• 제목/요약/키워드: Hybrid combustion

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다이아프램 두께 변화에 따른 하이브리드 로켓의 후퇴율 향상에 관한 연구 (Effect of Diaphragm Thickness on Regression Rate Improvement in Hybrid Rocket Motor)

  • 류성훈;오지성;문근환;김학철;문희장;김진곤
    • 한국항공운항학회지
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    • 제23권4호
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    • pp.1-5
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    • 2015
  • In this work, a study was conducted to investigate the effect of diaphragm thickness on the regression rate of the hybrid rocket motor. To observe the flow pattern and the recirculation zone, visualizations of combustion chambers with different diaphragm thickness (5mm, 10mm) were performed. It was found that the case with 5 mm thickness had a larger recirculation zone and therefore, had a higher regression rate than the case with 10mm thickness due to the increased residence time and heat transfer toward the fuel surface. Finally, it was concluded that the thickness of diaphragm can be a critical parameter for the enhancement of the regression rate.

Design Rules of Hybrid Stepping Machine for Free Piston Engine

  • Jeong, Sung-In
    • Journal of Electrical Engineering and Technology
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    • 제12권3호
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    • pp.1219-1226
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    • 2017
  • This paper presents the hybrid stepping machine for linear oscillating generators. The focus of the work is the suggestion of the improved model through the comparison of proposed models ; new flux concentrating PMs mover of the hybrid stepping generator is proposed based on the symmetrical and non-symmetrical stator cores of the surface mounted PMs mover, and non-slanted PMs and slanted PMs of the flux concentrating PMs mover. It is achieved using equivalent magnetic circuit considering leakage elements. Finally, this study suggests new hybrid stepping structure of linear oscillating generator.

Environmentally Friendly Hybrid Power System for Cultivators

  • Kim, Sang Cheol;Hong, Young Ki;Kim, Gook Hwan
    • Journal of Biosystems Engineering
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    • 제39권4호
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    • pp.274-282
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    • 2014
  • Purpose: In this study, a hybrid power system was developed for agricultural machines with a 20-KW output capacity, and it was attached to a multi-purpose cultivator to improve the performance of the cultivator, which was evaluated using output tests. Methods: The hybrid system combined heterogeneous sources: an internal-combustion engine and an electric power motor. In addition, a power splitter was developed to simplify the power transmission structure. The cultivator using the hybrid system was designed to have increased fuel efficiency and output power and reduced exhaust gas emissions, while maintaining the functions of existing cultivators. Results: The fuel consumption for driving the cultivator in the hybrid engine vehicle (HEV) mode was 341 g/KWh, which was 36% less than the consumption in the engine (ENG) mode for the same load. The maximum power take off output of the hybrid power system was 12.7 KW, which was 38% more than the output of the internal-combustion engine. In the HEV mode, harmful exhaust gas emissions were reduced; i.e., CO emissions were reduced by 36~41% and NOx emissions were reduced by 27~51% compared to the corresponding emissions in the ENG mode. Conclusions: The hybrid power system improved the fuel efficiency and reduced exhaust gas emissions in agricultural machinery. Lower exhaust gas emissions of the hybrid system have considerable advantages in closed work environments such as crop production facilities; therefore, agricultural machinery with less exhaust gas emissions should be commercialized. However, the high manufacturing cost and complexity of the proposed system are challenges which need to be solved in the future.

친환경 하이브리드 동력 시스템 개발 및 농기계 응용 (Development of an Environmental Friendly Hybrid Power System and its Application to Agricultural Machines)

  • 김상철;홍영기;김국환
    • 제어로봇시스템학회논문지
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    • 제21권5호
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    • pp.447-452
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    • 2015
  • A hybrid power system was developed for agricultural machines with a 20kW output capacity, and it was attached to a multi-purpose cultivator to improve the performance of the cultivator. The hybrid system combined heterogeneous sources: an internal-combustion engine and an electric power motor. In addition, a power splitter was developed to simplify the power transmission structure. The cultivator using a hybrid system was designed to have increased fuel efficiency and output power and reduced exhaust gas emissions, while maintaining the functions of existing cultivators. The fuel consumption for driving the cultivator in the hybrid engine vehicle (HEV) mode was 341g/kWh, which was 36% less than the consumption in the engine (ENG) mode for the same load. The maximum power take off output of the hybrid power system was 12.7kW, which was 38% more than the output of the internal-combustion engine. In the HEV mode, harmful exhaust gas emissions were reduced; i.e., CO emissions were reduced by 36~41% and NOx emissions were reduced by 27~51% compared to the corresponding emissions in the ENG mode. The hybrid power system improved the fuel efficiency and reduced exhaust gas emissions in agricultural machinery. The hybrid system's lower exhaust gas emissions have considerable advantages in closed work environments such as crop production facilities. Therefore, agricultural machinery with less exhaust gas emissions should be commercialized.

하이브리드 내연발전에서 도서 운영 결손액을 고려한 분산전원 최적 용량 산정 알고리즘 (Algorithm Calculating Optimal DG Capacity Considering Operating Deficit in Hybrid Internal Combustion Generation)

  • 손준호;김미영
    • 한국산학기술학회논문지
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    • 제19권10호
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    • pp.655-660
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    • 2018
  • 지리적 특성상, 도서지역에 전력을 공급하기 위해서 ICG(Internal combustion generation)가 사용되고 있으며, 이로 인하여 상당한 운영비, 염해문제 및 환경오염이 발생하고 있다. 이러한 도서지역에 대해서, KEPCO는 매년 상당한 운영결손액을 감당하고 있는데, 특히 연료비 및 지급수수료가 운영결손액의 상당 부분을 차지하고 있다. 특히, 지급수수료를 줄이기 위하여 근거리 도서 사이의 해저케이블을 통한 ICG 통합운영(integrated ICG, IICG)이 고려되고 있다. 한편, 저탄소 사회에 대한 수요 때문에 도서지역에 분산형전원(Distributed Generation, DG)이 도입되고 있다. 이러한 상황에서, 환경적 특성으로 인해 DG 출력이 불충분한 경우 보조 동력원으로 IICG가 사용되는, 즉, IICG에 DG를 도입한 하이브리드 내연발전(hybrid internal combustion generation, HICG)이 도입되고 있다. 따라서, 본 논문에서는 HICG에서 한전 운영결손액에 상응하게 도입될 수 있는 최적 DG 용량을 산정하는 알고리즘을 제안하였다. 시뮬레이션 결과, 연료비와 최대부하 크기는 최적 DG 용량에 큰 영향을 미치며, 최대부하가 서로 다른 여러 도서에 제안된 알고리즘을 적용하여 그 유효성을 확인하였다.

Hybridal Method for the Prediction of Wave Instabilities Inherent in High Energy-Density Combustors (2): Cumulative Effects of Pressure Coupled Responses on Cavity Acoustics

  • Lee, Gil-Yong;Yoon, Woong-Sup
    • International Journal of Aeronautical and Space Sciences
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    • 제7권2호
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    • pp.33-41
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    • 2006
  • Theoretical-numerical approach of combustion instability in a specific rocket engine is conducted with parametric response functions. Fluctuating instantaneous burning rate is assumed to be functionally coupled with acoustic pressures and have a finite or time-varying amplitudes and phase lags. Only when the amplitudes and phases of combustion response function are sufficiently large and small respectively, the triggered unstable waves are amplified.

둔체를 갖는 연소기에서 자려 연소 진동에 관한 수치해석 (Numerical Simulation of Self-excited Combustion Oscillation in a Dump Combustor with Bluff-body)

  • 김현준;홍정구;김대희;신현동
    • 대한기계학회논문집B
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    • 제32권9호
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    • pp.659-668
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    • 2008
  • Combustion instability has been considered as very important issue for developing gas turbine and rocket engine. There is a need for fundamental understanding of combustion instability. In this study, combustion instability was numerically and experimentally investigated in a dump combustor with bluff body. The fuel and air mixture had overall equivalence ratio of 0.9 and was injected toward dump combustor. The pressure oscillation with approximately 256Hz was experimentally obtained. For numerical simulation, the standard k-$\varepsilon$ model was used for turbulence and the hybrid combustion model (eddy dissipation model and kinetically controlled model) was applied. After calculating steady solution, unsteady calculation was performed with forcing small perturbation on initial that solution. Pressure amplitude and frequency measured by pressure sensor is nearly the same as those predicted by numerical simulation. Furthermore, it is clear that a combustion instability involving vortex shedding is affected by acoustic-vortex-combustion interaction. The phase difference between the pressure and velocity is $\pi$/2, and that between the pressure and heat release rate is in excitation range described by Rayleigh, which is obvious that combustion instability for the bluff body combustor meets thermoacoustic instability criterion.

DME 및 n-Heptane 연료의 디젤엔진 조건에서 분무연소특성 해석 (Numerical Study on the Characteristics of Spray Combustion Processes in the DME and n-heptane Fueled Diesel-like Engine Conditions)

  • 유용욱;석준호;이상길;김용모
    • 한국분무공학회지
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    • 제13권2호
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    • pp.91-98
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    • 2008
  • In the present study, in order to understand the overall spray combustion characteristics of DME fuel as well as to identify the distinctive differences of DME combustion processes against the conventional hydrocarbon liquid fuels, the sequence of the comparative analysis have been systematically made for DME and n-heptane liquid fuels. To realistically represent the physical processes involved in the spray combustion, this studyemploys the hybrid breakup model, the stochastic droplet tracking model, collision model, high-pressure evaporation model, and transient flamelet model with detailed chemistry. Based on numerical results, the detailed discussions are made in terms of the autoignition, spray combustion processes, flame structure, and turbulence-chemistry interaction in the n-heptane and DME fueled spray combustion processes.

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하이브리드 로켓 추진 시스템의 혼합 연소실 적용에 따른 Trade-off 평가 (Trade-off Evaluation due to Application of Mixing Chamber for Hybrid Rocket-Propulsion System)

  • 김학철;문근환;문희장;김진곤
    • 항공우주시스템공학회지
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    • 제10권3호
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    • pp.23-31
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    • 2016
  • The intermediate mixing chamber is one of various methods for improving the regression rate and combustion efficiency of the hybrid rocket. The mixing chamber with its non-combustible material makes the propulsion performance increase, but it leads to a low fuel-loading density in the combustion chamber; therefore, this performance-related trade-off between the mixing chamber and the low fuel-loading density was studied. In this study, the trade-off was conducted by comparing the intermediate-mixing-chamber case with a w/o-mixing-chamber case. The small hybrid-sounding rocket is designed with internal ballistics for comparing the rocket length to the weight. In addition, an external ballistic analysis was conducted for comparing the performances of the w/- and w/o-mixing-chamber cases. As a result, the intermediate-mixing-chamber case shows that the length and the weight were decreased to 12 % and 8 %, respectively; furthermore, when compared with the normal cases, the estimated altitude result of the w/-mixing-chamber case was increased to approximately 75 m.

Carbonation of Circulating Fluidized Bed Combustion Fly Ash with Hybrid Reaction

  • Lee, Ki Gang;Bae, Soon Jong
    • 한국세라믹학회지
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    • 제55권2호
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    • pp.160-165
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    • 2018
  • This paper investigates the reaction rate of $CO_2$ storing carbonation hybrid reaction by comparing the behavior of carbonation between $Ca(OH)_2$ and fly ash with that of CFBC (Circulating Fluidized Bed Combustion) containing plenty of Free-CaO. Because fly ash with CFBC contains a lot of unreacted CaO, it cannot be used as a raw material for concrete admixtures and its usages are limited. To reuse such material, we stabilized unreacted CaO by carbonation and investigated the carbonation rate. We used a pH meter and a thermometer to check the rate of the carbonization. Also, we set the contents of fly ash with CFBC, $Ca(OH)_2$, flow and fluid of $CO_2$, respectively, to 100 g, 50 g, 100 ~ 1000 cc/min and 400 g based on the content of Free-CaO. We used carbonated water instead of water, and added an alkaline activator to promote the carbonation rate. As a result, the addition of the alkaline activator and carbonated water promoted the rate of carbonation via a hybrid reaction.