• 제목/요약/키워드: Inlet Valve

검색결과 236건 처리시간 0.019초

LNG 연료 추진 선박용 크랭크실 릴리프 밸브 화염방지기의 유동해석 및 폭발시험 (CFD Analysis and Explosion Test of a Crankcase Relief Valve Flame Arrester for LNG-fuelled Ships)

  • 이효렬;안중환;김동건;안병훈;김화영
    • 한국생산제조학회지
    • /
    • 제25권3호
    • /
    • pp.171-176
    • /
    • 2016
  • Growing concerns about air pollution have led to increased demand for liquefied natural gas (LNG)-fuelled ships that have crankcases equipped with explosion relief valves to relieve excessive crankcase pressures and stop the flames emitted from the crankcase. The results of a computational fluid dynamics (CFD)-based feasibility analysis of the crankcase relief valve flame arrester design conducted using ANSYS CFX V14 showed that the inlet and outlet relief valve temperatures differed by $350-700^{\circ}C$. An explosion test was performed based on European standard EN14797 to evaluate the flame transmission and mechanical integrity of the valve. No flame transmission from the pressure vessel to the exterior was detected, and the mechanical integrity of the valve was confirmed. Thus, the relief valve components were found to be safe from the viewpoint of fracture.

이동식 수소 충전 장비용 수소 밸브의 유체 온도 변화에 따른 유동 특성의 수치해석적 연구 (A Numerical Analysis Study of Hydrogen Valve to Flow Characteristics by Fluid Temperature Variation for Mobile Charging Equipment)

  • 권준영;오승준;최정주;김용기
    • 한국수소및신에너지학회논문집
    • /
    • 제33권6호
    • /
    • pp.769-775
    • /
    • 2022
  • Global efforts to reduce carbon emissions have focused attention on the development of hydrogen energy and the development of various hydrogen mobility requires mobile hydrogen charging stations. In this study, the flow characteristics of the flow control hydrogen valve for mobile hydrogen charging equipment were studied according to the temperature change of hydrogen gas. The inlet pressure was 100 MPa, the outlet pressure to 70 MPa, and temperature condition was set -40℃ to 85℃. As a result, the difference in the valve flow coefficient, which determines the capacity of the valve, showed a difference within 5% depending on the temperature.

ABS 유압 장치의 유충 현상에 관한 연구 (A Study on the Pressure Surge of ABS Hydraulic System)

  • 김병우;송창섭
    • 한국자동차공학회논문집
    • /
    • 제9권5호
    • /
    • pp.140-147
    • /
    • 2001
  • The solenoid valve in ABS hydraulics, modulator is a two directional on-off valve and is controlled by around 100Hz high speed pulse width modulation. When the inlet valve is switched from open state to closed state, there are braking force degration, noise and vibration due to pressure surge phenomena in the hydraulic line and wheel cylinder. In this study, identifies pressure surge phenomenon in the braking process of a ABS, and investigates the way to reduce the phenomenon. For the purpose theoretical analysis on the pressure surge in the closed state hydraulic line, characteristic curve method based on wave equation was utilized. During this analysis, we could find pressure surge characteristics change due to hydraulic line change and PWM control conditions. In conclusion, by using the results of this study for the pressure surge prediction and reduction method, we could expect braking performance enhancement in Anti-Lock Braking System.

  • PDF

4밸브기관의 압축상사점 부근의 난류특성에 관한 수치해석적 연구 (A Numerical Study on the Turbulent Flow Characteristics Near Compression TDC is Four-Valve-Per-Cylinder Engine)

  • 김철수;최영돈
    • 한국자동차공학회논문집
    • /
    • 제1권1호
    • /
    • pp.1-13
    • /
    • 1993
  • The three-dimensional numerical analysis for in-cylinder flow of four-valve engine without intake port has been successfully computed. These computations have been performed using technique of the general coordinate transformation based on the finite-volume method and body-fitted non-orthogenal grids using staggered control volume and covariant variable as dependent one. Computations are started at intake valve opening and are carried through top-dead-center of compression. A k-$\varepsilon$model is used to represent turbulent transport of momentum. The principal study is the evolution of interaction between mean flow and turbulence and of the role of swirl and tumble in generating near TDC turbulence. Results for three different inlet flow configuration are presented. From these results, complex flow pattern may be effective for promoting combustion in spark-ignition engines and kinetic energy of mean flow near TDC is well converted into turbulent kinetic energy.

  • PDF

개폐 각도에 따른 볼 밸브에서의 유동 해석에 관한 연구 (A Study on Flow Analysis at Ball Valve according to Opening and Shutting Angle)

  • 조재웅;한문식
    • 한국기계가공학회지
    • /
    • 제10권2호
    • /
    • pp.46-51
    • /
    • 2011
  • This study result is obtained by flow analysis according to opening and shutting angle of ball valve. As opening and shutting angle becomes larger, vortex flow becomes smaller and flow rate becomes increased. And the pressure drop is shown to be smaller at the inlet and outlet of ball. As this angle becomes larger, mass flow rate becomes increased. Its rate becomes increased abruptly in case of opening and shutting angle at more than $60^{\circ}$.This analysis result can be applied usefully with no leak at pipe system field by the optimum control of mass flow rate according to opening and shutting of ball valve.

250마력 급 차량용 터보차저 서지현상에 대한 실험적 연구 (Experimental Study of Compressor Surge for 250-hp Class Vehicular Turbocharger)

  • 이형창;한재영;이명희;임석연;유상석
    • 대한기계학회논문집B
    • /
    • 제39권1호
    • /
    • pp.89-95
    • /
    • 2015
  • 터보압축기의 서지는 압축기의 불안정 운전영역으로 주로 소음과 맥동을 유발하며 수회 지속될시 압축기 시스템 전반에 걸쳐 막대한 피해를 입힌다. 압축기의 안전한 운전을 위해서는 서지현상에 대한 특성파악과 제어전략 수립이 중요하다. 서지현상의 제어는 주로 압축가스의 통과유동량 증대, 필요한 헤드 저감, 압축기 회전수 감속, 가스의 바이패스를 통하여 이루어진다. 본 연구에서는 차량용 터보차저에 서지를 유발했을 때 각 운전 구간별 발생되는 압력변동 특성을 연구하고자 한다. 서지 특성 확인을 위한 파라미터는 압축기 입구 유량과 출구 유량, 관경, 회전수 등으로 선정하였다. 입구단과 출구단 유량을 조절하여 서지 압력 변동을 조사한 결과, 출구단 보다는 입구단 유량의 급격한 변화가 서지와 압축기 내구에 더 영향이 크다는 것을 확인하였다.

선박용 체크밸브의 최적설계에 관한 연구 (A Study on the Optimization Design of Check Valve for Marine Use)

  • 이춘태
    • 동력기계공학회지
    • /
    • 제21권6호
    • /
    • pp.56-61
    • /
    • 2017
  • The check valves are mechanical valves that permit fluids to flow in only one direction, preventing flow from reversing. It is classified as one way directional valves. There are various types of check valves that used in a marine application. A lift type check valve uses the disc to open and close the passage of fluid. The disc lift up from seat as pressure below the disc increases, while drop in pressure on the inlet side or a build up of pressure on the outlet side causes the valve to close. An important concept in check valves is the cracking pressure which is the minimum upstream pressure at which the valve will operate. On the other hand, optimization is a process of finding the best set of parameters to reach a goal while not violating certain constraints. The AMESim software provides NLPQL(Nonlinear Programming by Quadratic Lagrangian) and genetic algorithm(GA) for optimization. NLPQL is the implementation of a SQP(sequential quadratic programming) algorithm. SQP is a standard method, based on the use of a gradient of objective functions and constraints to solve a non-linear optimization problem. A characteristic of the NLPQL is that it stops as soon as it finds a local minimum. Thus, the simulation results may be highly dependent on the starting point which user give to the algorithm. In this paper, we carried out optimization design of the check valve with NLPQL algorithm.

CO2냉매용 제어밸브의 응답 특성 (Transient Response Analysis of a Control Valve for CO2 Refrigerant)

  • 김보현;장지성
    • 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.

FCEV 충전 시스템 체크밸브의 수소 유입 극한 온도 조건에 따른 유동 성능 인자 분석 (Analysis of Flow Performance Factors According to Extreme Temperature Conditions of Hydrogen Inflow of FCEV Charging System Check Valve)

  • 오승훈;서현규
    • 한국수소및신에너지학회논문집
    • /
    • 제34권5호
    • /
    • pp.514-525
    • /
    • 2023
  • This study conducted numerical simulations with the purpose of analyzing the impact of variations in outlet pressure conditions under extreme temperature conditions on the fluid dynamics and performance of a check valve utilized in hydrogen refueling systems. Under the extreme temperature conditions, changes in outlet pressure conditions of the check valve were investigated to analyze velocity distributions, pressure distributions, and temperature distributions in the operational and connection regions. The analysis results indicated that changes in outlet pressure had a significant influence on the internal temperature variation of the check valve. Furthermore, due to density variations in the connection region caused by the cooling effect of excessively cooled hydrogen, a bias in the primary flow direction towards the lower part of the valve outlet was observed in the outlet area. Through a comparison of the results of the valve's inherent flow performance, represented by the flow coefficient, it was observed that when the pressure difference between the inlet and outlet was below 0.37 MPa, sufficient flow was not ensured.

전투기 흡입구 해머쇼크 설계압력에 대한 확률론적 접근법 (Probabilistic Approach for Fighter Inlet Hammershock Design Pressure)

  • 배효길;이훈식;김윤미;정인면;이상효;조대영
    • 항공우주시스템공학회지
    • /
    • 제13권5호
    • /
    • pp.72-78
    • /
    • 2019
  • 전투기 흡입구 덕트 구조물 설계에 중요한 하중조건으로 흡입구 해머쇼크 조건이 있다. 엔진 압축기 내부유동의 갑작스런 감소에 의하여 큰 압력의 해머쇼크가 발생하게 된다. 압축충격파인 흡입구 해머쇼크 해석을 위한 전통적인 방법은 극단적인 조건들의 조합을(최대 속도, 해수면, 저온 대기) 이용하였지만, 90년대 이후 확률론적 방법을 통해 적절한 해머쇼크 설계압력을 제시한 논문들이 발표되었다. 이를 참고로 본 연구는 한국공군의 비행운용데이터를 활용하여 흡입구 해머쇼크 압력을 확률론적으로 접근하였고, 이를 통해 전통적인 방법 대비 약 30 % 감소된, 흡입구 설계용 해머쇼크 압력을 해석하였다.