• Title/Summary/Keyword: 오리피스블레이드

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Comparison of the Performance of the VAV Dampers for the Circular Duct (원형 덕트용 VAV 댐퍼의 성능 비교)

  • Kwon, Young-Pil
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.24 no.9
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    • pp.699-703
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    • 2012
  • The performance of the typical VAV dampers; blade type, venturi type and blade-orifice type, for the circular duct, is obtained by measuring the volume flow rate as a function of the opening degree. The performance features are discussed by comparing the volume flow rate of each damper. It is shown that the blade-orifice type damper, recently developed, is excellent in its linearity of the performance and that it is worse than the blade type but much better than the venturi type in its flow resistance.

Effect of Blade Number Variations on Performance of Micro Gravitational Vortex Turbine in Free Water Surface (자유수면에서 블레이드 수 변화가 마이크로 중력식 와류 수차 성능에 미치는 영향)

  • Jong-Woo Kim;In-Ho Choi;Gi-Soo Chung
    • Journal of Wetlands Research
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    • v.25 no.3
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    • pp.176-183
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    • 2023
  • The aim of this paper is to understand the blade number effect on vortex turbine performance in the cylindrical vortex chamber below the free water surface. Using the same blade profile, the performance of gravitational vortex turbine is tested each with 2, 3, 4, 5 and 6 blades installed at the relative vortex height (y/hv) ranging from 0.065 to 0.417. The obtained results indicate that the rotation, voltage, current and power increase in the relative vortex height of 0.065 and 0.111 when increasing the number of blades at flow velocity of less than 0.7 m/s. The average power of the 5-blade turbine is more than others. The performance of the 4-blade turbine with a 130 mm diameter installed near the orifice is higher than that of the same number of blades with a 220 mm diameter in the vortex chamber.

Experimental Study on Synthetic Jet Actuators for Separation Delay (유동 박리를 지연시키기 위한 합성제트 구동기 연구)

  • Kwon, O-Hyun;Byun, Seon-Woo;Roh, Jin-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.1
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    • pp.10-17
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    • 2018
  • The size of commercial wind turbines has been increased. Generally, the pitch control is used to increase the efficiency of wind turbine. However, the pitch control has difficulty to control the local unsteady flow control which makes fatigue load and decreases the efficiency. In this research, Synthetic Jet Actuators(SJAs) are manufactured and applied into a wing section to delay flow separation and increase aerodynamic performances. The SJAs as a kind of zero-net mass-flux actuators injects and removes fluid through a small orifice with a given frequency. The SJA modules actuated by piezoelectric disks are manufactured and the aerodynamic performances are measured according to the shape of the orifice and the velocity of the jets through the wind tunnel test. It is confirmed that as the velocity of the jets are increased using rectangular shape orifice, drag force is decreased and lift force in increased.

Experimental Study on the Performance of a Two-Stage Vortex Turbine with a Free Water Surface (자유수면을 갖는 2단 와류 수차의 성능에 관한 실험적 연구)

  • Jong-Woo Kim;In-Ho Choi;Gi-Soo Chung
    • Journal of Wetlands Research
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    • v.26 no.3
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    • pp.236-244
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    • 2024
  • This research was conducted to determine the performance of a two-stage vortex turbine with a free water surface. The performance of the two-stage runner was studied by varying the flow rate and the position of the runner in the cylindrical vortex chamber. The experimental results showed that the performance parameters such as torque, voltage, current, and rotational speed increased with increasing flow rate. The runner depth ratio has a significant impact on the performance of the two-stage vortex turbine. The highest power generated by the two-stage runner occurred in the range of 0.054 to 0.162 runner depth ratio near the orifice. The power output of the two-stage runner was higher than that of the single runner due to more vortex and blade contact area in the flow range of 7.2 to 7.7 L/s.