• Title/Summary/Keyword: Design Pressure

Search Result 7,675, Processing Time 0.035 seconds

3-Dimensional Design Failure Curve of Marine Silty Sand under Different Confining Pressures Subjected to Cyclic Loading (반복하중을 받는 해양 실트질 모래의 구속압에 따른 3차원 설계파괴곡선 산정)

  • Suwon, Son;Jongchan, Yoon;Jinman, Kim
    • Journal of the Korean GEO-environmental Society
    • /
    • v.23 no.12
    • /
    • pp.25-31
    • /
    • 2022
  • Unlike structures installed on land, the structures installed on the offshore ground must consider long-term cyclic loads such as wave loads, wind loads and tidal loads at sea. Therefore, it is important to analyze the behavior of the ground subjected to long-term cyclic loads in order to design a structure installed on the ocean ground. In this paper, cyclic simple shear tests were performed to analyze the ground behavior for long-term cyclic loads according to the confining pressure, and a three-dimensional design failure curve was prepared that can easily check the failure characteristics according to the confining pressure. As a result of the analysis, it was confirmed that the position of the design failure curve is different depending on the confining pressure even under the same conditions of the cyclic shear stress ratio and the average shear stress ratio, and the number of cyclic loads reaching failure is affected by the confining pressure. From the created 3-D design failure curve under different confining pressure, the tendency and approximate value of the design failure curve according to the confining pressure can be estimated.

Design Program of Low Noise Centrifugal Fans (저소음 원심형 홴의 설계 프로그램)

  • 박준철;손정민;김기황;이승배
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 2001.11a
    • /
    • pp.529-535
    • /
    • 2001
  • A centrifugal fan design code was developed and packaged together with iDesignFan/sup TM/ as new models. This code generate centrifugal forward curved and backward curved bladed impeller optimally. It also predicts the aerodynamic performance and the overall sound pressure level of the rotating fan by assuming steady blade loading. The overall sound pressure level is used as an input parameter from the third loop of the designing process to acquire the most silent fan for the given aerodynamic performance parameters. With this kind of inverse design concept used in the code, the period of designing a fan is significantly shortened. A centrifugal fan design code, developed in this study and included in iDesignFan/sup TM/, predicts the aerodynamic performance such as design flow rate and static pressure. The aerodynamic performance in the design and off-design conditions is calculated by using the mean line analysis. For the steady loading calculation, the lift force distribution in a blade is used.

  • PDF

Determination of Valve Gate Open Timing for Minimizing Injection Pressure of an Automotive Instrument Panel (자동차용 인스트루먼트 패널의 사출압력 최소화를 위한 밸브 게이트 열림 시점 결정)

  • Cho, Sung-Bin;Park, Chang-Hyun;Pyo, Byung-Gi;Choi, Dong-Hoon
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.20 no.4
    • /
    • pp.46-51
    • /
    • 2012
  • Injection pressure, an important factor in filling process, should be minimized to enhance injection molding quality. Injection pressure can be controlled by valve gate open timing. In this work, we decided the valve gate open timing to minimize the injection pressure. To solve this design problem, we integrated MAPS-3D (Mold Analysis and Plastic Solution-3Dimension), a commercial injection molding CAE tool, to PIAnO (Process Integration, Automation and Optimization), a commercial PIDO (Process Integration, and Design Optimization) tool using the file parsing method. In order to reduce computational cost, we performed an approximate optimization using meta-models that replaced expensive computer simulations. At first, we carried out DOE (Design of Experiments) using OLHD (Optimal Latin Hypercube Design) available in PIAnO. Then, we built Kriging models using the simulation results at the sampling points. Finally, we used micro GA (Genetic Algorithm) available in PIAnO. Using the proposed design approach, the injection pressure has been reduced by 13.7% compared to the initial one. This design result clearly shows the validity of the proposed design approach.

Optimal Design of the Safety Valve by Response Surface Method (반응표면법을 이용한 안전밸브의 최적화)

  • Lee, Sang-Woo;Shin, Dae-Young;Byun, Cheol-Woong
    • Journal of the Computational Structural Engineering Institute of Korea
    • /
    • v.20 no.5
    • /
    • pp.551-556
    • /
    • 2007
  • High pressure storage of the agent gas in fire suppression system was composed of tank, main valve and safety valve, which prevents the fracture of the high pressure storage. The safety valve has circular thin plate as fracture plate that was destroyed over fracture pressure. When inner pressure of the storage is reached the fracture pressure, the safety valve discharges gas and degrades simultaneously the inner pressure of the storage. There are design variables such as flow path diameter, inner diameter of the plastic packing ring, thickness of plate and fillet radius. In this variables, thickness of plate is set to be a value of 0.2mm. The main effect of variables on the inner pressure, has been decided using factorial design and statistical analysis. Therefore, the relation of variables are expressed by regression equation. It is disclosed results that the difference of fracture pressures between the equation and experiment has $2{\sim}5%$. Finally, using response surface method, the optimal design of the safety valve could be decided with safety pressure of 25MPa, where the fracture occurs on circular thin plate.

Design of Ratio Control Valve for a Pressure Control Type CVT Using P-Line (P-라인을 이용한 압력제어방식 CVT 변속비제어밸브 설계)

  • 류완식;이용준;김현수
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.12 no.3
    • /
    • pp.145-151
    • /
    • 2004
  • In this paper, a pressure control type ratio control valve(RCV) is designed for a metal belt CVT. Steady state and transient characteristics of the pressure control CVT are investigated by simulations and experiments. In addition, P-line is proposed to predict the shift performance. It is found that the bigger the pressure margin, the faster the shift response. It is expected that the P-line can be used in design of the RCV to meet the desired shift performance.

Design of the Port Plate for Gerotor Pumps (제로터 펌프의 측판 설계)

  • Nam, Yun-Joo;Park, Myeong-Kwan
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.28 no.4
    • /
    • pp.406-414
    • /
    • 2004
  • In Gerotor pump, the pressure pulsations which occur due to the pump geometry result in vibration and noise of pump elements as well as cavitation in hydraulic system when the chambers of gerotor enter the delivery port and leave the suction port. Therefore it is important to study on the pressure pulsations before design and analysis of characteristics in Gerotor pump. In this paper, to reduce the unnecessary pressure pulsations, the port plate of Gerotor pump is designed based on the notch of the vane pumps and the relief grove of the piston pumps. The theoretical analysis of the pressure pulsations is performed in consideration of design parameters of the port plate which include each port positions and groove width and operating conditions which include rotational velocity and delivery pressure.

Unsteady Flow Analysis of Liquid Hydrazine Propellant for the Design Parameter Derivation of Satellite Propulsion System (인공위성 추진기관 설계변수 도출을 위한 Hydrazine 액체 추진제의 비정상 유동해석)

  • Choi, Jin-Chul;Kim, Jeong-Soo
    • Proceedings of the KSME Conference
    • /
    • 2000.11b
    • /
    • pp.497-501
    • /
    • 2000
  • One of the way to derive design parameters of the fuel feeding system in satellite is to analyze unsteady flow of liquid propellant (hydrazine) in the propulsion system. During steady thruster firing the flow rate is constant: if a thruster valve is abruptly shut down among a sets of thrusters, pressure spikes much higher than the initial tank pressure occur. This renders the fuel flow unsteady, and the fluid pressure and flow rate to oscillate. If the pressure spikes are high enough, there are possibilities that propellant explosively decomposes, thruster valves are damaged, and adiabatic detonation of the hydrazine propellant is potentially incurred. Reflected shockwaves could also affect the calibration and operation of the pressure transducers. These necessitate the analysis of unsteady flow in the propulsion system design, and the calculation results obtained through some governing parameter variation are presented in this work.

  • PDF

A structural analysis of deep depth injection mold to investigate the cause of crack (깊이가 깊은 사출금형의 크랙 원인 파악을 위한 강도해석)

  • Choi, S.H.;Lyu, M.Y.;Kim, D.W.;Kim, S.Y.;Shin, K.S.;Kim, K.Y.
    • Proceedings of the Korean Society for Technology of Plasticity Conference
    • /
    • 2008.05a
    • /
    • pp.297-300
    • /
    • 2008
  • High pressure is involved during injection molding operation specially packing phase. Cracks in the mold are often occurred by high cavity pressure. In this study, structural analysis of mold has been performed using commercial softwares, Abaqus and Ansys, to investigate cause of crack in the injection mold. Structural analysis contains four cases: stress distribution according to the cavity pressure, stress concentration according to the boundary conditions, stress concentration for inter-locking design of mold, and stress concentration for distributed cavity pressure. Through this study it was observed that the locations of stress concentrations were coincident with locations of crack. Robust mold design is being required to withstand high cavity pressure.

  • PDF

An Analysis of the Dynamic Characteristics of a Spool Type Pressure Control Valve (스풀형 압력제어밸브의 동특성 해석)

  • Moon, Kang Hyun;Huh, Jun Young
    • Journal of Drive and Control
    • /
    • v.15 no.4
    • /
    • pp.61-66
    • /
    • 2018
  • Almost every hydraulic system is equipped with a pressure relief valve, to maintain working pressure of the system at a pre-determined level. Thus, dynamic characteristics of such a relief valve, in conjunction with other hydraulic components, are important in designing the hydraulic control system. The single stage pressure relief valve is dynamically undesirable, due to relatively low viscous damping, that causes high frequency oscillations. This problem is overcome by introducing orifices in the inner pilot line, and drain line. In this study, for the single stage spool type pressure relief valve, the system equations were derived through an adequate linearisation and several simplifications were made, to use the transfer function formulation technique. All coefficients were evaluated and used, to make some results by using Matlab software. Results of analysis are compared with experimental results. In this study, parameters affecting stability of valve design are determined and suggested relative to the design.

Development of Design Method of Compression(SSC) Anchor (압축헝 앵커의 설계법 개발)

  • 임종철;홍석우;이태형;이외득
    • Journal of the Korean Geotechnical Society
    • /
    • v.15 no.1
    • /
    • pp.63-78
    • /
    • 1999
  • For the design of compression anchor, three things should be considered. The first is a resistance force by skin friction, the second is a tension strength of tendon, and the third is a compressive strength of grout. Especially, compressive strength of grout is the most important design parameter of compression anchor. When compression anchor is pulled out from the ground, the compressive strength of grout increases by confining pressure of ground($\sigma_{tg$). Here, $\sigma_{tg$ is the confining pressure which is produced by earth pressure at rest and by lateral expansion of grout. We call this phenomenon of increase of confining pressure "poisson effect". In this paper, the design method of compression anchor called SSC anchor and the computer program for the design are developed through compression tests of anchor body grout.ody grout.

  • PDF