• Title/Summary/Keyword: 팬성능

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Performance/Noise Optimization of Centrifugal Fan Using Response Surface Method (반응표면법을 이용한 원심팬 성능/소음 최적화)

  • Shin, Donghui;Heo, Seung;Cheong, Cheolung;Kim, Tae-Hoon;Jung, Jiwon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.41 no.3
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    • pp.165-172
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    • 2017
  • In this study, centrifugal fan blades used to circulate cold air inside a household refrigerator were optimized to achieve high performance and low noise by using the response surface method, which is frequently employed as an optimization algorithm when multiple independent variables affect one dependent variable. The inlet and outlet blade angles, and the inner radius, were selected as the independent variables. First, the fan blades were optimized to achieve the maximum volume flow rate. Based on this result, a prototype fan blade was manufactured using a 3-D printer. The measured P-Q curves confirmed the increased volume flow rate of the proposed fan. Then, the rotation speed of the new fan was decreased to match the P-Q curve of the existing fan. It was found that a noise reduction of 1.7 dBA could be achieved using the new fan at the same volume flow rate.

Numerical Investigation of Ground Effect of Dual Ducted Fan Aircraft During Hovering Flight (제자리 비행하는 이중 덕트 팬 비행체의 지면 효과에 대한 수치적 연구)

  • Lee, Yujin;Oh, Sejong;Park, Donghun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.10
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    • pp.677-690
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    • 2022
  • By using an actuator disk method based flow solver, aerodynamic analysis is carried out for a dual ducted fan aircraft, which is one of the VTOL compound aircrafts, and its associated ground effect is analyzed. The characteristics and accuracy of the solver for ground effect analysis is evaluated through a comparison with the results obtained from the sliding mesh technique. The aerodynamic performance and flow field characteristics with respect to the distance from the ground are analyzed. As the ground distance decreases, the fan thrust increases, but the deterioration of total normal force and hovering flight efficiency is identified owing to the decrease in the vertical force of the duct, fuselage, and wing. By examining the flow field in the bottom of the fuselage, the ground vortices and fountain flow generated by the interaction of the fan wake and ground are identified, and their influence on the aerodynamic performance is analyzed. The strength and characteristics of outwash with respect to the ground distance and azimuth direction are analyzed through comparison/examination of velocity profile. Influence of the ground effect with respect to collective pitch angle is also identified.

The Performance Evaluation of the Exhaust Stack used in High Riser Public House (초고층 공동주택 국소배기용 입상덕트의 배기성능평가)

  • Kwon, Yong-Il;Kim, Ung-Yong;Shin, Hyun-Gon
    • Journal of the Korea Organic Resources Recycling Association
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    • v.22 no.3
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    • pp.60-67
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    • 2014
  • Exhaust system used in toilet and cooking place of high riser public house is roof fan of two basic types : natural roof ventilator and natural/forced roof ventilator. Natural/forced roof ventilator has a motor in the rotary shaft. There are many high riser public house in Korea. These buildings were not viewed as being major contributors to exhaust pollutants producted in indoor. It was because many engineers thought that exhaust in high riser building depend on stack effect. This study investigates on stack pressure determined by exterior pressure and the difference pressure control in exhaust stack used in high riser public house. This paper focuses mainly on the effect of the time interval for power supply of motor installed in roof fan with function of natural wind velocity and of exhaust air volume of toilet. It is observed there are higher exhaust efficiency than the existing natural roof ventilator.

Steady-State Performance Simulation and Engine Condition Monitoring for 2-Spool Separate Flow Type Turbofan Engine (2-스풀 분리배기 방식 터보팬 엔진의 성능모사 및 진단에 관한 연구)

  • Gong, Chang Deok;Gang, Myeong Cheol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.4
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    • pp.60-68
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    • 2003
  • In this study, a steady state performance analysis program was developed for a turbofan engine, and its performance was analyzed at installed conditions. For the purpose of evaluation, the developed program was compared with the performance data provided by the engine manufacturer. It was confirmed that the developed program was reliable because the results by the developed program were well agreed with those by the engine manufacturer within 3.5%. The non-linear GPA(Gas Path Analysis) program for performance diagnostics were developed, and selection of optimal measurement variables was studied. Furthermore, in order to investigate effects of the number and the kind of measurement variables, the non-linear GPA was analyzed with various measurement sets. Finally, the measurement parameters selected in the previous step were applied to the fault detection analysis of the 2-spool separate flow type turbofan engine.

Study on Performance Improvement Air Cooled Condenser Considering Ambient Condition (대기 조건에 따른 공랭식 응축기 성능 저하 개선 연구)

  • Cha, Hun;Ryu, Gwang-Nyeon;Kim, Jung-Rae
    • Transactions of the KSME C: Technology and Education
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    • v.3 no.3
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    • pp.201-207
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    • 2015
  • Air cooled condenser for power plant is used at inland area of desert or mountainous area because condenser coolant like sea water is not necessary. However, the performance of air cooled condenser is influenced by ambient condition such as wind speed and air temperature. Therefore, various devices have been designed to improve the performance of air cooled condenser. In this study, the CFD analysis for air cooled condenser was carried out according to wind speed and wind screen configuration. As wind speed increased from 3m/s to 7m/s, the fan flow rate was reduced about 15.76% and the rise of inlet air temperature was 5.55 degree of Celsius. When the suitable wind screen is equipped, the fan flow rate went up about 5.18% and inlet air temperature dropped by 2.08 degree of Celsius in comparison with original case without wind screen at 7m/s wind speed.

Evaluation of Smoke Control Performance of Ventilation System Using by Hot Smoke Test (Hot Smoke Test를 이용한 주차장 환기설비의 제연 성능평가)

  • Joung, Suckhwan
    • Journal of Korean Society of Disaster and Security
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    • v.12 no.2
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    • pp.47-56
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    • 2019
  • Recently, in order to overcome the difficulty of entering a fire source due to the occurrence of a large amount of smoke in the event of a fire in a parking lot, it has used that a method of discharge smoke using air supply, exhaust fans and jet fans installed for ventilation of parking lots. In this study, the variation of flow in the smoke layer was observed using CCTV under two conditions, in which only the air supply fan operates and the manned fan operates together, and the temperature around the plume was compared to Albert eq. to assess its suitability as a parking lot ventilation performance evaluation method. As a result, it was found that the smoke layer could be disturbed if the Jet Fan was operated at the same time, which could lead to the possibility of an initial evacuation disturbance. However, the additional operation of the Jet Fan has been confirmed by the observation CCTV that the emission performance is improved, which is believed to help conduct the suppression operation. The temperature around the plume was measured and compared to Alpert eq, and was analyzed to be about $2^{\circ}C$ lower at the center axis of the plume and $9.0^{\circ}C$ higher at 8 m in the direction of the discharge of smoke. The results of temperature measurements around the plume were lower than the maximum temperature expected in AS 4391 and did not exceed the expected temperature risk caused by the experiment. As with these results, the temperature risk from the progression of hot smoke tests is foreseeable, so it will be available as one of the general evaluation methods for assessing smoke control performance in a parking lot without relevant criteria.

Numerical Analysis of Flows for Agricultural Dryer with Heat Pump (히트펌프를 이용한 농산물 건조기 유동 수치해석)

  • Park, Sang-Jun;Lee, Young-Lim
    • Proceedings of the KAIS Fall Conference
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    • 2011.05b
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    • pp.676-678
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    • 2011
  • 히트펌프 사이클을 이용한 건조 공정은 최종 제품의 생산을 위하여 많은 산업 분야에 요구되는 필수 공정으로 본 논문에서는 대형 히트펌프 건조기의 상부 분리대의 가이드 베인의 형상 및 수량을 최적화 하였다. 이를 위해 팬은 성능곡선 모델을 사용하였고, 증발기와 응축기는 다공성 매질로 가정하였다. 이는 팬을 통과하여 가이드 베인을 따라 건조기 입구로 들어가는 바람의 균일도를 예측할 수 있어 설계 정확도 향상에 기여할 수 있다.

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Simulation of Ventilation Capability Effect on The Smoke Spread in Railway Station (제연 팬 용량이 철도역사 연기확산에 미치는 영향 분석)

  • Jang, Yong-Jun;Koo, In-Hyuk;Kim, Hag-Beom;Kim, Jin-Ho
    • Proceedings of the KSR Conference
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    • 2011.05a
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    • pp.7-13
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    • 2011
  • Simulation study were performed for ventilation capability effect on the smoke spread in the deeply-underground subway station(DUSS). Singeumho station(The line # 5, Depth: 46m) was modeled and were analyzed for smoke-spread speed difference between the originally-designed-ventilation-capacity and the measured-ventilation-capacity. Field test data for actual fan in DUSS was applied as a boundary condition of a simulation. The whole station was covered in this analysis and total of 4 million grids were generated for this simulation. The fire-driven flow was analyzed case by case to compare the smoke-spread effects. In order to enhance the efficiency of calculation, parallel processing by MPI was employed and large eddy simulation method in FDS code was adopted.

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Effect of pitch angle and blade length on an axial flow fan performance (피치각과 날개 길이 변화에 따른 축류팬의 성능 및 소음 특성에 관한 실험적 연구)

  • Jeon, Sung-Taek;Cho, Jin-Pyo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.7
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    • pp.3170-3176
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    • 2013
  • In this study, the performance of an impeller according to blade length and pitch angle was studied experimentally by building a variable pitch impeller while changing blade length to review the effect of blade length and pitch angle on a fan's performance and sound characteristics. The pitch angle was changed in six steps from $20^{\circ}{\sim}45^{\circ}$ at intervals of $5^{\circ}$ while the blade lengths were changed 80 mm, 90 mm, 100 mm, 110 mm and 120 mm with an identical airfoil shape while carrying out the experiment.