• 제목/요약/키워드: Gas feeding system

검색결과 99건 처리시간 0.022초

와이어 공급에 의한 Inconel의 Nd:YAG 레이저 클래딩 (Nd:YAG Laser Cladding of Inconel with Wire Feeding)

  • 김재도;배민종;팽윤
    • Journal of Welding and Joining
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    • 제18권3호
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    • pp.83-88
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    • 2000
  • Laser cladding processing allows rapid transfer of heat to the material being processed with minimum conduction into base metal, resulting in low total heat input. The effects of Nd:YAG laser cladding with wire feeding on the mechanical properties of Inconel alloy were investigated. inconel alloy is used as the material of nuclear steam generator tubing because of its mechanical properties and corrosion resistance properties. The device for Nd:YAG laser cladding with wire feeding was designed. It consists of the wire feeding system, the wire cladding system and the shielding gas system which prevents the clad layer from being oxidized. Experimental as results indicated that the wire feeding direction and position were important for laser cladding with wire feeding. The wire feeding speed should be adapted according to cladding speed for good shaping of clad layer. The effect of heat on the HAZ size can be limited and the growth of grain size of HAZ size was not serious. The hardness of clad layer and heat affected zone increased with increasing of cladding speed.

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분사압력변화에 따른 액체 LPG 분무특성 -디젤분무와의 비교- (Liquid LPG Spray Characteristics With Injection Pressure Variation -Comparison with Diesel Spray-)

  • 임희성;박권하
    • 한국연소학회지
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    • 제4권2호
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    • pp.43-50
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    • 1999
  • Liquefied petroleum gas (LPG) has been used as motor fuel due to its low emissions and low cost. The fuel feeding system has been improved with stringent requirement for exhaust emissions. LPG carburetion system was first introduced, then the system has been changed to a precisely controlled gas injection system, but this gas feeding system has a limitation on improving power output. In order to improve an engine performance, a multi-point port injection system was introduced recently, and a liquid direct injection system into a cylinder was suggested as a next generation system to maximize a fuel economy as well as a power. This study addresses the analysis of the LPG spray from diesel injectors. The spray images are visualized and compared with diesel sprays in a wide injection pressure range. The photographs show much wider dispersion of LPG sprays.

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분사압력변화에 따른 액체 LPG 분무특성;디젤분무와의 비교 (Liquid LPG Spray Characteristics With Injection Pressure Variation;Comparison with Diesel Spray)

  • 임희성;박권하
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
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    • pp.21-26
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    • 1999
  • Liquefied petroleum gas(LPG) has been used as motor fuel due to its low emissions and low cost. The fuel feeding system has been improved with stringent requirement for exhaust emissions. LPG carburation system was firstly introduced, then the system changed into a gas injection system controlled precisely, but those gas feeding system has a limitation on improving power output. In order to improve an engine performance, a multi-point port injection system was introduced recently, and a liquid direct injection system into a cylinder was suggested as a next generation system to maximize a fuel economy as well as a power. This study addresses the analysis of the LPG spray from diesel injectors. The spray images are visualized and compared with diesel sprays in a wide injection pressure range. The photographs show much wider dispersion of LPG sprays.

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헬륨 가압시스템에 대한 온도특성 연구(II) (Study on Temperature Characteristic of Pressurization System Using Helium Gas)

  • 정용갑;조남경;길경섭;김영목
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.168-175
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    • 2005
  • 액체로켓 추진시스템에서 가압시스템은 발사체 추진제 탱크의 얼리지 공간에 제어된 가스를 공급하는 것이다. 가압시스템에서 고온 가스 열교환기를 적용하는 데는 가압제의 비용적을 증가시켜 전체 발사체 시스템의 중량을 감소시키는 장점이 있다. 가압시스템 성능에 있어서 주목할 만한 개선점은 극저온 시스템에서 얻어질 수 있다. 이러한 경우 가스 공급은 극저온 탱크 내부에 저장되어 진다. 극저온 가압제의 온도 특성은 가압시스템에서 구성 단품을 개발하는데 있어서 매우 중요하다. 본 연구에서는 SINDA/FLUINT를 이용한 수치적 모델링과 PTF(Propellant-feeding Test Facility)에서 수행된 실험에 대하여 해석 및 시험이 수행되었다.

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분말송급장치의 개조에 의한 미세$5\mu\textrm{m}$ $Al_2O_3$분말의 송급 특성개선 및 플라즈마 용사조건에 따른 코팅층의 특성분석 (Improvement of Powder Feeding Characteristics of Fine$5\mu\textrm{m}$ $Al_2O_3$ Powder by Modification of the Powder Feeding Systems and Characterization of the Coating Layer depending on Plasma Spraying Conditions)

  • 설동욱;김병희;정민석;임영우;서동수
    • Journal of Welding and Joining
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    • 제15권1호
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    • pp.116-124
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    • 1997
  • A scope of this study is to establish the optimum plasma spray conditions for fine ($5\mu\textrm{m}$) $Al_2O_3$ powder. However, the flowability of the $Al_2O_3$ powder is not so good because of irregular particle shape and fine particle size. Therefore, powder feeding system was modified by 1) change of powder feeding line material from polymer to copper 2) shorten the powder feeding tube length 3) heating the powder feeding system to $80^{\circ}C$4) vibrating the powder feeding line continuously, in order to feed the fine powder homogeneously. The homogeneous powder feeding conditions were obtained with the modified powder feeding system by controlling the powder carrier gas flow and the powder flow rate indicator. The best plasma spraying conditions for the fine $Al_2O_3$ powder were found out as 40kw gun power, 80 g/min. powder feed rate and 50 mm working distance after characterizing the microstructure, hardness and wear loss of the $Al_2O_3$ coating layer.

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KSR-III 추진기관 공급계 동특성 해석 (Dynamic Characteristic Analysis of KSR-III Propulsion Feeding System)

  • 정영석;조인현;정태규;권오성
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.1008-1013
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    • 2001
  • KSR-III propulsion system designed in KARI has a gas-pressurization system for propellant feeding system. This system uses a regulator for the control of the ullage pressure of propellant tank and a venturi for passive control of propellant flowrate. This system seems to be very reliable, but the flowrate of propellant varies according to the change of acceleration with the rocket flight. In this paper, dynamic characteristic of KSR-III propulsion feeding system was analyzed in flight condition. The purpose of this research is to find the variation of off ratio and propellant flowrate change for certification condition of engine reliability test.

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알루미늄입자의 유체화, 이송 및 점화에 대한 연구(I) (Development of aluminum powder feeding system)

  • 이선기;권수현;이병준;송동주;이지형
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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    • pp.241-243
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    • 2012
  • Experiments were conducted to get the design concepts for the continuous aluminum particle feeding system. Two opposed cylinders were used. Aluminum particles in one cylinder were ejected to the air by the supplying gas and the pressure of the other cylinder. It was not possible to eject more aluminum mass flowrate than that of gas if particles were just thrust by the pressure difference between two cylinders. Aluminum particle/air mixture in the flow system was successfully ignited by the electric spark.

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바이오가스를 이용한 가스화기 운전 방안 (The Gasifier Operation Method using Bio Gas)

  • 이중원;주용진;정재화;박세익;김의식
    • 한국수소및신에너지학회논문집
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    • 제24권3호
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    • pp.249-254
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    • 2013
  • The integrated gasification combined cycle (IGCC) system is well known for its high efficiency compared with other coal fueled power generation system. The aim of this study is to confirm the feasibility of using bio gas in coal feeding system and syngas recirculation system. The effects of using bio gas in the gasifier on the syngas composition were investigated through simulations using the Aspen Plus process simulator. It was found that these changes had an influence on the syngas composition of the final stream and bio gas can be used in a gasifier system.

183MW 대용량 동기기 구동 LCI 시스템 기동운전 분석 및 시험 (Start-up Analysis and Commissioning Test of LCI System for 183MW Large Synchronous Machine)

  • 류호선;차한주
    • 전기학회논문지
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    • 제62권5호
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    • pp.626-631
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    • 2013
  • Gas turbine systems are applied extensively in energy supplies to cover peak load requirements. The gas turboset must be accelerated by starting device up to 60%~80% of rated speed to ignite the gas turbine. Recently, the most favorable and economical starting device is the LCI(Load Commutated Inverter). The LCI runs up the gas turboset by feeding the generator as a synchronous motor. In this paper, we discuss in detail the driving principles and features of 183MW gas turbine system. During field application of LCI system, many tests have been conducted and the results were described in this paper. The test results will be considered as the important resources for development in future.

Gas-lift를 이용한 극저온 추진제의 재순환 성능에 대한 실험 (Experimental Study on Cryogenic Propellant Circulation using Gas-lift)

  • 권오성;이중엽;정용갑
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.551-554
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    • 2006
  • Inhibition of propellant temperature rising in liquid propulsion rocket using cryogenic fluid as a propellant is very important. Especially propellant temperature rising during stand-by after filling and pre-pressurization can bring into cavitation in turbo-pump. One of the method preventing propellant temperature rising in cryogenic feeding system is recirculating propellant through the loop composed of propellant tank, feed pipe, and recirculation pipe. The circulation of propellant is promoted through gas-lift effect by gas injection to lower position of recirculation pipe. In this experiment liquid oxygen and gas helium is used as propellant and injection gas. Under atmospheric and pressurized tank ullage condition, helium injection flow-rate is varied to observe the variation of recirculating flow-rate and propellant temperature in the feed pipe. There is appropriate helium injection flow-rate for gas-lift recirculation system.

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