• Title/Summary/Keyword: 공기구

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Evaluation of Composting Characteristics According to the Air Supply Change in Farm-Sized Swine Manure (농가규모 양돈분뇨 퇴비화시 공기공급량 변화에 따른 퇴비 특성 평가)

  • Lee, Sunghyoun;Jeong, Gwanghwa;Lee, Dongjun;Lee, Donghyeon;Jang, Yuna;Kwag, Junghoon
    • Journal of the Korea Organic Resources Recycling Association
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    • v.27 no.3
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    • pp.49-61
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    • 2019
  • Swine manure has been recognized as a organic sources for composting and many research was conducted to efficiently utilize and treat. This study was to evaluate a feasibility for producing swine manure compost under various treatment with mixture of swine manure and saw dust. Treatments were designed as follows; non aerated composting pile(REF), aerated composting pile of $100L/m^3$(EXP1), and aerated composting pile of $150L/m^3$(EXP2). The total days of fermentation were 28 days and each samples were collected at every 7 days from starting of composting. Temperature sensors were installed under 30~40cm from the surface of composting pile. Inner temperature in composting piles of EXP1 and EXP2 was rapidly increased to $67{\sim}75^{\circ}C$ within 1~2 days. The elevated temperatures found during the thermophilic phase are essential for rapid degradation of organic materials. While swine manure composted, moisture content, total nitrogen, EC of EXP1, EXP2 in sample at 28 days were lower than those of REF. But, pH and organic matter of EXP1, EXP2 in sample at 28 days were higher than those of REF. After finishing fermentation experiment, maturity was evaluated with germination test. Calculated germination index(GI) at REF, EXP1 and EXP2 were 23.49, 68.50 and 51.81, respectively. The values of germination index were higher at EXP1 and EXP2 which is aerated composting piles than REF which is non aerated composting pile. According to the results, composting process by aerated static pile compost had significant effect on the reduction of required period for composting. Supplying adequate amount of air to compost swine manure will greatly reduce composting period.

Characteristics of the Transverse Fuel Injection into a Supersonic Crossflow using Various Injector Geometries (분사구 형상에 따른 초음속 유동장 내 수직 연료 분사 특성)

  • Kim, Seihwan;Lee, Bok Jik;Jeung, In-Seuck;Lee, Hyoungjin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.3
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    • pp.53-64
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    • 2018
  • In this study, computational simulation was performed to investigate the characteristics of air/fuel mixing according to the shape of the injector exit when the transverse jet was injected into a supersonic flow. Non-reacting flow simulation was conducted with fixed mass flow rate and the same cross-sectional area. To validate the results, free stream Mach number and jet-to-crossflow memetum ratio are set to 3.38 and 1.4, respectively, which is same as the experimental condition. Further, separation region, structure of the under-expended jet, jet penetration height, and flammable region of hydrogen for five different injectors compared.

Efficient Opaque Ice Sphere Formation Using a Lightweight Geometric Approach

  • Jong-Hyun Kim
    • Journal of the Korea Society of Computer and Information
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    • v.29 no.3
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    • pp.91-98
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    • 2024
  • In this paper, we present a particle-grid blending framework based on a geometric approach to efficiently represent opaque ice spheres with air bubbles. The water temperature is diffused through the grid and the air bubbles represented inside the ice through the particles. To solve the problem of previous methods that generate noisy dissolved air fields, we use levelsets to lighten the algorithm, i.e., the number of active particles and the initial amount of dissolved oxygen can be used to efficiently control the termination conditions of heat diffusion. We also extend the previous dissolved air field method, which only computes near air bubbles, to transparent regions to represent realistic ice spheres, and introduce a levelset-based approach to accurately compute the orientation of particles. As a result, the method presented in this paper is about three times faster than the existing methods and shows visually improved visualization of opaque ice spheres, which can be used in the field of representing physical virtual ice forms.

외부가압 공기베어링의 동적 특성에 관한 해석

  • 김우정;박상신;한동철
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1991.11a
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    • pp.22-28
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    • 1991
  • 최근 전자 및 광학분야에 있어서의 눈부신 발전은 비구면 가공기나 초정밀 연삭기와 같은 초정밀 가공기계의 개발과 실용화에 힘입은 바 크다. 이러한 초정밀 가공기의 성능을 좌우하는 핵심요소로서 주축계를 들 수 있으며, 비교적 소형 경량의 공작물을 가공하는 기계의 주축용 베어링으로는 오일 베어링을 대신하여 공기베어링이 점차 널리 사용되고 있다. 본 논문에서는 점급기원의 가정하에 직접수치해법을 사용하는 해석 프로그램을 작성하여, 무차원화된 설게 변수들에 대한 외부가압 공기베어링의 정$\cdot$동특성수들을 구하고, 여기서 구해진 베어링의 정$\cdot$동특성수를 사용하여 베어리으이 공기막 반력을 계산한 후, 축중심 궤적의 비선형 해석을 수행함으로써 주축 회전 정도를 예측하고자 한다.

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Study on the Flow Characteristics of Supersonic Air Intake at Mach 4 (마하4 초음속 공기 흡입구 유동 특성에 관한 연구)

  • ;;;;Shigeru , Aso
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.10
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    • pp.61-70
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    • 2006
  • A Supersonic air intake model was designed for the high performance ramjet and dual-mode scramjet engine to operate at Mach 4 flight condition. The air intake was tested in the blowdown-type wind tunnel of Kyushu University to identify the internal flow characteristics corresponding to the flight parameters such as the back pressure, angle of attack and angle of yaw. Flow visualization was achieved by the Schlieren and oil flow visualization techniques. The intake performance was analyzed quantitatively based on the surface pressure and total Pressure measurements. The experimental results were compared with the computational fluid dynamics results. The present study exhibits the fundamental but rarely found experimental results of the high Mach number supersonic air intake.

The Study of Aerodynamic Characteristics of Ram-jet with Different Intake (서로 다른 램제트 흡입구에 따른 공기역학적 특성 연구)

  • Park, Soon-Jong;Park, Jong-Ho
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.6
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    • pp.9-16
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    • 2010
  • The SFRJ(Solid Fuel Ram-Jet) propulsion is attractive for projectiles because of the combination of high propulsive performance and low system complexity more than conventional projectiles. The Objective of this research was to characterize the inlet aerodynamic characteristics (center-body & pitot type) in SFRJ. Diffuser static pressure & combustion chamber pressure was tested and the AoA was changed $0^{\circ}$ and $4^{\circ}$ at Mach number of 3.0 for performance estimate. The performance study of inlet was carried out with the Schlieren system and Supersonic cold-flow system. Under mach 3.0, the center-body showed twice higher total pressure recovering ratio than the pitot type. A Computational fluid dynamic solution is applied internal flow of inlet and the solutions are compared with experimental results.

A Study on Health Check Solution using Indoor Air Purifier (실내 내장형 공기순환기를 이용한 헬스 체크 솔루션에 관한 연구)

  • Yang, Hee-Tak;Oh, Ji-Su;Lee, Keun-Ho
    • Journal of Internet of Things and Convergence
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    • v.3 no.1
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    • pp.25-31
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    • 2017
  • In the future a future type new city and the latest apartment will be built, and the IoT technology will be constructed and combined in large numbers indoors of ordinary households. An air cleaner that makes people in it comfortable is built in, and the suction port that sucks in the air of the air purifier and the discharge port that discharges it are set up around the room and come out. However, this is impossible to adjust because there is only a central switch on / off. Also, consuming a lot of electricity so that many electricity charges are caused by huge electricity consumption will eventually be a waste of resources. This would like to be adjusted and driven through the fine dust detection device to the room built-in air purifier and that has provided a solution to save electricity. In addition, since it exists in and around the room, you can grasp the position of the person and connect to the home network to enhance the convenience. Also, through analysis of the air, we provide a health-check solution that checks the user's health and adjusts it appropriately.

Investigation on the Characteristics Variation According to Air Supply Capacity in Layer Manure by Composting (공기공급량에 따른 산란계분의 퇴비화 특성변화에 관한 연구)

  • Kwag, J.H.;Cho, S.H.;Jeong, K.H.;Kim, J.H.;Choi, D.Y.;Jeong, Y.S.;Jeong, M.S.;Kang, H.S.;Ra, C.S.
    • Journal of Animal Environmental Science
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    • v.16 no.2
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    • pp.135-142
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    • 2010
  • The composting of layer manure is economical and efficiently process. In this study, the variation of composting characteristics in layer manure was investigated according to air supply capacity. The fermented compost was added in layer manure and mixed with sawdust inside composting reactors. The level of air supply capacity was varied in the range of $50{\sim}200\;{\ell}/m^3/min$. During composting the temperature variations of composting piles was different the temperatures of composting piles for T-1 ($50\;{\ell}/m^3/min$) and T-2 ($100\;{\ell}/m^3/min$) were reached at $40^{\circ}C$ and $50^{\circ}C$ within 2 days, respectively. For T-3 ($150\;{\ell}/m^3/min$) and T-4 ($200\;{\ell}/m^3/min$), their temperatures was $60^{\circ}C$ within same days and maintained during 8 days. Water contents decreased according to the air supply capacity; 8.9%, 15.4%, 18.0% and 18.6% for T-1, T-2, T-3 and T-4. The weight ratios of T-1, T-2, T-3 and T-4 were reduced to 12.8%, 15.6%, 18.1% and 17.9%, respectively. The decreasing volumetric ratios of T-1, T-2, T-3 and T-4 were 18.0%, 21.0%, 22.3% and 22.0%. The oxygen discharge concentrations during composting were 12 ppm for T-1, T-2 and 9 ppm for T-3 and T-4. After composting, fertilizer components such as total nitrogen (TN) and phosphorous pentoxide ($P_2O_5$) were examined at each air supply capacity. Nitrogen contents of the T-1, T-2, T-3 and T-4 were 0.75%, 0.74%, 0.72% and 0.64%. Also, The contents of $P_2O_5$ were 0.35%, 0.40%, 0.38% and 0.42% for T-1, T-2, T-3 and T-4.

램제트 엔진 흡입구 유동 및 연소유동 해석

  • 김성돈;정인석;윤영빈;최정열
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1999.10a
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    • pp.18-18
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    • 1999
  • IRR형태의 액체 램제트 추진기관의 공기 흡입구 유동과 내부 연소 유동을 파악하기 위한 수치적 해석을 수행하였다. 해석은 다원 혼합기체에 대한 압축성 Navier-Stoke 방정식과 공기/Kerosene에 대한 화학 반응을 고려하였으며, 결합된 형태의 k-$\omega$/k-$\varepsilon$ 2 방정식 난류모델을 이용하였다. 기본 유동 해법으로는 고차의 시간 및 공간 정확도를 가지는 근사 Riemann 해법과 LU-SGS 방법을 이용하였다.

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Heating and cooling properties in cultivation room and cultural characteristics of oyster mushroom according to type of air exchange (외부공기 유입방식에 따른 느타리버섯 생육실의 온도변화 및 자실체의 생육특성)

  • Jang, Myoung-Jun;Lee, Yun-Hae;Ju, Young-Cheol
    • Journal of Mushroom
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    • v.11 no.4
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    • pp.214-218
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    • 2013
  • This study was carried out to find out suitable input method for air exchange about bottle cultivation of oyster mushroom. There was no difference of average temperature in cultivation room, but T1(direct introduction of outside air) was higher than T2(heat exchanger) and T3(air buffer) in the standard deviation. The ratio of cooling operating was the highest in August and in the descending order, T1 54%, T3 43%, T2 33%. At ratio of energy reduction, T2 and T3 were higher than T1. The operating ratio of heater was highest in January and in the descending order, T1 53%, T3 37%, T2 30%. At ratio of energy reduction(%), T2 and T3 were higher than T1 similar to result of cooling operating. Therefore there were largest in August about Cooling Degree-Hour and in January about Heating Degree-Hour. And fruitbody yields quality was excellent in T2 and T3 than T1. The suitable effective type of air exchange in oyster mushroom cultivation are heat exchange and air buffer system.