 구성되었으며, 40% turn down ratio 운전, WI ${\pm}7%$의 fuel flexibility 성능 및 dual fuel 적용 가능한 운전 성능 목표를 가진다. 이를 위해 Dry Low NOx 형 연소기를 개발, 단일 노즐 연소시험을 수행 중이며, 2016년 상반기 중 상압연소리그시험을 거쳐 그 성능을 검증하고자 한다.

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