• Title/Summary/Keyword: 공기구동기

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Wind Tunnel Test of 2D Model for Plasma Flow Control using DBD Plasma Actuator (DBD 플라즈마 구동기를 이용한 2차원 모델의 플라즈마 유동제어 풍동시험)

  • Yun, Su-Hwan;Kim, Tae-Gyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.527-528
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    • 2012
  • DBD (Dielectric Barrier Discharge) plasma actuator was designed for aerodynamic drag reduction using plasma flow control, and the drag reduction was measured by wind-tunnel tests using 2D test model. At the zero wind velocity, the plasma flow control had no effect on the drag reduction because the flow separation and surface friction drag were not occurred. At the wind velocity of 2m/s, 9.7% of drag was reduced by the flow separation control. The drag reduction decreased as the wind velocity increased.

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A Study on Tracking Position Control of Pneumatic Actuators Using Neural Network (신경회로망을 이용한 공압구동기의 위치 추종제어에 관한 연구)

  • Gi Heung Choi
    • Journal of the Korean Society of Safety
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    • v.15 no.3
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    • pp.115-123
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    • 2000
  • Pneumatic actuators are widely used in a variety of hazardous working environments. Any process that involves pneumatic actuation is also recognized as "eco-friendly". In most cases, applications of pneumatic actuators require only point-to-point control. In recent years, research efforts have been directed toward achieving precise position tracking control. In this study, a tracking position control method is proposed and experimentally evaluated for a linear positioning system. The positioning system is composed of a pneumatic actuator and a 3-port proportional valve. The proposed controller has an inner pressure control loop and an outer position control loop. A PID controller with feedback linearization is used in the pressure control loop to nullify the nonlinearity arising from the compressibility of the air. The position controller is also a PID controller augmented with the friction compensation by a neural network. Experimental results indicate that the proposed controller significantly improves the tracking performance.rformance.

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A Evaluation Method of Operational Performance for Air-operated Gate Valve (공기구동 게이트밸브의 운전 성능평가 방법에 관한 연구)

  • Kim, Dae-Woong;Park, Sung-Keun;Kang, Shin-Cheul;Kim, Yang-Suk
    • The KSFM Journal of Fluid Machinery
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    • v.12 no.2
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    • pp.31-38
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    • 2009
  • The valve performance has been evaluated from the theoretical equation based on design information such as packing thrust, spring preload and friction coefficient(${\mu}$). The accuracy of those data can be lower than that of vendor's initial design data. Especially, the friction coefficient can be degraded with time than the original condition and the valve performance calculated using the previous friction coefficient can not be available. Accordingly, this paper is describing a new performance evaluation method of valve based on diagnostic test data which are acquired from a site valve tested in static and dynamic conditions. Especially, this paper provides a new method using friction coefficient(${\mu}$) which is derived from the diagnostic test data acquired in the valve's design basis condition.

Experimental Investigation of Performance for Supersonic Impulse Turbine (초음속 충동형 터빈의 성능에 대한 시험적 고찰)

  • Lee, Hang-Gi;Jeong, Eun-Hwan;Kim, Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.561-565
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    • 2009
  • The performance of supersonic impulse turbine was investigated experimentally. Experiment was performed with the compressed air instead of the high temperature burned gas because of the limitation of test facility and danger. As a result of the experiment with the compressed air, the performance in the real gas(burned gas) was predicted by the similarity method. The nozzle area of prototype turbine was calculated based on the real gas. So, it is difficult to satisfy the similarity conditions completely. Two similarity conditions were set and the design point for real gas was existed between two similarity conditions. And, the new turbine test model with calculated nozzle area based on the compressed air was tested. Therefore, similarity point of the new turbine test model was also existed between above two similarity points. It means that the design point for real gas was similar to the test point with the new turbine model.

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A Study of the Transient Characteristics of LRE Startup Using Several Starting Gases (다양한 구동가스를 사용한 액체로켓엔진의 시동특성 연구)

  • Moon, Yoon-Wan;Cho, Won-Kook;Seol, Woo-Seok
    • Aerospace Engineering and Technology
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    • v.7 no.2
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    • pp.170-175
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    • 2008
  • In this study, it was investigated that the characteristics of startup and compatibility using several type hot and cold gases. The characteristics of starting LRE by pyro starter was compared with that by a Helium spinner. The compatibility of pyro gas, a gaseous Helium, Hydrogen+Nitrogen mixture gas, and air was investigated by a simple 1D turbine analysis considered the properties of each gas and turbine efficiency. Most of them were compatible to start up the LRE however air was properly used only for low power mode of turbine.

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A Study of the Transient Characteristics of LRE Startup for Using Several Starting Gases (다양한 구동가스를 사용한 액체로켓엔진의 시동특성 연구)

  • Moo, Yoon-Wan;Kim, Seung-Han;Seol, Woo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.216-220
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    • 2006
  • In this study, it was investigated that the characteristics of startup and compatibility using several type hot and cold gases. The characteristics of starting LRE by pyro starter was compared with that by a He spinner. The compatibility of pyre gas, a gaseous He, H2+N2 mixture gas, and air was investigated by a simple 1D turbine analysis considered the properties of each gases and turbine efficiency. Most of them were compatible to start up the LRE but air was properly used only when the turbine was low power mode.

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The Intact Evaluation of High Pressure Control Valve Trim Parts (고차압 제어밸브 트림부 분석 및 개선방안 검토)

  • Jang, H.;Yoon, I.S.;Kim, Y.B.
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.581-584
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    • 2008
  • At the inlet and outlet differential pressure and The fluid velocity over 32m/s are damaged (Plug, sheet ring, trim) About reduction trim parts of the control valve. AOV of the differential pressure 1,500psi become often the damage in the nuclear power plant. Damages of AOV studied CFD analysis and improvement program. Multi-stage trim designs which decrease a fluid kinetic energy are demanded and AOV parts are demanded case hardening and material change.

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Development of Diagnosis System for Diaphragm Operated Globe Valve (다이어프램 구동형 글로브 밸브의 진단장비 개발)

  • Yang, Sang-Min;Shin, Sung-Ky
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.31 no.9
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    • pp.975-980
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    • 2007
  • Air-operated valve is one of principal valves that are used to control fluid flow in nuclear power plants. A periodic diagnosis for the safety of power plants is necessary. But there are many difficulties such as economic loss caused by income of high cost devices and a matter hard to deal with users. In this study, we developed the diagnostic system that users of power plants are easy to handle. The diagnostic system is composed of database module, diagnosis test module and analysis module.