• 제목/요약/키워드: Duct size

검색결과 181건 처리시간 0.022초

덕트의 입구조건이 팬의 특성에 미치는 영향 (The Effect of Duct Inlet Condition on Flow Characteristics of Fan)

  • 김종수;조강래
    • 설비공학논문집
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    • 제7권2호
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    • pp.217-224
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    • 1995
  • The effects of duct inlet conditions on fan characteristics and upper wind velocity fields were investigated for two kinds of impellers. As the duct inlet condition, the relative positions between duct inlet and fan impeller and the size of baffle plate mounted on a duct inlet were selected. The 3-dimensional velocity components in flow fields were measured by a 5-holes pitot tube. From the results of measurements, it was found that the size of baffle plate scarecely effect on upper wind flow fields and characteristics of fan. It was also confirmed that the upper wind velocity distributions can be estimated by the potential flow field with large baffle plate at duct inlet.

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고속제트 플럼에서의 기저압력 특성 (Characteristics of the Base Pressure in High-Speed Jet Plume)

  • ;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.193-195
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    • 2011
  • An abrupt increase of duct cross-section is frequently encountered in pressure reducing devices, valves of internal combustion engines and in gas pipelines. Supersonic flow in a rectangular duct passing an abrupt increase of cross-section is studied numerically. The behavior of base pressure of the dead-air region at sudden enlargement of the duct is clarified. This investigation concerns the determination of the base pressure, which is independent of the size of the enlarged part. Several flow patterns are identified with different enlargements according to the ratio between the downstream ambient pressure and the upstream reservoir pressure. Base pressure and the resulting shock-structure are highly depending on the size of duct enlargement. For a given duct, base pressure tends to minimum for a particular pressure ratio. In addition, the locations of secondary separation and reattachment points of the jet plume are found with respect to different duct enlargements.

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산적화물선의 에너지 저감 장치들의 성능 비교에 관한 연구 (A Study on the Performance Comparison of Energy Saving Devices for Handy-size Bulk Carrier)

  • 김억규;이강기;조권회
    • Journal of Advanced Marine Engineering and Technology
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    • 제39권1호
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    • pp.1-7
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    • 2015
  • 최근에 CO2 배출에 대한 환경 규제가 마련되었고, 연료유 가격은 계속해서 상승하고 있다. 이런 상황들을 극복하기 위해 연료소모량을 감소시키고 추진효율을 개선한 에너지 저감 추진장치들이 계속해서 개발되고 있다. 본 논문에는 핸디형 산적화물선에 적용한 PBCF, SCHNEEKLUTH duct, 비대칭 러더 벌브, Mewis duct의 성능 실험을 서술하였다. 그 결과, SCHNEEKLUTH duct가 다른 에너지 저감 장치들에 비해 연료소모량 절감과 추진효율의 향상 측면에서 더 효과적이었다. 또한 SCHNEEKLUTH duct가 거주구 진동에도 효과가 있음을 확인하였다. 그리고 연료소모량은 주기관 de-rating을 통해서도 절감할 수 있었다.

등압법과 T-method를 이용한 공조시스템 배관 설계에 관한 연구 (A Study on the Duct Design of HVAC System Using the Equal Friction Method and the T-method)

  • 박준석;최길환;조대승
    • 대한조선학회논문집
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    • 제46권4호
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    • pp.435-443
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    • 2009
  • Optimal duct design of a HVAC system requires analysis technology to accurately evaluate its pressure losses, flow rate and velocity for making a compromised design among fan capacity and duct size affecting initial manufacturing and operation costs, and noise induced by the HVAC system. In this paper, we carry out initial duct design using the equal friction method. Using the result, the T-method is applied for accurate analysis of flow rate. Then, the duct size is modified using the difference between the required and the calculated flow rate, which can guarantee required flow rate, reduce the pressure unbalance among duct paths and lead to select optimal fan performance. To verify the validity and effectiveness of the proposed design method, an example for HVAC system design including noise analysis is demonstrated.

전기구동 림 추진기의 덕트 형상 최적화 연구 (A study on optimization of duct shape of electric hubless rim-driven propeller)

  • 편용범;배재현;김형호;이창제
    • 수산해양기술연구
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    • 제59권1호
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    • pp.65-73
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    • 2023
  • This study analyzed the duct characteristics of hubless rim-driven propeller (RDP) used in underwater robots. In the previous study, flow visualization experiments were performed with an advancing ratio of 0.2 to 1. The vortex at the front of the duct increased in strength while maintaining its size as the advancing ratio decreased. Therefore, it is necessary to study the optimization of the duct shape. Conventional propeller thrusters use acceleration/deceleration ducts to increase their efficiency. However, unlike conventional propellers, it is impossible to apply to airfoil acceleration/deceleration ducts due to the RDP structure. In this study, duct wake flow characteristics, thrust force, and efficiency according to the duct shape of RDP were analyzed using numerical analysis techniques. Duct design is limited and six duct shapes were designed. As a result, an optimized duct shape was designed considering duct wake flow characteristics, thrust force, and efficiency. The shape that the outlet width of the RDP was kept constant until the end of the duct showed higher thrust force and efficiency.

주택환기시스템의 덕트 Layout에 따른 T-Method의 풍량 예측 및 실험 (Air Flow Prediction and Experiment by T-Method According to Duct Layout on House Ventilation System)

  • 주성용;이정재
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.523-528
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    • 2008
  • The accurate distribution of flow rate has been a very important part to control the air change rate since introduction of house ventilation system. An inappropriate selection of fan due to incorrect prediction of pressure loss in duct brings energy loss. In the previous study the pressure loss of general spiral duct was measured and database was constructed for finding correct loss factors in fitting upper stream. The purpose of this study is to compare and investigate the error range of flow rate by applying T-Method to bilateral symmetry and asymmetry layout of duct. The results of this study are as following. It is demanded to decide accurate size under duct design for house ventilation system. Because the small amount of Flow rate was considered at that time. The error range was 3.17% on case1 and 3.52% on case2. The error range difference was 0.35%.

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Numerical Analysis of Flow Uniformity in Selective Catalytic Reduction (SCR) Process Using Computational Fluid Dynamics (CFD)

  • Shon, Byung-Hyun
    • International Journal of Advanced Culture Technology
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    • 제10권3호
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    • pp.295-306
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    • 2022
  • The NOx removal performance of the SCR process depends on various factors such as catalytic factors (catalyst composition, shape, space velocity, etc.), temperature and flow rate distribution of the exhaust gas. Among them, the uniformity of the flow flowing into the catalyst bed plays the most important role. In this study, the flow characteristics in the SCR reactor in the design stage were simulated using a three-dimensional numerical analysis technique to confirm the uniformity of the airflow. Due to the limitation of the installation space, the shape of the inlet duct was compared with the two types of inlet duct shape because there were many curved sections of the inlet duct and the duct size margin was not large. The effect of inlet duct shape, guide vane or mixer installation, and venturi shape change on SCR reactor internal flow, airflow uniformity, and space utilization rate of ammonia concentration were studied. It was found that the uniformity of the airflow reaching the catalyst layer was greatly improved when an inlet duct with a shape that could suppress drift was applied and guide vanes were installed in the curved part of the inlet duct to properly distribute the process gas. In addition, the space utilization rate was greatly improved when the duct at the rear of the nozzle was applied as a venturi type rather than a mixer for uniform distribution of ammonia gas.

흡기계 능동소음제어를 위한 적응형 필터 알고리즘의 개발 (Design of a New VSS-Adaptive Filter for a Potential Application of Active Noise Control to Intake System)

  • 김의열;김호욱;이상권
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 추계학술대회 논문집
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    • pp.231-239
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    • 2009
  • The filtered-x LMS (FX-LMS) algorithm has been applied to the active noise control (ANC) system in an acoustic duct. This algorithm is designed based on the FIR (finite impulse response) filter, but it has a slow convergence problem because of a large number of zero coefficients. In order to improve the convergence performance, the step size of the LMS algorithm was modified from fixed to variable. However, this algorithm is still not suitable for the ANC system of a short acoustic duct since the reference signal is affected by the backward acoustic wave propagated from a secondary source. Therefore, the recursive filteredu LMS algorithm (FU-LMS) based on infinite impulse response (IIR) is developed by considering the backward acoustic propagation. This algorithm, unfortunately, generally has a stability problem. The stability problem was improved by using an error smoothing filter. In this paper, the recursive LMS algorithm with variable step size and smoothing error filter is designed. This recursive LMS algorithm, called FU-VSSLMS algorithm, uses an IIR filter. With fast convergence and good stability, this algorithm is suitable for the ANC system in a short acoustic duct such as the intake system of an automotive. This algorithm is applied to the ANC system of a short acoustic duct. The disturbance signals used as primary noise source are a sinusoidal signal embedded in white noise and the chirp signal of which the instantaneous frequency is variable. Test results demonstrate that the FU-VSSLMS algorithm has superior convergence performance to the FX-LMS algorithm and FX-LMS algorithm. It is successfully applied to the ANC system in a short duct.

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흡기계 능동소음제어를 위한 적응형 필터 알고리즘의 개발 (Design of a New VSS-Adaptive Filter for a Potential Application of Active Noise Control to Intake System)

  • 김의열;김병현;김호욱;이상권
    • 한국소음진동공학회논문집
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    • 제22권2호
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    • pp.146-155
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    • 2012
  • The filtered-x LMS(FX-LMS) algorithm has been applied to the active noise control(ANC) system in an acoustic duct. This algorithm is designed based on the FIR(finite impulse response) filter, but it has a slow convergence problem because of a large number of zero coefficients. In order to improve the convergence performance, the step size of the LMS algorithm was modified from fixed to variable. However, this algorithm is still not suitable for the ANC system of a short acoustic duct since the reference signal is affected by the backward acoustic wave propagated from a secondary source. Therefore, the recursive filtered-u LMS algorithm(FU-LMS) based on infinite impulse response(IIR) is developed by considering the backward acoustic propagation. This algorithm, unfortunately, generally has a stability problem. The stability problem was improved by using an error smoothing filter. In this paper, the recursive LMS algorithm with variable step size and smoothing error filter is designed. This recursive LMS algorithm, called FU-VSSLMS algorithm, uses an IIR filter. With fast convergence and good stability, this algorithm is suitable for the ANC system in a short acoustic duct such as the intake system of an automotive. This algorithm is applied to the ANC system of a short acoustic duct. The disturbance signals used as primary noise source are a sinusoidal signal embedded in white noise and the chirp signal of which the instantaneous frequency is variable. Test results demonstrate that the FU-VSSLMS algorithm has superior convergence performance to the FX-LMS algorithm and FX-LMS algorithm. It is successfully applied to the ANC system in a short duct.

악하선관 내 거대 결석 1예 (One Case of a Large Wharton's Duct Stone)

  • 고준석;강흥수;김진평;우승훈
    • 대한두경부종양학회지
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    • 제27권2호
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    • pp.215-217
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    • 2011
  • Salivary gland calculi account for the most common disease of the salivary glands. We experienced a rare case of submandibular duct(Wharton's duct) calculi of unusual size and shape in a 40 year-old male patient, who presented with pain and swelling in the region of submandibular gland. The author describes the management of this patient and reviews the literature.