• 제목/요약/키워드: Ice Protection System

검색결과 9건 처리시간 0.022초

항공기 결빙 보호장치의 기술 현황 및 전망 (Current Status and Prospect of Aircraft Ice Protection Systems)

  • 이재원;조민영;김용환;이관중;명노신
    • 한국항공우주학회지
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    • 제48권11호
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    • pp.911-925
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    • 2020
  • 항공기 결빙 보호장치는 항공기의 Window Shield 및 Engine Inlet, Wing 등에 적용되어 운용 중 발생할 수 있는 항공기와 센서의 표면 결빙으로 부터 항공기를 보호한다. 표면에 증식된 결빙은 항공기의 조종 안정성을 저하시키고 대기자료 프로브의 오작동을 일으킴으로써 심각한 사고의 원인이 되기도 하는데, 이를 방지하기 위하여 다양한 방식의 결빙 보호장치가 개발되었다. Electrothermal 방식은 비교적 간단한 구조이고 에너지 효율을 높이는 데 유리하여 가장 많이 사용되는 항공기 결빙 보호장치로 자리매김하고 있다. 본 리뷰 논문에서는 대표적인 결빙 보호장치인 Hot-air 및 Electro-thermal 방식을 집중적으로 분석하였고, 기술 현황과 적용 사례를 바탕으로 결빙 보호장치의 전망에 대해 고찰하였다.

대기 결빙 조건에서의 전기열 방식 결빙보호 시스템에 관한 전산해석 (COMPUTATIONAL ANALYSIS OF AN ELECTRO-THERMAL ICE PROTECTION SYSTEM IN ATMOSPHERIC ICING CONDITIONS)

  • 프린스 라즈;명노신
    • 한국전산유체공학회지
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    • 제21권1호
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    • pp.1-9
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    • 2016
  • Atmospheric icing may have significant effects not only on safety of aircraft in air, but also on performance of wind turbine and power networks on ground. Thus, ice protection measure should be developed to protect these systems from icing hazards. A very efficient method is the electro-thermal de-icing based on a process by which ice accretion is melted and blown away through aerodynamic forces. In this computational study, a state-of-the-art icing code, FENSAP-ICE, was used for the analysis of electro thermal de-icing system. Computational results including detailed conjugate heat transfer analysis were then validated with experimental data. Further, the computational model was applied to the DU21 airfoil section of NREL 5MW wind turbine with calculated heater parameters.

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.

회전익기 공기흡입구의 표면발생 결빙에 관한 전산 예측 (COMPUTATIONAL PREDICTION OF ICE ACCRETION AROUND A ROTORCRAFT AIR INTAKE)

  • 정기영;안국빈;명노신;조태환;정성기;신훈범
    • 한국전산유체공학회지
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    • 제17권2호
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    • pp.100-106
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    • 2012
  • Ice accretion on the surface of aircraft in flight can adversely affect the safety of aircraft. In particular, it can cause degradation of critical aircraft performances such as maximum lift coefficient and total pressure recovery factor in engine air intake. In this study, computational prediction of ice accretion around a rotorcraft air intake is conducted in order to identify the impingement region with high droplet collection efficiency. Then the amount of ice accretion on the air intake, which is essential in determining the required power of ice protection system, is calculated. Finally, the effect of icing wind tunnel size is investigated in order to check the compatibility with the real in-flight test environment.

전문가용 클라이밍 팬츠의 활동 기능성 수요특성 연구 (Professional climbers' demand for movement functionality in pants)

  • 정세미;천종숙
    • 복식문화연구
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    • 제21권2호
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    • pp.261-271
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    • 2013
  • This study aimed to identify professional climbers'demand for movement functionality in pants worn for rock climbing and ice climbing. Data were collected through in-depth interviews with 12 professional climbers using a semi-constructed questionnaire. The respondents were instructor-level experts whose climbing ability ranged from 5.9 to 5.14 on the Yosemite Decimal System rating scale. The research findings were as follows. Experts wore different climbing pants depending on the type of climbing. For example, they mostly wore high-stretch, second layer pants for rock climbing, while layering first layer, second layer, and third layer pants for ice climbing. There were gender differences regarding the parts of the body in which climbers reported the most discomfort when wearing climbing pants; male climbers most commonly responded 'knees', 'inner thighs' and 'hips' while their female counterparts most commonly responded 'inner thighs', 'exposed back and waist' and 'hips' in that order. Differences were found between rock climbing and ice climbing in terms of wear and tear on pants, preferred fabric properties, and length of pants. Wear and tear was found mainly on the hips and knees of rock climbing pants and on the inner lower hem of ice climbing pants. Listed in the order of preference, the most preferred fabric properties were elasticity, light weight, and durability for rock climbing pants and elasticity, insulation, and protection against water and wind for ice climbing pants. Regarding the length of rock climbing pants, respondents preferred ankle-length pants and cropped pants that did not cover the feet. For ice climbing pants, respondents favored heel-length pants that prevented pieces of ice from entering the clothing. Men showed a high level of preference for ergonomically cut climbing pants. Respondents said the waistband on climbing pants should be simplified so as not to adversely affect climbing maneuvers.

Survivability, Mobility, and Functionality of n Rover for Radars in Polar Regions

  • Stansbury, Richard S.;Akers, Eric L.;Harmon, Hans P.;Agah, Arvin
    • International Journal of Control, Automation, and Systems
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    • 제2권3호
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    • pp.343-353
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    • 2004
  • This paper presents the survivability, mobility, and functionality of a rover as part of a radar system for polar regions. Rovers can provide autonomy and precision for radars used to measure ice thickness and other characteristics of ice sheets in Greenland and Antarctica. These rovers can be used to move radar antennas in precise patterns for synthetic aperture radars while providing environmental protection and power to the onboard radar equipment. This paper describes the mobility, actuation, sensing, winterization, control, and virtual prototyping of a polar rover. The rover has been successfully tested in Greenland.

기존 사무소 건물 및 설비전문가 조사를 통한 설비시스템의 변화와 전망에 대한 연구 (A Study on the Transition & Expectation through Survey for Existing Building and Engineer's Opinion)

  • 이관호;김남규;박진철;이언구
    • 한국태양에너지학회 논문집
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    • 제25권2호
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    • pp.63-69
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    • 2005
  • This study is the survey of a transition procedure of building services systems(heat source, HVAC, water supply) through the survey of existing office buildings, building design documents. The preference & major consideration of system selection is the engineer's opinions. The results of this survey can be used in selection of building services system design. In this survey, "Hot & cold water generator system" and "single duct CAV+FCU system", "Elevated water tank system" are selected. The most important consideration in system selection is the energy saving in heat source system, and comfort in HVAC system, and water pressure in water supply system. They prefer "steam boiler+absorption chiller system" for heat source system, "steam boiler+ice thermal storage system", "hot & cold water generator system", "district heating+absorption chiller system" : "single duct CAV+FCU system" and "single duct VAV+convector system" for HVAC system: and "booster pump system" for water supply system.

A FRONTIER OF PARALLEL CFD: REAL-TIME IN-FLIGHT ICING SIMULATION OVER COMPLETE AIRCRAFT

  • Habashi, Wagdi G.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2010년 춘계학술대회논문집
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    • pp.1-1
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    • 2010
  • With the power of supercomputers increasing exponentially, there is an insatiable need for more advanced multi-disciplinary aerospace CFD simulations. A particular current interest is the 3D viscous turbulent simulation of the highly nonlinear aspects of aero-icing. The applications of CFD in that field are literally light-years behind aerodynamics, with a significant number of users still mired in correlations, or 2D, inviscid, incompressible, and, yes, Panel Methods simulations! Thus, the disparity of tools between aerodynamics and icing departments within an organization leads to a disconnect that makes ice protection a downstream isolated process that is not an integral part of the aerodynamic behavior of an aerospace system (aircraft, rotorcraft, jet engine, UAV, etc.). While 3D RANS has been recently introduced, it is still considered computationally too demanding for industry when wide parametric studies for certification are required. In addition, not unlike the situation in aerodynamics say 20 years ago, naysayers are at every corner claiming that CFD is not reliable and is of limited use.

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實環境を考慮したポーラスコンクリートの耐凍害性の評価(실제 환경을 고려한 다공질 콘크리트의 내동해성(耐凍害性) 평가) (Frost resistance of porous concrete assuming actual environment)

  • 中村拓郞;堀口敬;志村和紀;菅原隆
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2008년도 추계 학술논문 발표대회
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    • pp.227-233
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    • 2008
  • Porous concrete has large continuous voids of 20-30 % by volume, and this concrete is attractive as environmental material in Japan i.e. permeable road pavement, river bank protection with vegetation and green roof system which influence thermal environment. It is necessary to confirm the frost resistance when constructing porous concrete structure in cold region. However applicable test method and evaluation criterion of porous concrete has not defined yet. Therefore, the object of this study is to investigate the frost resistance of porous concrete and this investigation attempts to address this concern by comparing 4 kinds of specified freezing and thawing tests methods (JIS A1148 procedure A/B and RILEM CIF/CDF test) in consideration of actual environment. RILEM freeze-thaw tests are different from JIS A1148 freeze-thaw tests, which are widely adopted for evaluating the frost resistance of conventional concrete in Japan, in water absorption, cooling rate, length of freezing and thawing period, and number of freezing and thawing cycles. RILEM CIF test measures internal damage and is primarily applicable for pure frost attack. CDF test is appropriate for freeze-thaw and de-icing salt attack. JIS A1148 procedure A/B showed extremely low frost resistance of porous concrete if the large continuous voids were filled with water and the ice expansion in the large continuous voids set in during cooling. Frost resistance of porous concrete was improved by mixing coarse aggregate (G7) which particle size is smaller and fine aggregate in JIS freezing and thawing tests. RILEM CIF/CDF test showed that freeze-thaw and de-icing resistance of porous concrete was seems to be superior in that of conventional concrete.

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