• 제목/요약/키워드: Anti-Icing

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기하구조 및 지형적 요소를 고려한 융설시스템 설치 기준 정립에 관한 연구 (Study about the Standard of Anti-icing System Based on Geography and Geometric Designs)

  • 이동현;정원석;김지원;고석범
    • 한국도로학회논문집
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    • 제13권2호
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    • pp.95-102
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    • 2011
  • 융설액 분사 시스템은 강설이 예상되거나 진행 중인 상황에서 즉시 대응이 가능하며, 강설 초기에 효율적인 처리로 강설로 인해 발생 가능한 교통사고와 교통 지정체를 감소시킬 수 있는 장점을 가지고 있다. 그러나 시스템의 설치비용이 고가이고, 설치되는 장비의 종류에 따라 운영 및 유지관리 비용이 지속적으로 소요되기 때문에 모든 도로 구간에 설치하는 것은 현실적으로 불가능하다. 최근 국내에서는 결빙 위험 구간을 파악할 수 있는 프로그램들이 개발되어 턴키 및 대안 설계에 활용되고 있다. 그러나 프로그램 개발 업체들마다 분석 방식이 상이하고 객관적인 기준이 없는 실정이다. 이에 따라 융설시스템 적용구간에 대한 기준 마련도 시급하다고 볼 수 있다. 본 연구에서는 선형, 기상조건, 일조조건 등을 다양한 도로 조건을 정량화하여 어떤 구간에 우선적으로 융설시스템을 적용하여야 하는지 판단할 수 있는 기준을 제시한다. 이를 위해 국내 지역별 기상 조사, 지형지물에 의해 음지 발생 여부 분석, 선형과 미끄럼 저항성을 고려한 차량 시뮬레이션 등을 수행하고 이론적 검토를 통해 설치 기준 방법론을 정립하는데 중점을 둔다.

항공기 제빙 시스템의 인증에 대한 연구 (Study for Certification of Aircraft De-icing System)

  • 전종협
    • 항공우주시스템공학회지
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    • 제6권2호
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    • pp.7-12
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    • 2012
  • De-icing system is essential for any aircraft to fly in icing conditions. So there are two kinds of aircraft-those that are certificated for flight in icing conditions and those that are not. Icing certification involves a rigorous testing program, and relatively few light aircraft carry this approval. From a legal perspective, aircraft that do not have all required ice protection equipment installed and functional are prohibited from venturing into an area where icing conditions are known. There are a few kinds of de-icing system. It is necessary to review the systems in point of aircraft certification considering the operational and safety issues.

얼음두께를 이용한 결빙시험조건의 간접 확인기법 (Indirect Verification of the Icing Test Condition Using Ice Thickness)

  • 김유경;박남은;최기오
    • 한국항공우주학회지
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    • 제46권11호
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    • pp.944-951
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    • 2018
  • 회전익기의 결빙운용능력이 요구될 경우 자연결빙 비행시험전 풍동시험과 인공결빙시험을 선행하면 개발기간을 단축시킬수 있다. 한국형기동헬기의 경우 인공결빙 시험을 수행하여 각 시험조건에서 방 제빙기능의 정상작동을 확인 후 자연결빙시험을 수행하였다. 인공결빙시험에서 시험조건인 액적량(LWC)과 액적 평균직경(MVD)을 확인하기 위해 정밀센서인 구름기상정보관측기(CCP)를 사용하는데 시험환경, 장비오차등의 이유로 측정치의 불확실성이 존재할 수 있어 시험조건 확인이 다방면으로 필요하다. 동체에 착빙된 얼음두께로부터 LWC를 계산하여 측정값과 비교한 결과, 시험조건을 간접적으로 검증해 볼 수 있는 효과적인 방법임을 확인하였다.

액상분사식 LPG 인젝터의 아이싱 생성 특성 및 억제 방법 (Icing Characteristics in Liquid-Phase Injection of LPG Fuel)

  • 이선엽;김창업;최교남;강건용
    • 한국분무공학회지
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    • 제14권4호
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    • pp.147-152
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    • 2009
  • Since a liquid-phase LPG injection system allows accurate control of fuel injection and increase in volumetric efficiency, it has advantages in achieving higher engine power and lower emissions compared to the mixer type LPG supplying system. However, this system also leads to an unexpected event called icing phenomenon which occurs when moisture in the air near the injector freezes and becomes frost around the nozzle hole due to extraction of heat from surrounding caused by instant fuel vaporization. As a result, it becomes difficult to control air/fuel ratio in engine operation, inducing exacerbation of engine performance and HC emission. One effort to mitigate icing phenomenon is to attach anti-icing injection tip in the end of nozzle. Therefore, in this study, the effect of engine operation parameters as well as surrounding conditions on icing phenomenon was investigated in a bench test rig with commercially-used anti-icing injection tips. The test results show that considerable ice was deposited on the surface near the nozzle hole of the anti-icing tip in low rpm and low load operating conditions in ambient air condition. This is because acceleration of detachment of deposited ice from the tip surface was induced in high load, high rpm conditions, resulting in decrease in frost accumulation. The results of the bench testing also demonstrate that little or no ice was formed at surrounding temperature below a freezing point since the absolute amount of moisture contained in the intake air is too small in such a low temperature.

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회전익기 공기흡입구 주위 방빙장치 성능 해석 (Investigation of the Performance of Anti-Icing System of a Rotorcraft Engine Air Intake)

  • 안국빈;정기영;정성기;신훈범;명노신
    • 한국항공우주학회지
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    • 제41권4호
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    • pp.253-260
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    • 2013
  • 회전익기의 공기흡입구 주위 표면에 발생한 결빙은 엔진의 성능을 저해하는 요인으로 비행 안전성에 심각한 영향을 끼칠 수 있다. 항공기 표면에 발생하는 결빙현상을 분석하는데 많은 비용이 소요되는 결빙 풍동 시험 및 비행시험에 비해 전산유체역학을 기반으로 한 결빙 시뮬레이션은 매우 효과적인 도구가 될 수 있다. 본 연구에서는 결빙조건에서 회전익기 공기흡입구 부근에 설치된 방빙장치의 작동 유무에 따른 결빙의 양과 발생 영역을 CFD 예측기법 및 결빙 풍동시험을 통해 분석하였다. 방빙장치를 작동시킨 경우 공기 흡입구 표면에서의 결빙의 질량과 최대 두께가 약 80% 이상 감소하는 것을 확인하였다.

KC-100 항공기의 표면발생 Icing 형상 및 공력 영향성 연구 (An Investigation of Icing Effects on the Aerodynamic Characteristics of KC-100 Aircraft)

  • 정성기;이창훈;신성민;명노신;조태환;정훈화;정재홍
    • 한국항공우주학회지
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    • 제38권6호
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    • pp.530-536
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    • 2010
  • 비행 중 대기조건에 의한 결빙은 항공기 안전성과 직결되며, 특히 항공기 표면 발생 결빙은 공력 특성 변화를 야기하여 제어면 성능을 저해하는 요소가 된다. KC-100 항공기의 결빙에 의한 공력 영향성 조사를 위해 결빙 전문 CFD 코드인 FENSAP-ICE를 이용하였다. 항공기의 공력 특성을 대표하는 주날개 단면 익형을 먼저 고려하고 다음으로 전기체형상에 대해 결빙 해석을 수행하였다. 또한 Anti-Icing 및 De-Icing 장치 설계를 위해 항공기 부품별 결빙 영역 및 결빙 증식 크기를 조사하였다. 결빙 영역은 주날개 및 수평 꼬리날개의 앞전에서 단면 코드길이 기준 약 7.07%, 11.2% 범위를 나타냈고, Wind Shield의 경우 약 16.7%에서 결빙이 발생하였다. 결빙에 의한 공력특성 변화의 경우, 받음각 0도에서 KC-100 항공기의 양력은 64.3% 감소한 반면 항력은 55.2% 증가하였다.

액상분사식 LPG엔진 인젝터의 후적 및 아이싱 특성에 관한 연구 (A Study of Droplets and Icing Characteristics on Injector in a Liquid Phase LPG Injection Engine)

  • 김창업;최교남;강건용;박철웅
    • 한국분무공학회지
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    • 제12권1호
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    • pp.38-44
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    • 2007
  • Since the Liquid Phase LPG injection (LPLI) system has Advantages in power generation and emission characteristics compared to the mixer-type fuel-supply system, a variety of studies regarding LPLi system has been conducted and its applications are made in automobile industry. However, the heat extraction due to the evaporation of liquid fuel, causes not only a post-accumulation of fuel but also an icing phenomenon which is a frost of moisture in the air around the nozzle tip. Since there exists a difficulty in the accurate control of air fuel ratio in both fuel supply systems, it can result in poor engine performance and a large amount of harmful emissions. This research examines the characteristics of icing phenomenon and develops anti-icing bushing to prevent an icing on the surface of the injection tip. It was found that n-butane, which has a relatively high boiling point ($-0.5^{\circ}C$), was a main species of post-accumulation. Also the results show that the post-accumulation problem was allevaited the utilization of a large inner to outer bore ratio and smooth surface roughness. In addition, an icing phenomenon and its formation process were found to be mainly affected by the humidity and the temperature of inlet air in an inlet duct. Also, it was observed that an icing phenomenon is lessened using aluminum bushing whose end coincides with the end of fuel injection tip in length.

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소수성 표면의 형상 변화를 통한 액적의 방빙 가시화 연구 (Droplet anti icing visualization research through hydrophobic variation of surface structure)

  • 최진욱;Wang Tao;김설하
    • 한국가시화정보학회지
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    • 제21권3호
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    • pp.7-14
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    • 2023
  • In this study, we investigated the freezing delay time on surfaces with different patterns under -30° conditions through visualization experiments. Among various pattern structures, we fabricated the shape and surface of liquid from the spacing using circular filaments and hole structures. Additionally, using a high-speed camera, we visualized the freezing scenes, enabling us to obtain freezing images and measure the freezing time of the liquid. For each structure, the contact angle and solid fraction of the surface varied. We observed that the freezing delay time was longest when the contact angle was largest and the solid fraction was smallest within the experimental results. We analyzed the variation in anti-icing time using the heat exchange equation between the patterned surface and the liquid.

Bioinspired Nanoengineering of Multifunctional Superhydrophobic Surfaces

  • Choi, Chang-Hwan
    • 한국표면공학회:학술대회논문집
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    • 한국표면공학회 2015년도 추계학술대회 논문집
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    • pp.102-133
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    • 2015
  • Nature, such as plants, insects, and marine animals, uses micro/nano-textured surfaces in their components (e.g., leaves, wings, eyes, legs, and skins) for multiple purposes, such as water-repellency, anti-adhesiveness, and self-cleanness. Such multifunctional surface properties are attributed to three-dimensional surface structures with modulated surface wettability. Especially, hydrophobic surface structures create a composite interface with liquid by retaining air between the structures, minimizing the contact area with liquid. Such non-wetting surface property, so-called superhydrophobicity, can offer numerous application potentials, such as hydrodynamic drag reduction, anti-biofouling, anti-corrosion, anti-fogging, anti-frosting, and anti-icing. Over the last couple of decades, we have witnessed a significant advancement in the understanding of surface superhydrophobicity as well as the design, fabrication, and applications of superhydrophobic coatings/surfaces/materials. In this talk, the designs, fabrications, and applications of superhydrophobic surfaces for multifunctionalities will be presented, including hydrodynamic friction reduction, anti-biofouling, anti-corrosion, and anti-icing.

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빙해선박 풍우밀문의 결빙방지 성능평가 및 설계기준에 관한 연구 (A Study on the Anti-lcing Performance Evaluation and Design Guide for Weather-Tight Door of the Vessels Operating in Cold Region)

  • 서영교;정영준
    • 대한조선학회논문집
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    • 제50권6호
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    • pp.450-457
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    • 2013
  • For the design guide of a vessel operating in cold region, numerical analysis was carried out to evaluate the weather-tight door which installed the heating cables by using ANSYS 13.0 Transient Thermal. The numerical analysis was performed by considering Advection-Diffusion equation. This study based on the experimental results of 'A study on Anti-Icing Technique for Weather-Tight Door of Ice-Strengthened Vessels'(Jeong, et al., 2011a) in KIOST. For validation of the numerical analysis results, the cold chamber experimental data measured by the heat sensors in certain location of the weather-tight door was used. The external environmental temperature which varies from $5^{\circ}C$ to $-55^{\circ}C$ was considered in numerical analysis. Also three different heating cables which have the heat capacity of 33W/m, 45W/m and 66W/m were adapted for the design parameters to be the most efficient and guidelines for anti-icing design of the weather tight door.