• Title/Summary/Keyword: 연료 2단 연소

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A Basic Study of Fuel 2-staging Y-jet Atomizer to Reduce NOx in Liquid Fuel Burner (액체 연료용 버너에서 NOx 저감을 위한 연료2단 분사 Y-jet 노즐에 관한 기초연구)

  • Song, Si-Hong;Lee, Gi-Pung;Kim, Hyeok-Je;Park, Seok-Ho
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.11
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    • pp.1616-1623
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    • 2001
  • A basic experimental study has been carried out to find out the design parameters of fuel 2-staging atomizers in order to reduce nitrogen oxides(NOx) rate emitted from the steam boilers used the liquid fuel. The heavy fuel oil(B-Coil) and fuel 2-staging Y-jet twin-fluid atomizers were adopted in this study. The results of this paper were obtained from the real as well as the model scale atomizers. In the case of model atomizers test, NOx reduction rate was strongly dependent on the staged fuel rate, but it was weakly dependent on the injection hole arrangement and air swirl conditions. The real scale atomizers was designed and manufactured on the base of these test results, and those was mounted and operated in the real boiler generates 185 ton steam per an hour. The reduction rate of the model and real plant was reached 10∼30% of base NOx by atomizers. but dust was sharply increased in the low O$_2$combustion region of the real plant.

A Study on the Performance Characteristics of PE-$N_2O$ Hybrid Rocket Motor with the Variation of Fuel Grain Configuration (PE-$N_2O$ 하이브리드 로켓 모터의 연료 그레인 형상 변화에 따른 성능 특성에 관한 연구)

  • Jo, Seung-Hyun;Kim, Sang-Kyum;Kim, Seong-Jin;Kim, Jong-Chan;Yoon, Chang-Jin;Sung, Hong-Gye;Kim, Jin-Kon;Moon, Hee-Jang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.398-401
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    • 2007
  • The performance characteristics of Polyethylene-Nitrous oxide (PE-N2O) hybrid rocket motor with the variation of the grain geometry was investigated. To compare the performance parameters under the different port number, single and four port grains were used in this study. In order to improve the performance by enhancing mixing between fuel and oxidizer, the fuel grain having the mixing chamber was additionally studied. From the motor firing tests, it is found that the motor having 4-port fuel grain with the mixing chamber showed the highest performance among all cases. Therefore we have confirmed that with only the geometrical change of the fuel grain, it was possible to give quite influential improvement on the motor performance

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Diesel Combustion Strategies Effect on Exhaust Emissions and Hydrocarbon Species (디젤 연소 전략에 따른 배기가스 및 탄화수소 종 분석)

  • Han, Man-Bae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.7
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    • pp.759-765
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    • 2012
  • This study investigates the effect of diesel combustion strategies on exhaust emissions and hydrocarbon species emissions for a 1.7 L common rail direct injection diesel engine at 1500 rpm and 3.9 bar BMEP. The first strategy is a method to adopt no EGR with a split injection composed of pilot and main injection (split injection). The second is to adopt a moderate EGR rate with main injection only (single-1). The third is to use a high level of EGR and main injection with rail pressure increase, $i.e.$ low-temperature diesel combustion (single-2). Split injection and single-1 showed a renowned phenomenon of a PM-NOx trade-off, whereas single-2 was observed of a PM-NOx trade-off to reduce PM and NOx simultaneously. HC speciation results show that the split injection produced the least amount of HC species, regardless of the carbon number bin, followed by single-1 and single-2. The ratios of methane, acetylene, and CO to THC increased as a combustion A/F ratio is richer due to reduced oxygen content in the vicinity of the combustion zone, thus enhancing pyrolysis.

Ignition Experiments of a High Pressure Liquid Propellant Thrust Chamber (실물형 연소기의 점화시험)

  • Moon Ilyoon;Kim SeungHan;Kim Jonggyu;Lim Byoungjik;Lee Kwangjin;Kim Intae
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.265-268
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    • 2005
  • A series of ignition tests had been conducted for a thrust chamber propelled by Jet A-1 and liquid oxygen with a chamber pressure of 52.5 bara and a thrust of 30 tonf. The chamber ignited by a hypergolic fluid, TEAL, keeps its first constant pressure low at $63\%$ of the design value by $61\%$ of a liquid oxygen mass flow rate and $67\%$ of fuel for 0.25 sec. The operating O/F ratio of the chamber was kept at lower values than that of the design operating condition throughout the whole ignition procedure. Surge of the chamber pressure is below $6\%$ of the design value.

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Characteristics of the Co-Combustion of Coal and Bio-Solid Fuel using Biomass as an adjunct (석탄과 보조제로 바이오매스를 사용한 바이오 고형연료의 혼소 특성)

  • Hyeon, Wan-Su;Jin, Yong-Gyun;Jo, Eun-Ji;Han, Hyun-Goo;Min, Seon-Ung;Yeo, Woon-Ho
    • Journal of the Korea Organic Resources Recycling Association
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    • v.28 no.2
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    • pp.49-57
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    • 2020
  • Due to the sewage sludge's characteristics of high water content and low calorific value, it is hard to use sewage sludge as an energy source. In this study, we investigated production of bio-solid fuel which is mixed both sewage sludge and woody biomass in order to improve the sewage sludge's characteristics and replace fossil fuels. A thermogravimetric analysis was used to investigate the co-combustion characteristics of the mixed coal and bio-solid fuel of 5%, 10%, 15%, respectively. The analysis was carried out under non-isothermal conditions by raising the internal temperature of 25℃ to 900℃ with an increment of 10℃/min. In the case of comparing single coal sample and mixture sample of coal and bio-solid fuel, the initiation combustion temperature has slightly changed. However, both the maximum combustion temperature and the termination start combustion temperature were hardly noticeable. The initiation combustion was occurred between 200~315℃ and the thermal decomposition causing a significant weight change occurred between 350~700℃. As a result of the kinetic analysis of the co-combustion, the activation energy was decreased as the mixing rate was higher. Therefore, it is able to co-combust the mixed coal and bio-solid fuel in power plants.

A Study on Combustion Characteristics of Hybrid Rocket with the Variation of L/D Ratio (하이브리드 로켓의 L/D 비 변화에 따른 연소특성 연구)

  • Kim Soo-Jong;Kim Jin-Kon;Lee Seung-Chul;You Woo-Jun;Lee Jung-Pyo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.4
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    • pp.31-38
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    • 2005
  • In this paper, the combustion characteristics of a hybrid propulsion system were studied with various L/D(length vs diameter) ratio of the single po.1 type solid fuel. Experiments were performed for 2 cases with the fixed grain port diameter and fuel length respectively. For the first case, results show that there are no large variations for regression rates as the L/D ratio changes. And as the L/D ratio increases, the O/F ratio decreases and thrust, characteristic velocity tends to increase. For the second case, there is no large change for O/F ratio, thrust and characteristic velocity as L/D ratio changes. On the other hand, as the L/D ratio decreases, only the regression rate tends to increase. Experimentally, exponent n in $\dot{r}=a{G_0}^n$ was found about 0.5 and then the O/F ratio was shown nearly constant. In the experiment, PE and gas oxygen were used as a fuel and an oxidizer.

Unsteady Analysis for Combustion Characteristics of PRF75 Fuel under HCCI Conditions (균일예혼합 압축착화 조건에서 PRF75 연료의 비정상 연소특성 해석)

  • Oh, Tae Kyun;Lee, Su Ryong
    • Journal of the Korean Society of Combustion
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    • v.18 no.4
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    • pp.21-28
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    • 2013
  • HCCI engines have mainly focused on achieving low temperature combustion in order to obtain higher efficiency and lower emission. One of practical difficulties in HCCI combustion is to control the start of combustion and subsequent combustion phasing. The choice of primary reference fuels in HCCI strategy is one of various promising solutions to make HCCI combustion ignition-controlled. The behavior of ignition delay to the frequency variation of sinusoidal velocity oscillation is computationally investigated under HCCI conditions of PRF75 using a reduced chemistry in a counterflow configuration. The second-stage ignition is more delayed as the higher frequency is imposed on nozzle velocity fluctuation whereas the first-stage ignition is not much influenced.

Performance Analysis of PE-GOX Hybrid Rocket Motor Part I : Regression Rate Characteristics (PE-GOX 하이브리드 로켓 모터의 성능 예측 Part I : 후퇴율 특성)

  • Youn, Chang-Jin;Song, Na-Young;Yoo, Woo-Jun;Jeon, Chang-Soo;Kim, Jin-Kon;Sung, Hong-Gae;Moon, Hee-Jang
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.2
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    • pp.71-78
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    • 2007
  • An experimental investigation was conducted to clarify the combustion characteristics of Polyethylene-GOX(PE-GOX) hybrid motor using a single-port fuel grain configuration. Data from the experiments were analyzed to evaluate the length-averaged regression rate of PE-GOX propellants. Based on the existing theories, the empirical regression rate formulas provided from Marxman[3,4] and Altman[14] showed good concordance with the PE-GOX experiments. The accuracy of the regression rate was then evaluated and compared with the measured one. As a result, Marxman's model was somewhat more precise than Altman's model in these experiments. Moreover, the consideration of the empirical regression rate showed that O/F ratio has minor variation due to the quasi constant inflow of the fuel during motor firing.

The Numerical Analysis Study about the Air-Fuel Mixing Characteristics by the Change on the 3D Cavity Size (3차원 Cavity 크기 변화에 의한 공기-연료 혼합특성의 수치적 해석 연구)

  • Seo, Hyung-Seok;Jeon, Young-Jin;Byun, Yung-Hwan;Lee, Jae-Woo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.93-98
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    • 2007
  • The air velocity flowing in inner combustion chamber of SCramjet is supersonic and the time of its stay is very short as a few milliseconds. Within this short time, fuel injection, air-fuel mixing, and combustion process should be accomplished. Several methods are suggested for mixing enhancement. Among these, cavity is selected to study for mixing characteristics. The numerical simulation is performed in the case of freestream Mach number of 2.5 and cavity located in front of fuel jet injection. 3 different sized cavities of the same length-height ratio were used in order to recognize the effect about cavity size. Also, the case without cavity was analyzed to find the effect of cavity. Used code compared with the result of experiment under identical conditions and it was verified. Through this comparison and verification, mixing enhancement by cavity size could be confirmed.

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An Experimental Study on the Two Stage Ignition of Cool Flame and Hot Flame in HCCI Engine According to Fuel Composition (연료조성에 따른 HCCI 엔진의 냉염 및 열염의 2단연소 특성에 관한 실험적 연구)

  • 이기형;김형민;류재덕;이창식
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.1
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    • pp.17-24
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    • 2004
  • As the environmental pollution becomes serious global problem, the regulation of emission exhausted from automobiles is strengthened. Therefore, it is very important to know how to reduce the NOx and PM simultaneously in diesel engines, which has lot of merits such as high thermal efficiency, low fuel consumption and durability. By this reason, the new concept called as Homogeneous Charge Compression Ignition(HCCI) engines are spotlighted because this concept reduced NOx and P.M. simultaneously. However, it is well known that HCCI engines increased HC and CO. Thus, the investigation of combustion characteristics which consists cool and hot flames for HCCI engines were needed to obtain the optimal combustion condition. In this study, combustion characteristics for direct injection type HCCI engine such as quantity of cool flame and hot flame, ignition timing and ignition delay were investigated to clarify the effects of these parameters on performance. The results revealed that diesel combustion showed the two-stage ignition of cool flame and hot flame, the rate of cool flame increase and hot flame decrease with increasing intake air temperature. On the other hand, the gasoline combustion is the single-stage ignition and ignition timing is near the TDC. In addition mixed fuel combustion showed different phenomenon, which depends on the ratio of gasoline component. Ignition timing of mixed fuel is retarded near the TDC and the ignition delay is increased according to ratio of gasoline.