• Title/Summary/Keyword: Combustion system

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Research Trends of Spray and Combustion Characteristics Using a Gelled Propellant (젤 추진제의 분무 및 연소특성 연구동향)

  • Hwang, Tae-Jin;Lee, In-Chul;Koo, Ja-Ye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.5
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    • pp.96-106
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    • 2011
  • There are many advantages in applying gel propellant to a gel propulsion system. These include higher performances, the energy management of liquid propulsion system, reliable storability and low leakage characteristics. Additionally, gel propulsion system are preferable to the high density impulse of propulsion system. Also, when compared to liquid propellants, the gel propellants acquire greater heat energy. Gel propellants achieve a high specific impulse when metal particles with aluminum and boron are added. With respect to atomization, an inactive process occurs due to the variable viscosity of the metal particles and gelling agents. To improve the defect of atomization and combustion characteristics of gel propellant, a variety of issues related to spray and combustion is introduced here.

Novel Ramjet Propulsion System with H2O2-Kerosene Rocket as an Initial Accelerator (H2O2-케로신 로켓을 초기 가속장치로 갖는 새로운 램젯 추진기관)

  • Park, Geun-Hong;Lim, Ha-Young;Kwon, Se-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.5
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    • pp.491-496
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    • 2008
  • New concept ramjet propulsion system with liquid bipropellant rocket using "Green Propellant" hydrogen peroxide for launch stage is proposed. In this novel concept, hydrogen peroxide gas generator produces hot oxygen at launch stage and kerosene injects to this jet in combustor. For basic study of this new concept ramjet system, investigation of auto-ignition characteristics and combustion of decomposed hydrogen peroxide and kerosene was conducted. In various test cases, auto-ignition and stable combustion was verified. The combustion temperature of 400°C and Fuel/Oxidizer mixture ratio of 0.6 were the limit of auto ignition. Through the experiment results, the possibility of novel concept combined propulsion system using hydrogen peroxide gas generator is ascertained.

Performance Analysis of an Inert Gas Generator for Fire Extinguishing

  • Kim, Su-Yong;Arkadiy F. Slitenko
    • 연구논문집
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    • s.29
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    • pp.5-15
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    • 1999
  • Present study deals with performance analysis of an inert gas generator (IGG) which is to be used as an effective mean to suppress the fire. The IGG uses a turbo jet cycle gas turbine engine to generate inert gas for fire extinguishing. It is generally known that a lesser degree of oxygen content in the product of combustion will increase the effectiveness of fire suppressing. An inert gas generator system with water injection will bring advantages of suffocating and cooling effects which are considered as vital factors for fire extinguishing. As the inert gas is injected to the burning site, it lowers the oxygen content of the air surrounding the flame as well as reduces the temperature around the fire as the vapour in the inert gas evaporates during the time of spreading. Some important aspects of influencing parameters, such as, air excess coefficient. $\alpha$, compressor pressure ratio, $ pi_c$, air temperature before combustion chamber, $T_2$, gas temperature after combustion chamber, $T_3$, mass flow rate of water injection, $M_w$, etc., on the performance of IGG system are investigated. Calculations of total amount of water needed to reduce the turbine exit temperature to pre-set nozzle exit temperature employing a heat exchanger were made to compare the economics of the system. A heat exchanger with two step cooling by water and steam is considered to be better than water cooling only. Computer programs were developed to perform the cycle analysis of the IGG system and heat exchanger considered in the present study.

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A Study on the Characteristics of Exhaust Emissions in Diesel Engines with Scrubber EGR System (스크러버형 EGR시스템 디젤기관의 배기 배출형 특성에 관한 연구)

  • 하정호
    • Journal of Advanced Marine Engineering and Technology
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    • v.22 no.4
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    • pp.481-489
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    • 1998
  • The effects of recirculated exhaust gas on the characteristics of fuel economy combustion and exhaust emissions have been experimentally investigated by a four-cylinder four cycle indirect injection water-cooled and marine diesel engine operating at several loads and speeds. in order to reduce the soot contents in the recirculated exhaust gas to intake system of the engine a novel diesel soot removal system with a cylinder-type scrubber which has 6 water injectors(A water injector has 144 nozzles in 1.0 mm diameter) is specially designed and manufactured for the experiment system The experiments in this study are performed at the fixed fuel injection timing of $15.3^{\circ}$ BTDC regardless of experimental conditions, The brake specific fuel consumption rate is slightly fluctuated with EGR in the range of experimental conditions, The maximum value of premixed combustion for the rate of heat release is decreased with EGR at engine load 25% and the ignition is slightly delayed with EGR at engine load 100% NOx emissions are markedly decreased with EGR especially at high loads while soot emissions are increased as the EGR rate rises.

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Pulverized coal injection system development to raise combustion efficiencies of a blast furnace (고로의 연소효율을 높이기 위한 미분탄 공급 시스템 개발)

  • An, Young-Jin;Kang, Pub-Sung;Kwak, Na-Soo;Choi, Gyung-Min;Lee, Min-Cheol
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.3163-3168
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    • 2008
  • Pulverized coal (PC) has become an important auxiliary fuel in the iron and steel industry since the technique of pulverized coal injection (PCI) system was developed for iron making. Combustion efficiencies of pulverized coal in blowpipes and tuyeres under various operational are numerically predicted to recognize the performance with the locations of nozzles in a blast furnace. A variety of parameters including the pulverized coal quantities, oxygen amounts, inlet temperature of the tuyeres and mass flow rate of coal carrier gas are taken into consideration. Also In order to develop more efficient than existing coal injection system, this study applies a flame measurement system using a charge couple device (CCD) camera and frame grabber. And it has used algorithms of auto sampling from flame shape information and composed the device for location control of PCI. This study find to further improve the blast furnace performance by the control of PCI locations.

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Design and Application of Emergency Blockage System for Engine Part at IPPT and SQT (IPPT, SQT에서의 엔진부 비상정지 시스템 설계 및 운용)

  • 하성업;이중엽;정태규;한상엽
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.2
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    • pp.44-53
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    • 2003
  • A vertical hot-firing test facility was established to carry out the IPPT(Integrated Propulsion Performance Test) and SQT(Stage Qualification Test) of KSR-III(Korea Sounding Rocket-III). The components for actual launcher were mostly used, hence these tests were carried out under the condition of relatively lower safety margin. To perform hot-firing tests with the maximum safety, an engine emergency blockage system was investigated and applied. An emergency blockage system using combustion chamber pressures and acceleration signals was set up to monitor ignition delay and fail, flame out, propellant feeding status, unstable combustion and excessive structural vibration. With such a system, the test safety could be secured by rapid judgement and follow-up measures, which made IPPT and SQT be safely completed.

Combustion Characteristics of the SOFC Products for SOFC/Gas Turbine Hybrid Power Generation System (SOFC/가스터빈 혼합발전을 위한 SOFC 생성물의 연소특성)

  • Lee, Byeong Jun;Bae, Chul Han
    • Journal of the Korean Society of Combustion
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    • v.19 no.3
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    • pp.44-52
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    • 2014
  • Solid oxide fuel cell(SOFC) makes electric power using hydrogen or reformed from methane and emits high temperature products that contain flammable species like hydrogen, carbon monoxide and methane which varies with operation condition. SOFC/gas turbine integrated system which uses thermal and chemical energy of the discharges is more efficient than SOFC itself. Burning character of the SOFC products will affect the efficiency and stability of the system. Experiments were conducted to know the characteristics of the flame for two typical composition of SOFC products, i.e. start-up and steady state composition. When coflowing air temperature was higher than $600^{\circ}C$, auto-ignitin occurred for both fuels. Though start-up fuel has higher contents of hydrogen, it makes longer flame than steady state composition. It was inferred that the amount of oxidizer necessary to burn makes this phenomenon. Steady state composition fuel was unstable since it contains lots of water. Nozzle that had 6 holes, distance between each hole was 16.7 times of hole diameter, improved the stability of the flame.

Development of Eco-Friendly Range Extension UTV Hybrid Vehicle System (주행거리 확장을 위한 하이브리드형친환경UTV 차량 시스템 개발)

  • Kim, Kee Joo;Won, Si Tae
    • Journal of the Korean Society for Precision Engineering
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    • v.33 no.12
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    • pp.1015-1020
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    • 2016
  • An advantage of electric vehicles is that they are environmentally sustainable because they do not emit exhaust gases, such as $CO_2$ or Nox. A disadvantage is the low power performance of the motor and battery source, necessitating a reduction in the weight of the vehicle to increase efficiency. Another disadvantage is that the rechargeable battery enables an electric vehicle to only run for a limited number of miles before requiring electric charging. To solve these problems, the hybrid vehicle has been developed by combining environmental sustainability with the high performance of a conventional internal combustion engine. In this study, an electric UTV (Utility Terrain Vehicle) was transformed into a hybrid vehicle system by outfitting the vehicle with a drive auxiliary power system including a 125 cc internal combustion engine. This modification enabled us to extend the range of the hybrid UTV from 50km to 100km per one electric charging.

Development of the Drive-away Motor for Cold Launch System (저온 사출장치용 이탈모타 개발)

  • Baek, Gook-Hyun;Oh, Jong-Yun;Lee, Young-Won;Lee, Ji-Hyung;Jung, Jin-Suk
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.4
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    • pp.93-98
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    • 2012
  • To solve the combustion instability, especially chuffing phenomena, happened during development process of a drive-away motor that was required for cold launch system of missile, various technical approaches have been performed through ground firing tests. The ignition energy or its supply system, generally closely related with the chuffing phenomena, does not affect suppression of the chuffing, but the increase of characteristic length($L^*$) as well as the addition of 2% ZrC as a damping material is effective to suppress the chuffing. Therefore we could have a typical experience on the combustion instability in double base propellant.

Numerical Analysis of Turbulent Combustion and Emissions in an HRSG System (가스터빈 열 회수 증기 발생기의 난류연소 해석과 배기가스 예측 및 검증)

  • Jang, Jihoon;Han, Karam;Park, Hoyoung;Lee, Wook-Ryun;Huh, Kangyul
    • KEPCO Journal on Electric Power and Energy
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    • v.5 no.2
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    • pp.103-111
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    • 2019
  • The combined cycle plant is an integration of gas turbine and steam turbine, combining the advantages of both cycles. It recovers the heat energy from gas turbine exhaust to use it to generate steam. The heat recovery steam generator plays a crucial role in combined cycle plants, providing the link between the gas turbine and the steam turbine. Simulation of the performance of the HRSG is required to study its effect on the entire cycle and system. Computational fluid dynamics has potential to become a useful to validate the performance of the HRSG. In this study a solver has been implemented in the open source code, OpenFOAM, for combustion simulation in the heat recovery steam generator. The solver is based on the steady laminar flamelet model to simulate detailed chemical reaction mechanism. Thereafter, the solver is used for simulation of HRSG system. Three cases with varying fuel injections and gas turbine exhaust gas flow rates were simulated and the results were compared with measurements at the system outlet. Predicted temperature and emissions and those from measurements showed the same trend and in quantitative agreement.