• 제목/요약/키워드: Pressure and Rotating

검색결과 650건 처리시간 0.02초

회전 막유화에 의한 알지네이트 미소 구체의 제조 (Preparation of Alginate Microspheres by Rotating Membrane Emulsification)

  • 민경원;염경호
    • 멤브레인
    • /
    • 제31권1호
    • /
    • pp.52-60
    • /
    • 2021
  • SPG (Shirasu porous glass) 원통형 막을 회전 시키는 회전 막유화를 사용하여 칼슘 알지네이트 미소 구체를 제조할 때, 단분산 미소 구체를 제조하기 위한 회전 막유화 공정변수들의 최적 조건을 결정하였다. 회전 막유화의 공정 변수로는 막의 회전 속도, 막간 압력차, 연속상에 대한 분산상의 비율, 알지네이트 농도, 유화제의 농도, 안정제 농도, 가교제 농도 및 막의 세공 크기를 설정하고, 이들 변수로 제조된 알지네이트 미소 구체의 크기와 단분산성에 미치는 영향을 검토하였다. 이 결과 회전 막유화의 공정 변수들 중에서 막모듈의 회전 속도, 유화제의 농도, 가교제의 농도가 증가 할수록 미소 구체의 크기가 감소하였으며, 반면에 연속상에 대한 분산상의 비율, 막간 압력차, 알지네이트 농도가 증가할수록 미소 구체의 크기가 증가하였다. 세공 크기 3.2 ㎛인 SPG막을 사용한 회전 막유화에서 공정변수 조절을 통해 최종적으로 입자 크기가 4.5 ㎛의 단분산 알지네이트 미소 구체의 제조가 가능하였다.

2단 축류팬과 엇회전식 축류팬의 공력 특성에 관한 실험적 연구 (Experimental Study on the Aerodynamic Characteristics of a Two Stage and a Counter-Rotating Axial Flow Fan)

  • 조이상;조진수
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2000년도 춘계학술대회논문집B
    • /
    • pp.541-547
    • /
    • 2000
  • Experiments were done for the comparison of performance and flow characteristics between a two stage axial flow fan and a counter-rotating axial flow fm. The fan performance curves were obtained by the Korean Standard Testing Methods for Turbo Fans and Blowers (KS B 6311). The fan flow characteristics were measured using a five-hole probe by the non-nulling method. Each stage of the two stage axial flow fan used for the present study has an eight bladed rotor and thirteen stator blades. The front and the rear rotor of the counter-rotating axial flow fan have eight blades each and are driven by coaxial counter rotating shafts through a gear box located between the rear rotor and the electric motor. Both of the two axial fan configurations use identical rotor blades and the same operating conditions for the one-to-one comparison of the two. Performance characteristics of the two configurations were obtained and compared by varying the blade setting angles and axial gaps between the blade rows. The passage flow fields between the hub and tip of the fans were measured and analyzed for the particular operating conditions of peak efficiency, minimum and maximum pressure coefficients.

  • PDF

정점을 중심으로 회전하는 강성옹벽에 작용하는 주동토압 (Active Earth Pressure behind Rigid Retaining Wall Rotating about the Top)

  • 백규호;사공명
    • 한국지반공학회논문집
    • /
    • 제20권8호
    • /
    • pp.181-191
    • /
    • 2004
  • 옹벽의 벽면이 거친 경우에 강성옹벽에 작용하는 주동토압의 크기와 분포형태는 뒷채움재의 내부마찰각과 옹벽의 벽면마찰각 뿐만 아니라 뒷채움재에서 발생하는 아칭효과와 파괴면의 형상에도 영향을 받는다. 따라서 강성옹벽에 작용하는 주동토압의 크기와 비선형의 분포형태를 정확히 산정하기 위해서는 토압 산정 시 뒷채움재에서 발생하는 아칭효과와 실제적인 파괴면의 형상을 고려해야 한다. 본 연구에서는 강성옹벽이 옹벽의 정점을 중심으로 회전하는 경우에 대하여 뒷채움재에서의 아칭효과와 실제적인 비선형의 파괴면 형상을 고려함으로써 비선형의 주동토압을 산정할 수 있는 토압산정식을 제안하였다. 그리고 제안식에 대한 정확도를 검증하기 위하여 제안식으로부터 얻어진 예측치들을 기존의 모형시험 결과들과 비교한 결과 제안식은 만족스런 토압 예측치를 제공하는 것으로 나타났다.

배압실의 설계를 통한 상호회전 스크롤 압축기의 전복 모멘트 최소화 (Minimization of Tilting Moment of Co-Rotating Scroll Compressor by Design of Back Pressure Chamber)

  • 구인회;박진무
    • 대한기계학회논문집A
    • /
    • 제24권5호
    • /
    • pp.1305-1313
    • /
    • 2000
  • In a co-rotating scroll compressor, both scrolls rotate on their fixed axes contrary to the conventional orbiting type scroll machine. This implies fixed locations and directions of the gas pressure force and sealing force. Because the tilting moment is mainly caused by interplay between the resultant force of above forces and bearing reaction force, the variation during one cycle is relatively small. Under real operation, this moment is balanced by the restoring moment created by the reaction between the baseplate and thrust bearing or between the scroll tip and baseplate. If these reactions become too large, greater torque is required due to increased friction in addition to the wear of mating parts. Consequently, appropriate study and minimization of tilting moment is important in the design of scroll machines. In this study, taking into account of the small variation of tilting moment during one cycle, we minimize the moment and thrust bearing reaction force by a properly designed back pressure chamber. As a result, for both the driving and driven scrolls, the tilting moment and the reaction force of thrust bearing can be minimized. And the stability is improved for all cases.

Pressure Pulsation Characteristics of a Model Pump-turbine Operating in the S-shaped Region: CFD Simulations

  • Xia, Linsheng;Cheng, Yongguang;Cai, Fang
    • International Journal of Fluid Machinery and Systems
    • /
    • 제10권3호
    • /
    • pp.287-295
    • /
    • 2017
  • The most detrimental pressure pulsations in high-head pump-turbines is caused by the rotor-stator interaction (RSI) between the guide vanes and runner blades. When the pump-turbine operates in the S-shaped region of the characteristic curves, the deteriorative flow structures may significantly strengthen RSI, causing larger pressure pulsations and stronger vibration with an increased risk of mechanical failure. CFD simulations were carried out to analyze the impacts of flow evolution on the pressure pulsations in the S-shaped region of a model pump-turbine. The results show that the reverse flow vortex structures (RFVS) at the runner inlet have regular development and transition patterns when discharge reduces from the best efficiency point (BEP). The RFVS first occur at the hub side, and then shift to the mid-span near the no-load point, which cause the strongest pressure pulsations. The locally distributed RFVS at hub side enhance the local RSI and makes the pressure fluctuations at the corresponding sections stronger than those at the rest sections along the spanwise direction. Under the condition of RFVS at the mid-span, the smaller flow rate make the smaller difference of pressure pulsation amplitudes in the spanwise direction. Moreover, the rotating stall, rotating at 35.7%-62.5% of the runner rotational frequency, make the low frequency components of pressure pulsations distribute unevenly along the circumference in the vaneless space. However, it have little influence on the distributions of high components.

변형 Roebuck 압축기를 이용한 J-T 네온 냉각시스템의 열역학적 설계 (Thermodynamic Design of J-T Neon Refrigeration System Utilizing Modified Roebuck Compression Device)

  • 정제헌;정상권
    • 설비공학논문집
    • /
    • 제15권5호
    • /
    • pp.432-438
    • /
    • 2003
  • This paper describes a modified Roebuck compression device as a potential compression device of a rotating cryogenic refrigeration system in superconducting machine such as generator or motor. The conventional cryogen transfer method from stationary refrigeration system to rotating system can be eliminated by an on-board cryogenic refrigeration system that utilizes well-designed multi-stage modified Roebuck compression device. This paper shows basic thermodynamic analysis of modified Roebuck compression device and its application for compressing neon at 77 K with substantial pressure ratio when the rotor diameter is 0.8 m with rotating speed of 3600 rpm. The device does not require any moving part in rotating frame, but two separate thermal reservoirs to convert thermal energy into mechanical compression work. The high temperature thermal reservoir is atmospheric environment at 300 K and the low temperature thermal reservoir is assumed as a liquid nitrogen bath at 77 K. The concept of the compression device in this paper demonstrates its usefulness of generating high-pressure neon at 77 K for rotating J-T neon refrigeration cycle of superconducting rotor.

편심환내의 회전 유동 (Rotating Flows in Eccentric Cylinders)

  • 심우건
    • 한국생산제조학회지
    • /
    • 제6권3호
    • /
    • pp.9-16
    • /
    • 1997
  • A numerical method based on the spectral collocation method is developed for the steady rotating flows in eccentric annulus. Steady flows between rotating cylinders are of interest on lubrication in large rotating machinery. Steady rotating flow is generated by the rotating inner cylinder with constant angular velocity. The governing equations for laminar flow are simplified from Navier-Stokes equations by neglecting the non-linear convection terms. Integrating the pressure round the rotating cylinder based on the half Sommerfeld method, the load on the cylinder is evaluated with eccentricity. The attitude angle and Sommerfeld variable are calculated from the load. It is found that those values are influenced by the eccentricity. The attitude and Sommerfeld reciprocal are decreased with eccentricity. As expected, the effect of the annular gap ratio on them is negligible.

  • PDF

고 연소압을 받는 디젤엔진 피스톤의 핀-보스 베어링 윤활해석 (Pin-Boss Bearing Lubrication Analysis of a Diesel Engine Piston Receiving High Combustion Pressure)

  • 전상명;하대홍
    • Tribology and Lubricants
    • /
    • 제24권3호
    • /
    • pp.133-139
    • /
    • 2008
  • In recently designed diesel engines, the running conditions for piston pin bearings have become very severe due to combustion pressure and temperature increase. In this paper, it will be investigated the tendency of piston pin rotating motion by calculating the friction coefficient at piston pin bearings, the oil film thickness and the frictional torques induced by hydrodynamic shear stress. Finally, the pressure distributions on the oil film of piston pin bearings will be found by two-dimensional lubrication analysis in order to help the optimum design of the bearings of piston pin. Specially, it is investigated the effects on the film pressure distribution due to the change in maximum combustion pressure.

반복경계조건을 도입한 3차원 유한요소법에 의한 회전탄대의 소성변형 공정해석 (Plastic Deformation Analysis of Rotating Band by Three-Dimensional Finite Element Method Using Recurrent Boundary Condition)

  • 양동열;이영규;박용복;조용찬;한만준
    • 소성∙가공
    • /
    • 제5권2호
    • /
    • pp.122-129
    • /
    • 1996
  • The main objective of the study is to offer some basic information in relation to optimal shape and dimensions of the rotating band through the development of three-dimensional finite element method for metal forming analysis of the rotating band whose primary function is to impart spin to the projectile. The three-dimensional metal forming analysis of the rotating band has perfor-med by using recurrent boundary conditions. Such design factors as the outside diameter the total length and the profile of the rotating band must be considered carefully in order to design an optimal rotating band. Above design factors can be determined from such available analysis results as the deformed shape and the deformation load. of the rotating band and the normal pressure of the rotating band on a projectile shell. The remeshings are needed to carry out plastic deformation analysis with severe deformation through which the complete process analysis gets possible. The results can be utilized effectively in determining the optimal shape and size of the rotating band.

  • PDF

장애물이 없는 3.5' 동시회전 디스크의 유동교란에 관한 수치적 연구 (Numerical Simulation toy Flow Disturbance Between 3.5' Co-rotating Disks Unobstructed in Shroud)

  • 공대위;주원구
    • 정보저장시스템학회:학술대회논문집
    • /
    • 정보저장시스템학회 2005년도 추계학술대회 논문집
    • /
    • pp.242-245
    • /
    • 2005
  • The rotating flow in the space between co-rotating disks is of considerable importance in information storage systems. Hard disk drivers(HDD) in computer are used extensively as data storage capacity. The trend in the computer industry to produce smaller disk drives rotating at higher speed requires an improved understanding of fluid motion in the space between disks. In this study, we have tried LES model for inner-disk flowfield to investigate the flow disturbance and the flow structure driven by co-rotating disks. The boundary pattern between inner region and outer region obtained lobe-shape structure clearly and its number has been validated on experimental data by our previous study. We obtain the spectra of velocity and pressure components with several frequencies. We revealed there are two kinds of disturbances, one is global wave propagation and another is local wave propagation on Ekman boundary layer.

  • PDF