• Title/Summary/Keyword: 팬성능

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Measuring performance and SPL of refrigerator fan using anechoic fan tester (무향팬테스터를 이용한 냉장고용 팬 성능/소음 측정)

  • Jeoung, Jeoung-Kyo;Lee, Jun-Hwa;Joo, Jae-Man;Kang, Jung-Hun
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.11a
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    • pp.253-256
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    • 2004
  • Acoustical noise at low frequency range (below 500Hz) of refrigerator result from fans which are inside of the refrigerator. In generally to evaluate and apply to refrigerator it is recommended that acoustical noise and fluidic performance of the fan were measured simultaneously. To do that twin-room type anechoic wind tunnel was needed. But constructing twin room type anechoic wind tunnel was very expensive and estimation of small refrigerator fan performance was not easy. So in this paper we composed anechoic fan tester. A successful noise and performance measurement was performed using the anechoic fan tester. Existing 22 kinds of refrigerator fan were investigated and mapped into one database. Refrigerator duct pressure resistance were measured and reflected into the fan database to find out appropriate fan. Through the application of fan database, the refrigerator became less noise compared to current one and these data shows what is the best way to reduce fan noise.

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Experimental study of improvement of ventilation efficiency at intersection in network-form underground road tunnel (네트워크형 지하 도로터널 분기부에서의 환기효율 향상방안에 대한 실험적 연구)

  • Lee, Ho-Seok;Hong, Ki-Hyuk;Choi, Chang-Rim;Kang, Myung-Koo;Lim, Jae-Bom;Mun, Hong-Pyo
    • Journal of Korean Tunnelling and Underground Space Association
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    • v.14 no.2
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    • pp.107-116
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    • 2012
  • The experiment was performed to analyze the intersectional ventilation efficiency by intersection structure and Jet Fan in network-form road tunnel. For this, the size of real road tunnel was reduced by 1/45. To apply traffic inertia force when driving, blower fan was used to form an airflow in model tunnel and the intersectional efficiency was also investigated by measuring the speed at local point of the tunnel. To improve the reduction of ventilation caused by the structure character, Jet Fan was installed to optimize ventilation efficiency in tunnel.

A Realization of Real Time Algorithm for Fault and Health Diagnosis of Turbofan Engine Components (터보팬엔진의 실시간 구성품 결함 및 건전성 진단 알고리즘 구현)

  • Han, Dong-Ju;Kim, Sang-Jo;Lee, Soo-Chang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.10
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    • pp.717-727
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    • 2022
  • An algorithm is realized for estimating the component fault and health diagnosis such as a deterioration. Based on the turbofan engine health diagnosis model, from the health parameters which are estimated by a real time tracking filter, the outliers are eliminated efficiently by an effective median filter to minimize an false alarm. The difference between the fault and deterioration trends is identified by the detection measure for abrupt change, thereby the clear diagnosis classifying the fault and the health condition is possible. The effectiveness of the algorithm for fault and health diagnosis is verified from the simulated results of engine component faults and deterioration.

Periodic and Pseudo-static Channel Time Allocation Scheme for IEEE 802.15.3 High-Rate Wireless PANs (IEEE 802.15.3 고속율 무선 팬을 위한 주기적인 유사 정적 채널 시간 할당 방법)

  • Kim, Sun-Myeong
    • Journal of the Korea Society for Simulation
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    • v.17 no.4
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    • pp.89-97
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    • 2008
  • In wireless personal area networks (WPANs), the successful design of channel time allocation algorithm is a key factor in guaranteeing the various quality of service (QoS) requirements for the stringent real-time constraints of multimedia services. In this paper we propose a channel time allocation algorithm for achieving a high quality transmission and high channel error tolerance of MPEG stream in the IEEE 802.15.3 high-rate wireless PANs. Our algorithm exploits the characteristics of MPEG stream. When a new MPEG stream arrives, a DEV models it by the traffic envelope and delivers the traffic envelope to the piconet coordinator (PNC) along with the channel time request. The PNC performs channel time allocation according to the envelope. Performance of the proposed scheme is investigated by simulation and analysis. Our results show that compared to conventional scheme, the proposed scheme is very effective and provides a good performance under typical channel error conditions.

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Optimal Design of the Stacking Sequence on a Composite Fan Blade Using Lamination Parameter (적층 파라미터를 활용한 복합재 팬 블레이드의 적층 패턴 최적설계)

  • Sung, Yoonju;Jun, Yongun;Park, Jungsun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.6
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    • pp.411-418
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    • 2020
  • In this paper, approximation and optimization methods are proposed for the structural performance of the composite fan blade. Using these methods, we perform the optimal design of the stacking sequence to maximize stiffnesses without changing the mass and the geometric shape of the composite fan blade. In this study, the lamination parameters are introduced to reduce the design variables and space. From the characteristics of lamination parameters, we generate response surface model having a high fitness value. Considering the requirements of the optimal stacking sequence, the multi-objective optimization problem is formulated. We apply the two-step optimization method that combines gradient-based method and genetic algorithm for efficient search of an optimal solution. Finally, the finite element analysis results of the initial and the optimized model are compared to validate the approximation and optimization methods based on the lamination parameters.

Control System of Turbofan Engine with Variable Inlet Guide Vane (가변 안내익을 이용한 터보팬 엔진 제어시스템)

  • Bae, Kyoungwook;Min, Chanoh;Cheon, Bongkyu;Lee, Changyong;Lee, Daewoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.3
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    • pp.237-242
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    • 2014
  • Surge phenomenon can be occurred in a compressor when the performance of turbofan engine for an aircraft is changed considerably such as take-off phase. This study is aimed to avoid surge phenomenon. This paper propose the PID and Fuzzy control System for the turbofan engine with control inputs, the VIGV(Variable Inlet Guide Vane) in closed loop, and the fuel mass flow in open loop. We design the Dynamic modeling, NPSS S-function, which is connection block of simulink between NPSS(Engine analysis program) and Simulink. Finally, we certify the performance to prevent a serge phenomenon in the VIGV control system using the both methods, PID and fuzzy.

Optimization of Fan-Shaped Hole for Gas Turbine Blade on Thin Wall (가스터빈 블레이드의 얇은 벽에서의 팬 형상 홀 최적화)

  • Hyun, Minjoo;Park, Hee Seung;Kim, Taehyun;Song, Ho Seop;Lee, Hee Jae;Cho, Hyung Hee
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.4
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    • pp.71-77
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    • 2021
  • Several cooling techinques have been studied for protecting gas turbine blades from hot gas. In terms of film-cooling techniques, various shapes of film cooling holes have been studied including fan shaped holes, which are used on gas turbine blades. However, owing to increasing demands on smaller gas turbines, a research on film-cooling holes on thin walls is required. This study was conducted at blowing ratios of 1 and 2, using numerical analysis. Through the numerical analysis, the effect of geometrical parameters on the effectiveness of fan-shaped hole film cooling was studied. Moreover, optimization was performed on three geometrical parameters: metering length, lateral expansion angle and forward expansion angle. As a result, we realized that the optimal fan-shaped holes on each blowing ratio were found to have very similar geometry and cooling performance.