• 한국항공우주학회지
• /
• 제39권7호
• /
• pp.634-642
• /
• 2011

비행조종작동기 제어용 파일럿 밸브의 내부 유동 및 응답 특성을 분석하기 위해 캐비테이션 모델과 격자 이동 기법을 사용하여 정상/비정상 유동의 수치 해석을 수행하였다. 작동 온도와 시간에 따른 밸브 내부 유동을 분석한 결과, 일정 온도 이상에서 밸브 특성이 안정되는 현상을 발견하였고 캐비테이션이 밸브 성능에 미치는 영향성을 파악하였다. 밸브 내부 압력과 응답 특성을 분석하였으며 비정상 유동이 발달하여 정상 유동 특성과 일치하는 것을 확인하였다.

• 드라이브 ㆍ 컨트롤
• /
• 제15권4호
• /
• pp.11-16
• /
• 2018

Pilot operated control valve for $CO_2$ refrigerant is a valve that can perform various functions according to the user's intention by replacing pilot units, widely used for flow rate, pressure, and temperature control of refrigeration and air conditioning systems. In addition, $CO_2$ refrigerant, that requires high pressure and low critical temperature, can be installed and used in all positions of the refrigeration system, regardless of high or low pressure. In this paper, response characteristics are modeled and analyzed based on behavior of the main piston of the pilot-operated control valve. Although various factors influence operation of the main piston, this paper analyzes the effect of equilibrium pressure depending on valve installation position and application, and inlet and outlet orifice size of the load pressure feedback chamber to determine feedback characteristics of the main piston. As a result, it was possible to quantitatively analyze the effect of change in equilibrium and load pressure feedback chamber flow path size on the change in main piston dynamic and static characteristics.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2010년도 추계학술대회 논문집
• /
• pp.775-776
• /
• 2010

• 항공우주기술
• /
• 제13권2호
• /
• pp.160-166
• /
• 2014

액체로켓 엔진용 개폐밸브는 파일럿 공압으로 포핏을 열고 스프링 힘에 의해 닫음으로써 로켓엔진의 추진제 유량을 제어한다. 현재 개발 중인 엔진용 개폐밸브는 다이어프램 액추에이터에서 압력을 제거하면 닫히도록 설계되어 있다. 다이어프램을 설계하고 개발하기 위해 밸브가 열리고 닫히는 특성에 따라 수명을 분석할 필요가 있다. 밸브가 닫히기 시작하는 시점의 작동 유체의 압력을 결정하고, 포핏이 열리는 시점의 압력을 결정되어 힘평형이 설계되어 있다. 수명시험은 상온 유동에서 다이어프램부의 크랙에 의한 누설은 용접 부위에서 발생했다. 다이어프램 액추에이터의 작동 수명은 헬륨 파일럿 압력의 22 MPa 시험에서 61회이다.

• 드라이브 ㆍ 컨트롤
• /
• 제15권2호
• /
• pp.38-45
• /
• 2018

In this study, the theory of fluid mechanics and dynamics is used to build a mathematical model for a three-stage flow control valve. The significance of the study is that the mathematical model can easily be used to study the effect of different design parameters on the performance of the valve. The geometry of the valve and the properties of the fluid were used in this study to determine the variation in the performance of the valve when varying the magnetic force on the pilot spool. While a linearization technique is not used to solve the developed model, the solution of the mathematical model is found in the time domain by simulation of the equations using a software package. The results indicate that if the developed mathematical model is solved for the different values of magnetic force, the valve behaves linearly; the valve is thus called the proportional flow control valve.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2003년도 춘계학술대회 논문집
• /
• pp.1006-1011
• /
• 2003

In this study, a novel systematic design procedure by Genetic Algorithm of a two stage relief valve is proposed. First of all, a mathematical model describing the dynamics of a balanced piston type relief valve has been derived. Governing equations such as dynamic equations for the main spool and the pilot spool and flow equations for each orifice are established. The mathematical model is verified by comparing the results of simulation with that of experiments. Furthermore, influences of the parameters on the dynamic characteristics of a relief valve have been investigated by simulation of the proposed model. Major design parameters on the valve response are determined, which affect the system response significantly. And then, using the determined parameters, the optimization of the two stage relief valve by Genetic Algorithm, which is a random search algorithm can find the global optimum without converging local optimum, is performed. The optimal design process of a two stage relief valve is presented to determine the major design parameters. Fitness function reflects the changing pressure according to parameters. It is shown that the genetic algorithms satisfactorily optimized the major design parameters of the two stage relief valve.

• 한국신뢰성학회지:신뢰성응용연구
• /
• 제14권4호
• /
• pp.230-235
• /
• 2014

The failure modes of pneumatic directional control valves include leakage, wear of the spool seal, and sticking of the spool. Among them, the main failure mode of the valve is leakage. The leakage is caused by the wear of the spool seal. However, due to the characteristics of the seal material, the leakage rate is fluctuated a lot rather than constantly increased over time. If life analysis is performed using the first time data of leakage failure, predicted life cycles can be different from the real life cycles. This paper predicts life cycles of the pilot pneumatic directional control valve based on the three point moving average which considers the average of the fluctuating leakage rate.

• 항공우주기술
• /
• 제11권1호
• /
• pp.84-90
• /
• 2012

연소기용 연료개폐밸브는 파일롯 공압으로 포핏을 열고 스프링 힘에 의해 닫음으로써 로켓엔진의 연료 유량을 제어한다. 현재 개발 중인 연소기 연료개폐밸브는 액추에이터에서 압력이 제거되더라도 유로부에 해당 압력이 존재한다면 스스로 열림을 유지하는 방식으로 설계되어 있다. 밸브의 성능을 평가하기 위해 밸브가 열리고 닫히는 특성에 따라 힘 평형 상태를 분석할 필요가 있다. 이를 위하여 밸브의 포핏이 열리기 위한 파일롯 압력과 닫히기 위한 유로부 압력을 힘 평형에 의해 조절되도록 설계하였다. 또한, 상용 소프트웨어인 Fluent CFD 해석을 통해 밸브의 고유유량계수를 구해보았다. 예측과 해석을 통해 획득된 결과들은 실험 결과와 비교하였다.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2003년도 춘계학술대회 논문집
• /
• pp.828-831
• /
• 2003

The benefits of the pneumatic valve with piezoelectric element are faster response times, low energy consumption, and the ability to be used in hazardous environments and field bus systems. In this paper, PZT actuator, 2 and 3 stages pneumatic valve were designed and manufactured. Also. characteristics of the pneumatic valve with piezoelectric element were tested with a testing system. It is confirmed that the PZT actuator is useful one for controlling the direction of pilot valve.

• 유공압시스템학회논문집
• /
• 제8권4호
• /
• pp.9-16
• /
• 2011

Because of the increasing demand on the high precision and high response of a machinery, proportional control valves are widely adopted at various application fields. This paper studies on the static and dynamic characteristics of a pilot proportional pressure control valve. An experimental apparatus including hydraulic pump, variable speed inverter, pressure and flow sensors and data aquisition system was set up. And various experiments such as P-Q-V curves, step responses due to input voltage and flow rate, hysteresis, frequency response of the proportional valve was carried out and the results are discussed.