• Title/Summary/Keyword: gas generator

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A Study on control mode of hybrid multi-function welder (하이브리드 다기능 용접기 제어 모드에 관한 연구)

  • Kim, Jin-Seok;Choi, Jae-Ho;Jeong, Yang-Kwon
    • The Journal of the Korea institute of electronic communication sciences
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    • v.8 no.3
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    • pp.439-445
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    • 2013
  • This study is on the system that can integrate generator and charger to use as a welder and generator for need. Specifically, it was hybrid generator consisted with select switch to use generator controller and multiple function welder, that function were auto-stopping generator when generator power finish to recharge in recharger battery and Co2 MMA TIG MIG MAG are devide depend on supplying gas. This control system of voltage, high-frequency, motor and gas valve was implemented in order to improve the performance and convenience of existing welders to choose only one or two at a time.

On-Line Detection of Shorted Turn in Generator Rotor Windings (발전기 회전자 권선의 운전중 층간단락 탐지)

  • Kim, Hui-Dong;Lee, Yeong-Jun;Park, Jong-Jeong;Ju, Yeong-Ho
    • The Transactions of the Korean Institute of Electrical Engineers C
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    • v.48 no.3
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    • pp.192-199
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    • 1999
  • During start up and shut down, the generator is rotating at a low speed and copper dusts cause arcing between the turns in the slot. Shorted turns occurred primarily by the movement of these copper dusts between individual windings in the generator rotor. Detection of shorted turns was performed in five gas turbine generators in two combined cycle power plants. Two types of permanent and temporary flux probes were used in this paper. These flux probes have been used to develop a methodology for detecting shorted turns in an operating generator's rotor. The flux probes sense the rotor winding slot leakage flux and produce a voltage proportional to the rate of change of the flux. This pattern of flux variation is the signature unique to each rotor winding. An appropriate waveform analysis technique canidentify the pole location, the slot number, and the number of shorted turns within each slot. Shorted turns in field winding of gas turbine generator(125.7 MVA) were detected to twelve turns on al total 190 turns.

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Application of a Turbojet Engine for Fire Extinguishing

  • Slitenko, A.F.;Kim, SooYong
    • International Journal of Aeronautical and Space Sciences
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    • v.1 no.1
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    • pp.62-69
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    • 2000
  • Present study deals with performance analysis of an inert gas generator (IGG) which can be used as effective means to suppress fire. The IGG uses a turbo-jet engine to generate inert gas for fire extinguishing. It is generally known that a less degree of oxygen content in the product of combustion will increase the effectiveness of fire extinguishing. An inert gas generator system with water injection has advantages of suffocating and cooling effects that are very important factors for fire extinguishing. Some aspects of influencing parameters, such as, air excess coefficient, compressor pressure ratio, air temperature before combustion chamber, gas temperature after combustion chamber, mass flow rate of water injection etc. on the performance of IGG system are investigated.

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Development of Mixed Hydrogen Gas Generator Power Conversion System (Mixed Hydrogen Gas Generator용 전력변환장치 개발)

  • Jung, Jang-Gun;Mun, Sang-Pil;Cho, Gil-Je;Kim, Chang-Il
    • Proceedings of the KIEE Conference
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    • 2007.11c
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    • pp.88-92
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    • 2007
  • In this paper, the basic experiment, electrolytic cell design and basic manufacturing have been made to interpret the characteristics of Hydrogen-Oxygen-Gas-Generator. As for the detailed matters, the data research on basic technology on Hydrogen-Oxygen-Gas and analysis on characteristics of Hydrogen-Oxygen-Gas from basic experiment. Also the experiment of characteristics and comparative evaluation between constant current source using IGBT converter from existing method and constant current source using new phase shift PWM control method converter. As results when it has injected constant DC current, we has compared Gas quantities by variable ripple frequencies using phase shift PWM control method converter. Therefore, in linear region, it has not different Gas quantities by constant DC current and by phase shift PWM control method converter. Also, it has increased Gas quantities wilder linear region when put ripple frequency at saturation region. Through, Gas quantities and input power, it has acquired higher input power per Gas quantities at put pulse curren. Therefore, when designing converter or inverter for electrolysis, which has ripple current.

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Combustion Characteristics of Fuel-rich Gas Generator with Impinging Injector for a Liquid Rocket Engine (액체로켓엔진에서 충돌형 분사기 형태의 연료과잉 가스발생기 연소특성)

  • Han, Yeoung-Min;Kim, Seung-Han;Lee, Kwang-Jin;Moon, Il-Yoon;Seol, Woo-Seok;Lee, Chang-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.6
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    • pp.64-70
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    • 2005
  • The overall results of hot firing tests of fuel-rich gas generator with impinging injector at design and off-design points are described. The gas generator consists of an injector head with impinging injector, a water cooled combustor wall, a turbulence ring to enhance mixing, an instrument ring measuring temperature and pressure and a nozzle. The combustion tests were successfully performed without damage of gas generator. Test results show that the outlet temperature is not dependent on residence time of hot gas within 4~6msec but dependent on chamber pressure. The relation between outlet temperature and combustion efficiency resulting from measured pressure, mass flow rate and area of nozzle throat is shown. The overall O/F ratio is the critical parameter to determine the outlet temperature and the linear correlation between two parameters is established.

Hot-Fire Test of a Turbopump for a 30 Ton Class Engine in Real Propellant Environment (30톤급 엔진용 터보펌프 실매질 고온시험)

  • Hong, Soon-Sam;Kim, Jin-Sun;Kim, Dae-Jin;Kim, Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.11-17
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    • 2009
  • Hot-fire test of a turbopump for a gas generator cycle rocket engine of 30 ton class was carried out in real propellant environment. Liquid oxygen and kerosene were used for the oxidizer pump and the fuel pump, respectively, while hot gas produced by the gas generator was supplied to the turbine. A part of the propellant discharged from the pumps was provided to the gas generator. The turbopump was run stably at both on-design and off-design conditions, satisfying all the performance requirements. This paper describes one of the test cases, where the turbopump was run for 120 seconds at three different operating modes in one test. In terms of performance characteristics of pumps and turbine, the results from turbopump assembly test using real propellant showed a good agreement with those from the turbopump component tests using simulant working fluid.

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A Study on the safety measures for the protection of hydrogen cooling system of generator (수소를 냉각매체로 하는 발전기 안전대책에 관한 연구)

  • Lee Choon-Ha;Yuk Hyun-Dai
    • Journal of the Korean Institute of Gas
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    • v.8 no.4 s.25
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    • pp.55-61
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    • 2004
  • This paper provided a counter measures against the troubles and accidents that are likely to take place in the power plant using hydrogen gas as a coolant for the cooling system of the generator. Because of the extremely wide flammability limits of hydrogen in comparison to the other flammable gases, the safety measures against the hydrogen accidents is very important to ensure the normal operation of electric-power facility. This study's purpose was a presentation of standard model of safety management of hydrogen equipments in the coal firing power plant such as following items: 1) providing the technical prevention manual of the hydrogen explosions and hydrogen fires occurring in the cooling system of power generator; 2) the selection of explosion-proof equipments in terms of the risk level of operating environment; 3) the establishment of regulations and counter measures, such as the incorporation of gas leakage alarm device, for preventing the accidents from arising, 4) the establishment of safety management system to ensure the normal operation of the power plant.

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Development and Performance Analysis of Gas Generator with Plunger-type Flow Control Valve for Ducted Rocket : Part I (Plunger 타입 유량조절장치를 적용한 덕티드 로켓용 가스발생기 개발 및 성능분석 : Part I)

  • Lee, Jungpyo;Han, Seongjoo;Cho, Sungbong;Kim, Kyungmoo;Lim, Jaeil;Lee, Kiyeon
    • Journal of Aerospace System Engineering
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    • v.15 no.3
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    • pp.79-86
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    • 2021
  • For a preliminary study on a thrust-throttleable Variable Flow Ducted Rocket, a gas generator and flow control valve were developed, and ground combustion tests were performed. The gas generator and flow control valve operated at the required performance level for parameters, such as heat-resistance, combustion-time, pressure, and temperature. The combustion characteristics of a fuel-rich solid propellant mixed with Boron/MgAl/AP, etc., were also analyzed. A Plunger-type flow control valve was designed to control the discharge flow area, and it was confirmed that the flow control valve was able to control the combustion gas flow rate and pressure. However, due to the reduction of the discharge flow area caused by adhesion of combustion products, the combustion pressure continuously increased. The analysis of the pressure increase is covered in Part 2 of this paper.

Investigation of the Coil Deforamtion of the Gas Turbine Generator Rotor Using Finite Element Analysis (유한요소해석을 이용한 가스터빈 발전기 로터의 계자권선 변형 해석)

  • Yun, W.N.;Park, H.K.;Kang, M.S.;Kim, J.S.
    • Journal of Power System Engineering
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    • v.13 no.6
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    • pp.95-101
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    • 2009
  • The generator for gas turbine power generation consists of the rotor which generates magnetic field, the winding coil which is the path for the field current and the wedge and retaining ring which prevents the radial movement of the coil. Relatively severe deformation was observed at the coil end section during the inspection of the generator for peaking-load operation, and the thermal-electricity and the centrifugal force were evaluated by the simple modeling of the windings to find the cause. But the simulation stress was not sufficient to induce the coil plastic deformation. The analysis result seems to be applicable to the base-load generators which runs continuously without shut down up to a year, but there had been more deformation than simulated for the generator which is started up and shut down frequently. The cause of the coil deformation was the restriction of the expansion and shrinkage. The restriction occurs when the winding coil shrinks, and the stress overwhelms the yield stress and cause the plastic deformation. The deformation is accumulated during the start-ups and shut-downs and the thermal growth occurs. The factors which induce the coil restriction during the expansion and shrinkage should be reduced to prevent the unallowable deformation. The resolutions are cutting off the field current earlier during the generator shut-down, modifying the coil end section to remove the stress concentration and making the insulation plate inserted between the coil end section and the retaining ring have the constant thickness.

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A Study on the Exhaust Gas Created by Staged Combustion and Gas Generator Cycle LRE by Using CEA (CEA를 이용한 다단연소사이클 및 가스발생기 사이클 LRE 배출가스 성분 분석)

  • Moon, In-Sang;Moon, Il-Yoon;Lee, Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.863-866
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    • 2011
  • Recently environmental issue is more and more emphasized and 'Green Growth' became on of the key words of this Government. Based on this trend, the exhaust gases out of the gas generator cycle and the staged combustion cycle LRE whose propellants are kerosene and LOx were compared. For this purse, 8 tonf class of each cycle engine was designed and the amount and the components of the gases were investigated by using CEA. As expected, the staged combustion cycle engine generates less pollutants than the other cycle. In addition, the graphite that is generated by the gas generator can be reacted with the oxygen in the atmosphere creating additional pollutants.

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