• Title/Summary/Keyword: 시험챔버

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The Removal of Indoor Suspended Microorganisms of Eco-friendly Antimicrobial Copper Net Filter (친환경소재인 항균동망 필터의 실내 부유 미생물 제거 연구)

  • Kim, Dong-Woo;Je, Dong-Hyun;Ji, Keunho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.4
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    • pp.311-316
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    • 2018
  • As the lives of people have improved, the demand for improved indoor air quality has increased. Various methods are used to remove biological air pollutants, such as UV/photocatalytic devices and ozone generators. However, these methods have disadvantages such as energy consumption, high corrosivity and toxicity. To overcome these disadvantages, an antibacterial copper filter was fabricated and its antimicrobial activity was then tested against two fungi (P. pinophilum, C. globosum) and one bacteria (S. aureus) Moreover, the ability to remove suspended microorganisms was tested step by step from the chamber stage to the air conditioning system. The results revealed 100% antimicrobial activity after 24 hours for the two fungi, while this value was 99.9% after 18 hours for the bacteria. Moreover, the antibacterial activity was higher when the chamber and air purifier were used than was obtained using a general antibacterial HEPA filter. Also, as a filter for system air conditioner, the antibacterial activity was lowered in offices and hospitals. In conclusion, the copper filter was found to have sufficient antibacterial activity for use as an antibacterial filter; however, further research on its preparation methods and materials is warranted.

Humidity Dependence of Tribological Behavior of DLC Films (DLC 필름의 마찰마모 특성의 습도 의존성에 대한 연구)

  • Park, Se-Jun;Lee, Kwang-Ryeol;Lee, Seung-Cheol;Ko, Dae-Hong
    • Journal of the Korean Vacuum Society
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    • v.15 no.3
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    • pp.287-293
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    • 2006
  • Diamond-like carbon (DLC) film was deposited using benzene $(C_6H_6)$ by r. f-plasma assisted chemical vapor deposition. The tribological properties of the DLC film were tested by rotating ball-on-disc type tribometer isolated by a chamber. The tribological test was performed in air environment of relative humidity ranging from 0 to 90% in order to observe the tribological behavior of the DLC film with the change of humidity. We used steel ball and DLC coated steel ball to investigate the effect of the counterface material. Using steel ball, the friction coefficient of DLC film increased from 0.025 to 0.2 as the humidity increased from 0% to 90%. In case of DLC coated steel ball which didn't form the Fe-rich debris, the friction coefficient showed much lower dependence of humidity as 0.08 in relative humidity 90%. We confirmed that the high humidity dependence of the friction coefficient using steel ball resulted from the increase of debris size with humidity and the formation of Fe-rich debris by the wear of steel ball. And the friction coefficient was immediately dropped when the relative humidity changed from 90% to 0% during test using steel ball. From this result, we confirmed that the effect of the Fe-rich debris on the friction coefficient was that Fe element in debris formed the highly sensitive graphitic transfer layer to humidity.

THERMAL BALANCE MODELLING AND PREDICTION FOR A GEOSTATIONARY SATELLITE (정지궤도 위성의 열평형 시험 모델링 및 예비 예측)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon
    • 한국전산유체공학회:학술대회논문집
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    • 2009.04a
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    • pp.142-147
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    • 2009
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be tested under vacuum condition and very low temperature in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels such as north and south panels. They will be controlled from 90K to 273K by circulating GN2 and LN2 alternatively according to the test phases, while the shroud of the vacuum chamber will be under constant temperature, 90K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test.

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Contamination measurement, Analysis & Control for Satellite (인공위성의 오염 측정, 분석 및 관리)

  • Lee, Sang-Hoon;Hong, Seok-Jong;Cho, Hyok-Jin;Seo, Hee-Jun;Moon, Guee-Won
    • Aerospace Engineering and Technology
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    • v.9 no.2
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    • pp.116-122
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    • 2010
  • It is necessary to be careful about contamination control to minimize the accumulation of the contamination material on satellite surface during the I&T phase. In the space environment which characterized by high vacuum, high and very low temperature, contamination material causes satellite to lose its own performance. Especially, contamination material can accumulate on critical surfaces such as lenses, mirrors, and sensors. KARI(Korea Aerospace Research Institute) conducts the clean room to control and minimize the contamination effect. This paper introduces the principle of contamination and the method of measure and analysis for the contamination.

Development of Bulging Process for Regenerative Cooling Nozzle of Liquid Rocket Thrust Chamber (액체로켓 연소기 재생냉각형 노즐의 벌징 공정 개발)

  • Ryu, Chul-Sung;Choi, Hwan-Suk
    • Aerospace Engineering and Technology
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    • v.7 no.2
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    • pp.103-109
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    • 2008
  • A study has been conducted on the bulging process of regenerative cooling nozzle which is essential for the manufacturing of liquid rocket thrust chamber. Tension tests have been performed for the material to be used for the development of the bulging process and mechanical properties are obtained by the test. Two or three bulging tools were required to complete the bulging process. The necking of the material was a major failure encountered in the bulging process and a research has revealed that grain size of the material has considerable effect on its occurrence. The presently developed bulging process with a controlled grain size material has been successfully applied to the manufacturing of subscale and 30-tonf full scale regeneratively cooled nozzle while demonstrating the applicability and usefulness of the presently developed bulging process.

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Bulging Process of Liquid Rocket Combustion Chamber Nozzle (액체로켓 연소기 노즐의 벌징 공정)

  • Ryu, Chul-Sung;Choi, Hwan-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.3
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    • pp.271-278
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    • 2008
  • A study has been conducted on the bulging process of liquid rocket engine nozzle which is essential to the manufacturing regenerative cooling combustion chamber. Mechanical properties of the material used for the bulging were experimentally obtained by tension tests. Deformation of the bulged nozzle was confirmed by a structural analysis. The developed bulging process and the deformation analysis result were confirmed by manufacturing of the bulged nozzle specimens and the bulging test. There has been a bulging failure among 7 bulged specimens due to the necking of the material. The cause of necking was investigated by comparing microstructure of the material. The investigation has revealed grain size of the material has considerable effect on the occurrence of the necking.

An Experimental Study of a Diffuser Test Rig for Simulating High-Altitude Environment by using Hot (고온 연소가스를 이용한 고공 환경 모사용 디퓨저 실험장치 연구)

  • Yang, Jae-Jun;Lee, Yang-Suk;Kim, Yoo;Ko, Young-Sung;Kim, Yong-Wook;Kim, Chun-Taek
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.31-34
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    • 2007
  • Performance tests of supersonic exhaust diffuser were conducted by using hot combustion gas for simulating high-altitude environment. The test rig consists of a combustion chamber, a vacuum chamber, water cooling ring and diffuser. Before combustion experiments, the preliminary leak tests were carried out on the liquid rocket engine and diffuser by using high pressure nitrogen(30barg) and a vacuum pump. The leak test results showed that there was no leaks at high pressure and vacuum pressure conditions.

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A Study on Predication model for TVOC Emissions of Finishing material in Apartment House (공동주택 건축내장재의 TVOC 방출량에 관한 예측모델 연구)

  • Kim, Hyung-Soo;Lee, Kyung-Hoi
    • KIEAE Journal
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    • v.2 no.3
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    • pp.55-62
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    • 2002
  • While cognition about an environment pollution becomes important recently, the intense pollution measures about an indoor air environment is required. In the case of building indoor environment, over 80% of modem people is living in building and these days an interest of building interior materials which becomes a reason for indoor environmental pollution in public house, office, is increasing. An experimental measurement method of this study is as follows. (1) American EPA TO-17, ASTMD5116-97, measurement method in VOCs experiment of Japanese closet industrial association (2) 2.4-DNPH cartridge method in HCHO experiment, based on American EPA TO-11 and measurement method of Japanese closet industrial association (3) standard compound is analyzed by using HPLC after solvent extraction process (4) paint and furniture are selected as measurement objects (5) we also made small chamber to grasp an emission characteristic of HCHO and VOCs and to get an environment-amicable forecast model through it, then we developed the model which can forecast emission rate by chamber experiment.

Study on Spray Characteristics of GCSC Injector with Recess in High Pressure Condition (고압조건에서 기체-액체 분사기의 리세스에 따른 분무 특성 연구)

  • Kim, Jong-Gyu;Han, Yeoung-Min;Choi, Hwan-Seok;Yoon, Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.57-60
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    • 2011
  • The spray characteristics according to the recess length of the GCSC injector and the change of momentum flux ratio(MFR) of the gas and the liquid have been examined through high pressure cold flow test using a high pressure chamber. The liquid in this experiment was water, and the gas was nitrogen. The spray images were taken by a back-lit strobe imaging technique. Results showed that the spray was a wide hollow cone at the lower MFR(liquid velocity was fixed) and the spray became a narrow solid cone as the MFR was increased. And the injector with short recess length produced a narrow solid cone at the higher MFR.

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The Design, Structural Analysis and High Pressure Chamber Test of a Thick Pressure Cylinder for 2000 m Water Depth (수심 2000m 용 두꺼운 내압용기의 설계, 구조해석과 내압시험)

  • Choi, Hyeuk-Jin;Lee, Jae-Hwan;Kim, Jin-Min;Lee, Seung-Guk;Maring, Kothilngam
    • Journal of the Society of Naval Architects of Korea
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    • v.53 no.2
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    • pp.144-153
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    • 2016
  • This paper aims to demonstrate the design, structure analysis, and hydrostatic pressure test of the cylinder used in 2000m water depth. The cylinder was designed in accordance with ASME pressure vessel design rule. The 1.5 times safety factor required by the general rule was applied to the design of the cylinder, because ASME rule is so excessive that it is not proper to apply to the hydrostatic pressure test. The finite element analysis was conducted for the cylinder. The cylinder was produced according to the design. The hydrostatic pressure test was conducted at the hyperbaric chamber in KRISO. The results of finite element analysis(FEM) and those of the hydrostatic pressure test were almost the same, which showed that the design was exact and reliable.