• Title/Summary/Keyword: Torque Flow rate

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Design Optimization of Two-Way Pump Casing through Flow Analysis (양방향 펌프의 유동 해석을 통한 펌프 케이싱의 최적설계)

  • Kim, Dong-Hwi;Noh, Yoojeong;Lim, O-Kaung;Choi, Eun-Ho;Choi, Ju Yong
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.31 no.2
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    • pp.79-85
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    • 2018
  • A two-way pump can reduce costs by draining and circulating water out and into the drum of the washing machine using a single motor whereas a conventional one-way pump uses two motors for doing the same function. However, when the water is drained through the drainage outlet in the two-way pump casing, a backward or inhalation flow occurs and the water flows to the circulation outlet. Likewise, when the water is circulated, the backward flow or inhalation makes the water flow to the drainage outlet. In this study, design optimization of the two-way pump casing is performed to maximize its performance while improving backward flow and inhalation occurring inside of the pump casing. For this, design variables of the pump casing that mainly affect the performance of the pump such as flow rate and torque of the motor were selected through the analysis of mean. Using response surface models for the performances, the ratio of the flow rate to the torque was maximized with satisfying the constraints for the back flow and inhalation through design optimization.

Numerical Analysis for the Optimum Design of Shroud Tidal Stream Generation System (쉬라우드 조류 발전 시스템 상부 두께 변화에 따른 유속 변화에 관한 연구)

  • Lee, Uk Jae;Lee, Sang Ho;Han, Seok Jong;Jeong, Shin Taek;Choi, Hyuk Jin;Ko, Dong Hui
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.30 no.3
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    • pp.134-141
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    • 2018
  • Numerical simulations were carried out to investigate the flow velocity changes in the flow field due to the variation in the thickness of the upper part of the shroud tidal power generation system. In this study, it was performed under constant flow velocity condition. In addition, performance analysis of shroud was performed under the same conditions. As the height of the upper part increases, the flow velocity rate gradually increases, and it tends to decrease at a certain height. As a result of analyzing the shape of the blade and the shape of the blade combined with the shroud, the torque of the blade increased due to the increase of the flow rate by the shroud system. It is expected that the shape of the structure obtained by this study and the analysis of the flow velocity distribution in the flow field can provide the data necessary for the development of an efficient shroud tidal power generation system.

A Study on the Parallel Line Pivoted Pad Thrust Bearing (평행선 지지식 추력베어링에 관한 연구)

  • 이경우;김종수;제양규
    • Tribology and Lubricants
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    • v.15 no.1
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    • pp.24-28
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    • 1999
  • This paper describes a new pivoting technique to improve bearing performance in pivoted pad thrust bearings. This new technique adjusts the pivot line in a line pivoted pad thrust bearing to be parallel to the trailing edge of a sector shaped pad. Bearing performance factors such as load carrying capacity, frictional torque and flow rate are numerically investigated for conventional point-pivoted and line-pivoted pads and for the new parallel-line pivoting technique. It is shown that the load carving capacity can be maximized with the new technique.

Numerical Study of the Thermal Effects on the Centrifugal Instability (온도 분포가 원심 불안정성에 미치는 영향에 대한 전산해석적 연구)

  • Hwang Jong-Yeon;Mutabazi Innocent;Lee Sung-Su;Yoon Dong-Hyeog;Yang Kyung-Soo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.30 no.6 s.249
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    • pp.578-586
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    • 2006
  • Numerical simulations are carried out to investigate the thermal effects of the gravitational potential on the centrifugal instability of a Taylor-Couette flow, and to further study the detailed flow fields and flow bifurcations to spiral vortices. The effects of centrifugal potential on the centrifugal instability are also investigated in the current study. Spiral vortices have various types of mode depending on Grashof number and Reynolds number. The correlation of Richardson number with the spiral angle of the spiral vortices shows that the structure of the spiral vortices strongly depends on the Richardson number. The heat transfer rate of the inner cylinder increases with increasing Grashof number. It is also confirmed that the torque required to rotate the inner cylinder increases as Grashof number increases.

Complete Characteristic Curve for a Reactor Coolant Pump (원자로 냉각재 펌프의 완전 특성 곡선)

  • Yoo, IlSu;Park, MuRyong;Hwang, SoonChan;Yoon, EuiSoo
    • The KSFM Journal of Fluid Machinery
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    • v.15 no.5
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    • pp.5-10
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    • 2012
  • An experimental test facility for the complete characteristics of pumps is constructed at KIMM(Korea Institute of Machinery and Materials). All sensors instrumented in test facility for measuring flow rate, pressure, force and moment are in-situ calibrated by primary method. This paper describes the test facility and test technique of the complete characteristics of pumps, together with an experimental test results for a reactor coolant pump which is designed at KIMM for the first time in Korea. The test results for the mixed-flow type pump of $n_s$=1.425 are presented by three curves: constant head, torque, and speed.

Analysis of Fluid Flow Characteristics Around Rolling Element in Ball Bearings (볼 베어링의 구름 요소 주위 유동 특성에 대한 해석)

  • Jo, Jun Hyeon;Kim, Choong Hyun
    • Tribology and Lubricants
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    • v.28 no.6
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    • pp.278-282
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    • 2012
  • Various bearings such as deep-groove ball bearings, angular-contact ball bearings, and roller bearings are used to support the load and to lubricate between the shaft and the housing. The bearings of potential rolling systems in a turbo pump are the deep-groove ball bearings as comparing with the bearings with rolling elements such as cylindrical rollers, tapered cylindrical rollers, and needle rollers. The deep-groove ball bearings consist of rolling elements, an inner raceway, an outer raceway and a retainer that maintain separation and help to lubricate the rolling element that is rotating in the raceways. In the case of water-lubricated ball bearings, however, fluid friction between the ball and raceways is affected by the entry direction of flow, rotation speed, and flow rate. In addition, this friction is the key factor affecting the bearing life cycles and reliability. In this paper, the characteristics of flow conditions corresponding to a deep-groove ball bearing are investigated numerically, with particular focus on the friction distribution on the rolling element, in order to extend the analysis to the area that experiences solid friction. A simple analysis model of fluid flow inside the water-lubricated ball bearing is analyzed with CFD, and the flow characteristics at high rotation speeds are presented.

Flow Visualization in Porous Cylinder with Partial Slots (부분 슬롯을 가진 다공성 실린더의 내부 유동 가시화)

  • Son, Min;Kim, Dohun;Koo, Jaye;Chang, Hongbeen;Kang, Moonjung
    • Journal of Aerospace System Engineering
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    • v.8 no.3
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    • pp.1-5
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    • 2014
  • An inner flow of a porous cylinder with partial slots was visualized to study fluidic phenomena in a solid rocket motor. A high-pressure chamber and an air supply system for high flow rate were used. In order to visualize the inner flow, the smoke generator with a cam-driven pump and heaters and high speed camera were adopted. The results of the cylinder type and the partial slot type were compared. As a result, the injected smoke flow in the partial slot type had circumferential fluctuations unlike the cylinder type. It was found that the circumferential flow induced from the partial slots could be the cause of combustion instability and roll torque.

Effect of Blade Angles on a Micro Axial-Type Turbine Operated in a Low Partial Admission Rate (부분분사 마이크로 축류형터빈에서의 익형각 효과에 관한 연구)

  • Cho, Soo-Yong;Cho, Bong-Soo;Cho, Chong-Hyun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.4
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    • pp.10-18
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    • 2007
  • A tested micro axial-type turbine consists of two stages and its mean radius of rotor flow passage is 8.4 mm. This turbine could be applied to a driver of micro power system, and its rotational speed in the unloaded state reaches to 100,000 RPM. The performance of this system is sensitive depending on the blade angles of the rotor and stator because it is operated in a low partial admission rate, so a performance test is conducted through measuring the specific output power and the net specific output torque with various blade angles on the nozzle, stator and rotor. The experimental results show that the net specific output torque is varied by 15% by changing the rotor blade angle, and the optimal incidence angle is about $10.3^{\circ}$.

Study of Engine Oil Jet System Effect on Engine Friction (Engine Oil Jet System이 Engine Friction에 미치는 영향에 대한 연구)

  • Min, Sun-Ki
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.6
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    • pp.687-692
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    • 2016
  • When turbochargers are applied to engines, the temperature of the engine becomes high, making the cooling of pistons very important. To solve this problem, an oil jet is used. The oil jet provides oil to the underside of piston for cooling. When an oil jet is used, oil pump size-up and oil cooler are needed because of the increased oil flow rate and higher oil temperature. On the other hand, these increase the friction torque of the engine. This study examined how much the friction torque of an engine increases by an oil jet, oil cooler, and oil pump size-up. In addition, the proportions of the friction torque of the engine increased by each part were measured by changing the engine assembly condition. At low speed, the oil pump and oil cooler had a larger effect on the friction torque than the other factors. At high speed, oil cooler had a larger effect than the other factors.

Onset of Inertial Oscillation in a Rotating Flow (회전유동에서의 관성진동 원인규명)

  • Park, Jun-Sang
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2536-2539
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    • 2008
  • A study has been made on how to occur inertial oscillations in a rotating flow. The flow is considered to be induced by differentially-rotating top and bottom disks with infinite radius. The top and bottom disks are assumed to be set in motion over a finite initial start-up time duration from initial solid body rotation ($\Omega$) to each finial state, i.e., the top disk is rotating at the angular velocity (${\Omega}+{\Delta}{\Omega}$) and the bottom disk (${\Omega}-{\Delta}{\Omega}$). The system Reynolds number, which is a reciprocal of conventional Ekman number in rotating flows, is very high so that a boundary layer flow near disks is pronounced. From a strict theoretical analysis, it is clearly found the fact that inertial oscillation in a rotating flow is caused by excessive input of torque during start-up phase. Above finding comes from the following physics of theoretical result: in the case of abrupt start-up within very shorter time-duration than spin-up time scale, the inertial oscillation is magnified but it could be completely depressed in the case of mildly accelerated start-up, i.e., start-up process being established over diffusion time scale.

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