• 제목/요약/키워드: concept of the air

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다변량 통계분석을 이용한 서울시 고농도 오존의 예측에 관한 연구 (Prediction of High Level Ozone Concentration in Seoul by Using Multivariate Statistical Analyses)

  • 허정숙;김동술
    • 한국대기환경학회지
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    • 제9권3호
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    • pp.207-215
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    • 1993
  • In order to statistically predict $O_3$ levels in Seoul, the study used the TMS (telemeted air monitoring system) data from the Department of Environment, which have monitored at 20 sites in 1989 and 1990. Each data in each site was characterized by 6 major criteria pollutants ($SO_2, TSP, CO, NO_2, THC, and O_3$) and 2 meteorological parameters, such as wind speed and wind direction. To select proper variables and to determine each pollutant's behavior, univariate statistical analyses were extensively studied in the beginning, and then various applied statistical techniques like cluster analysis, regression analysis, and expert system have been intensively examined. For the initial study of high level $O_3$ prediction, the raw data set in each site was separated into 2 group based on 60 ppb $O_3$ level. A hierarchical cluster analysis was applied to classify the group based on 60 ppb $O_3$ into small calsses. Each class in each site has its own pattern. Next, multiple regression for each class was repeatedly applied to determine an $O_3$ prediction submodel and to determine outliers in each class based on a certain level of standardized redisual. Thus, a prediction submodel for each homogeneous class could be obtained. The study was extended to model $O_3$ prediction for both on-time basis and 1-hr after basis. Finally, an expect system was used to build a unified classification rule based on examples of the homogenous classes for all of sites. Thus, a concept of high level $O_3$ prediction model was developed for one of $O_3$ alert systems.

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열매체 가열기 설비에서의 폭발위험관리에 관한 연구 (A Study on Explosion Risk Management for Hot Oil Heater)

  • 장철;권진욱;황명환
    • 대한안전경영과학회지
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    • 제19권3호
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    • pp.1-9
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    • 2017
  • In the industrial field, various type of fuel have been used for product processing facilities. Recent for 10 years, the usage of natural gas (NG) was gradually increased. Because it has many merits; clean fuel, no transportation, storage facility and so on. There are common safety concept that strict explosion protection approaches are needed for facilities where explosive materials such as flammable liquid, vapor and gases exist. But some has an optimistic point of view that the lighter than air gases such as NG disperse rapidly, hence do not form explosion environment upon release into the atmosphere, many parts has a conventional safety point of view that those gases are also inflammable gases, hence can form explosion environment although the extent is limited and present. In this paper, the heating equipments (Hot Oil Heater) was reviewed and some risk management measures were proposed. These measures include hazardous area classification and explosion-proof provisions of electric apparatus, an early gas leak detection and isolation, ventilation system reliability, emergency response plan and training and so on. This study calculates Hazardous Area Classification using the hypothetical volume in the KS C IEC code.

최적화 기법을 활용한 UAM 버티포트 수용량 산정방법 연구 (A Study on the UAM Vertiport Capacity Calculation MethodUsing Optimization Technique)

  • 이승준;백호종;박장훈
    • 한국항공운항학회지
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    • 제31권2호
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    • pp.55-65
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    • 2023
  • Due to extreme urbanization, ground transportation in the city center is saturated, and problems such as the lack of expansion infrastructure and traffic congestion increase social costs. To solve this problem, a 3D mobility platform, Urban Air Mobility (UAM), has emerged as a new alternative. A vertiport is a physical space that conducts a similar role to an airport terminal. Vertiport consists of take-off and landing facilities (TLOF, Touchdown and Lift-Off area), space for boarding and disembarking from UAM aircraft (gates), taxiways, and passenger terminals. The type of vertiport (structure, number of facilities) and concept of operations are key variables that determine the number of UAM aircraft that can be accommodated per hour. In this study, a capacity calculation method was presented using an optimization technique (Deterministic Integer Linear Programming). The absolute capacity of the vertiport was calculated using an optimization technique, and a sensitivity analysis was also performed.

비포화 흐름에서 모세관 이력현상 모형의 고찰 : State of The Art (Capillary Hysteresis Model in Unsaturated Flow : State of The Art)

  • 박창근;선우중호
    • 물과 미래
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    • 제25권3호
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    • pp.65-77
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    • 1992
  • 본 연구의 목적은 기존에 발표된 이력현상 모형들을 분류하여 각 모형들의 특징을 비교하고 새로운 이력현상 모형의 형태에 대해 논하고자 한다. 기존에 발표된 이력현상 모형은 내삽모형, 축척모형과 영역모형으로 대별되며, 그중 영역모형만이 이론적 배경을 가지고 있다. 모형의 보정을 위해 한 개의 주곡선의 자료가 필요한 기존의 모형들의 타당성을 검증하기 위하야 Rubicon Sandy Loam과 Dune Sand의 실측자료와 비교하여 본 겨롸, 이들 모형들은 실측자료를 잘 모사할 수 없음을 알 수 있었다. 따라서 새로운 모형의 형태의 가능성을 종속여역모형에서 찾을수 있으며, 종속영역모형주에서도 순수한 매체에 대해 공극으로 공기의 진입에 대한 이웃하는 공극들의 방해효과의 정도를 설명하는 가중치를 도입한 모형(Model III-1, Mualem, 1984)을 단순화시키기 위해 이 모형에 적절한 가정을 부가한 형태의 모형이 새로운 형태의 모형에 대한 하나의 대안이 될 수 있음을 본 연구는 제시하고 있다.

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Design, development and ground testing of hingeless elevons for MAV using piezoelectric composite actuators

  • Dwarakanathan, D.;Ramkumar, R.;Raja, S.;Rao, P. Siva Subba
    • Advances in aircraft and spacecraft science
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    • 제2권3호
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    • pp.303-328
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    • 2015
  • A design methodology is presented to develop the hingeless control surfaces for MAV using adhesively bonded Macro Fiber Composite (MFC) actuators. These actuators have got the capability to deflect the trailing edge surfaces of the wing to attain the required maneuverability, besides achieving the set aerodynamic trim condition. A scheme involving design, analysis, fabrication and testing procedure has been adopted to realize the trailing edge morphing mechanism. The stiffness distribution of the composite MAV wing is tailored such that the induced deflection by piezoelectric actuation is approximately optimized. Through ground testing, the proposed concept has been demonstrated on a typical MAV structure. Electromechanical analysis is performed to evaluate the actuator performance and subsequently aeroelastic and 2D CFD analyses are carried out to see the functional requirements of wing trailing edge surfaces to behave as elevons. Efforts have been made to obtain the performance comparison of conventional control surfaces (elevons) with morphing wing trailing edge surfaces. A significant improvement in lift to drag ratio is noticed with morphed wing configuration in comparison to conventional wing. Further, it has been shown that the morphed wing trailing edge surfaces can be deployed as elevons for aerodynamic trim applications.

초소형 IT 부품 조립을 위한 지능형 민첩 생산시스템 (Agile and Intelligent Manufacturing System for a Small IT Parts Assembly)

  • 김원;강희석;조영준;정지영;서일홍
    • 제어로봇시스템학회논문지
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    • 제13권5호
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    • pp.499-506
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    • 2007
  • The tiny camera module used in a modern cellular phone requires precise assembly processes. To meet the requirement of high resolution and functionality, the number of parts used in a camera module becomes larger and larger. As the market grows rapidly, an automatic camera phone assembly process is required. However, diverse production line and short life cycle make it difficult to build an affordable assembly line. To attack this problem, a flexible and expandable lens assembly system is proposed. To save the manufacturing line set-up time, modular concept is adopted. Also, each module is designed to have intelligence to simplify the set-up process. The assembly system is built up on the standard flat-form that includes a vibration free base, air and electric supplies, and electronic controllers, etc. Furthermore, the assembly cell has the capability of handling tiny, thin, or transparent parts which are very difficult to identify without machine vision.

KARI의 헬리콥터 로터 소음관련 기술개발 현황 (Status of Helicopter Rotor Noise Technology Development in KARI)

  • 황창전;정기훈;송근웅;주진;이욱
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.187-192
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    • 2006
  • Helicopter noise has been considered as one of major design factors like a performance and safety since the public acceptance, comfortability and stealth aspects were important for customers. According to the airworthiness regulation, the noise levels in throe different flight conditions shall comply with the specific limits. Main and tail rotors noise is most dominant in far field due to the low and mid range frequency characteristics. It is an air-born noise so That the accurate aerodynamic data is necessary for the accurate noise prediction. In KARI, low noise main and tail rotors as well as analysis codes have been developed since 2000. The approach for low noise main rotor is a kind of tip modifications, so called twin vortices tip to reduce the BVI noise. Analysis results show the 9.3dB reduction in terms of pseudo EPNL. The uneven spacing concept is applied for low noise tail rotor. Three or four decibel noise reduction is achieved by new optimized uneven spacing. Rotor noise and aerodynamic prediction codes have been improved also.

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SK케미칼 연구소에 적용된 친환경 기술 적용 효과 분석 - 에너지 및 수자원 절감 적용 효과를 중심으로 - (The Analysis on Eco-friendly Technologies Effect Applied to SK Chemicals R&D Center)

  • 유지용;이유하;이영렬;양재웅;박현근
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2009년도 하계학술발표대회 논문집
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    • pp.409-414
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    • 2009
  • The SK Chemical R&D center is an eco-friendly building designed as top score in the GBCC(GREEN BUILDING CERTIFICATE CRITERIA). This building has applied various eco-friendly technologies such as energy /water resource cutdown, improvement of indoor quality and improvement of user convenience, etc through eco-friendly concept from the design phase. In this thesis, an economic efficiency evaluation has been performed on building energy cwater resource cutdown technologies among them and the results are as follows. The building energy has cut down about 40% compared to ordinary buildings and the investment recovery period was shown as about 5 years. The water resource has cut down about 63% compared to ordinary buildings and the investment recovery period was shown as about 10 years.

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인간-기계 인터페이스 및 증강현실 기술의 항공운항 분야 적용 (Application of Human Machine Interface and Augmented Reality Technology to Flight Operation)

  • 박형욱;정준;장조원;주성현;황영하
    • 한국항공운항학회지
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    • 제27권2호
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    • pp.54-69
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    • 2019
  • The primary objective of this paper is to introduce the application of Human-Machine Interface (HMI) and Augmented Reality (AR) technologies in flight operations. These include: self-check-in, baggage handling, airport security and surveillance, airport operations monitoring, In-Flight Entertainment and Connectivity (IFEC), cockpit design, and cabin crew support. This paper investigates the application status and development trends of HMI and AR technologies for airports and aircraft. These technologies can provide more efficient in-flight passenger service and experience by using AR devices. This paper also discusses the developments such as; the Integrated Control Application (ICA) for the IFEC interface, AR flight simulation training program using the fixed-based simulator, and the AR aircraft cabin interior concept test program. These applications present how HMI and AR techniques can be utilized in actual flight operations. The developed programs in this paper can be applied to their purpose within aircraft interiors and services to enhance efficiency, comfort, and experience.

가스터빈에서의 연소불안정 현상 (Combustion Instability in Gas Turbine Engines)

  • 오정석;윤영빈
    • 한국추진공학회지
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    • 제12권4호
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    • pp.63-77
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    • 2008
  • 본 논문에서는 가스터빈에서의 연소불안정 현상과 그 메커니즘에 대해 살펴보았다. 연소불안정 연구를 위한 접근 방법이 논의되었고 전 세계 연소불안정 관련 연구그룹들의 최신 연구동향이 소개되었다. 현재까지도 연소불안정현상은 기관의 성능, 내구성, 작동 등에 영향을 미치는 중요한 문제 중의 하나이다. 덧붙여 가스터빈기관에서 연소불안정 현상은 공기 또는 연료의 섭동과 열방출율 사이의 상호 중첩된 결과로 알려져 있으며, 이는 NOx 감소 전략과도 관련이 있다. 따라서 연소불안정 연구에 대한 현황을 이해하기 위하여 가스터빈에서의 연소불안정 현상에 대하여 정리하여 보았다.