• Title/Summary/Keyword: 공기 이젝터 시스템

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Starting Characteristics Study of Scramjet Engine Test Facility(SETF) (스크램제트 엔진 시험설비의 시동특성 연구)

  • Lee, Yang-Ji;Kang, Sang-Hun;Oh, Joong-Hwan;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.451-458
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    • 2010
  • Unlike most aerodynamic wind-tunnel, Scramjet Engine Test Facility(SETF) of Korea Aerospace Research Institute should simulate enthalpy condition at a flight condition. SETF is a blow-down type, high-enthalpy wind tunnel. To attain a flight condition, a highly stagnated air comes into the test cell through a supersonic nozzle. Also, an air ejector of the SETF is used for simulating altitude conditions of the engine, and facility starting. SETF has a free-jet type test cell and this free-jet type test cell can simulate a boundary layer effect between an airplane and engine using facility nozzle, but it is too difficult to predict the nature of the facility. Therefore it is required to understand the starting characteristics of the facility by experiments. In this paper, the starting characteristics of the SETF and modifications of the ejector are described.

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Flow Characteristics of Central-Driven Ejector with Design Parameters (중앙구동 이젝터의 설계변수에 따른 유동특성)

  • Park, Sang Kyoo;Yang, Hei Cheon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.8
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    • pp.645-651
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    • 2015
  • The objective of this study is to experimentally investigate the effect of design parameter on the mass ratio of a central-driven ejector. The design parameters are the primary nozzle area and distance ratios, diffuser exit-area ratio and mixing-tube length ratio. The experimental setup was an open-loop continuous circulation system which has a movable nozzle ejector, an electric motor-pump, a water tank, a control panel and high-speed camera unit. We calculated the mass ratio using the measured primary and suction-flow rates with the experimental parameter of primary water-flow rate or pressure. The results showed that the mass ratio increased with the primary nozzle distance ratio and mixing tube length ratio, while the mass ratio decreased with the primary nozzle-area ratio and diffuser exit-area ratio.

The Stream and Exhaust Gas Characteristics for Variation of Exhaust Gas Temperature of Marine Incinerator Ejector (선박용 소각로 이젝터의 배출온도 변화에 따른 유동과 배기특성)

  • 김태한
    • Journal of Ocean Engineering and Technology
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    • v.14 no.2
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    • pp.60-64
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    • 2000
  • An experimental study was performed to investigate the optimal ejector and operating condition of vessel incinerator. Exhaust gas temperature and secondary air which makes vacuum pressure at ejector throat regions were considered as an important factor. According to the measurement of pressure temperature and nitrogen oxides between non combustion and combustion we found the stream and exhaust gas characteristics of incinerator. This results can give us the exhaust gas temperature control system air pollutant reduction method and the optimum ejector design.

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A Study on the Hypersonic Air-breathing Engine Ground Test Facility Composition and Characteristics (극초음속 공기흡입식 추진기관 지상 시험설비의 구성 및 특성에 관한 연구)

  • Lee, Yang-Ji;Kang, Sang-Hun;Yang, Soo-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.6
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    • pp.81-90
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    • 2015
  • In order to know the characteristics of the hypersonic air-breahting engine, high altitude and Mach number ground test is necessary. Therefore, high pressure and high temperature condition should be simulated to do ground test of the hypersonic air-breathing engine. In this paper, the hypersonic air-breathing engine ground test facility of the Korea Aerospace Research Institute was introduced and the composition and characteristics were described.

A Study on the Closed-Loop Air Drying Technology for Drying Wastewater Sludge (하수슬러지 건조를 위한 폐루프 공기건조 기술에 관한 연구)

  • Lee, Jung-Eun;Cho, Eun-Man;Kang, Dong-Hyo
    • Journal of Korean Society of Environmental Engineers
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    • v.34 no.12
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    • pp.821-827
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    • 2012
  • Air drying is a technology to dry sludge at the ejector and multi cyclone as intaking and blowing air from outside. So, this technology has a weak point that operating fluctuation is large according to an outside conditions as well as energy consumption is also large due to open loop structure. This is to develop the closed-loop air drying system to be built the dehumidifier consisted of condenser, cooler and compressor at rear side of separator of air dryer, as a way to solve some problem. Air is circulation by the method of blowing-drying-dehumidifying-blowing within this system. It is analyzed that an air circulated at closed-loop air drying equipment contains the energy of 50% more compared with open-loop air drying and is operated regularly because of quality maintenance of air to dry sludge. And also it is analyzed that the cost of drying sludge of 1 ton by closed-loop air drying equipment is lower about 35% than conventional equipment. Therefore, this is evaluated by useful drying technology to face an unexpected climatic conditions due to regular operation as well as low energy consumption.

Development of Inorganic Sludge Drying System Technology Applied with Ejector by Air Velocity (이젝터를 적용한 무기성 슬러지 건조시스템 기술개발)

  • Cho, En-man;Jeong, Won-hoon;Kim, Dong-keon;Kim, Bong-hwan
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.21 no.9
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    • pp.35-41
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    • 2022
  • The moisture content of many inorganic sludges is less than 70% during dewatering. Hence, a mono or piston pump cannot feed the sludge dryer. Thus, most inorganic sludge should be moved to a landfill or recycled directly without any reduction method. This development was invented to apply cyclone dryers using air and specially designed for the continuous injection of sludge sources by negative pressure and high air velocity for low moisture inorganic matter. Therefore, wastewater sludge and raw water treatment sludge discharged from various industrial fields might be settled by this development. The cyclone dryer was commercialized useful as moisture reduction equipment. This development was applied using a sludge injection system for sludge feeding and under the cooperation of ejector design computational fluid dynamics. Furthermore, this paper presented good ejector model results, blowing an airflow of 264 m3/min at an actual performance test.

Development of the Scramjet engine Test Facility(SeTF) in Korea Aerospace Research Institute (한국항공우주연구원 스크램제트 엔진 시험설비의 개발)

  • Lee, Yang-Ji;Kang, Sang-Hun;Oh, Joong-Hwan;Yang, Soo-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.3
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    • pp.69-78
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    • 2010
  • Korea Aerospace Research Institute started on design and development of a hypersonic air-breathing engine test facility from 2000 and completed the test facility installation in July 2009. This facility, designated as Scramjet engine test facility(SeTF), is a blow-down type high enthalpy wind tunnel which has a pressurized air supply system, air heater system, free-jet test chamber, fuel supply system, facility control/measurement system and exhaust system. In this paper, details of the specifications, and configuration of the SeTF are described. For verifying characteristics of the SeTF, wind tunnel tests are now on progress and some of the data are also described.

An Experimental Study on the Water Evaporation Conditions of the Enclosed Tank (밀폐용기내의 물의 저압 증발 최적조건에 관한 실험적 연구)

  • Kim, S.H.;Shin, Y.S.;Lee, Y.W.;Chung, H.S.;Jeong, H.M.
    • Journal of Power System Engineering
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    • v.8 no.1
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    • pp.41-47
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    • 2004
  • Cooling towers are widely used not only for cooling products and equipment in manufacturing process but HVAC(Heating, Ventilation and Air Conditioning) system. As a cooling tower is the terminal apparatus which discharges heat from industrial process, the efficiency of heat exchange in the cooling tower greatly affects to the overall performance of a thermal system. In this paper, we constituted a new water cooling system by using a Latent heat of evaporation in an enclosed tank, and this system is consisted of an enclosed vacuum tank and water driven ejector system. Several experimental cases were carried out for improvement methods of high vacuum pressure and water cooling characteristics. The ejector performance was tested in case of water temperature variations that flows into the ejector. Based on the vacuum pressure by water driven ejector, the water cooling characteristics were investigated for the vaporized air condensing effects.

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