• Title/Summary/Keyword: Torque Flow rate

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Development of a Small Floating Outboard Type Water-Jet Propulsion System (부유식 일체형 소형워터제트 추진시스템 개발)

  • Jeong, Jae Hoon;Yi, Chung Seob;Lee, Chi Woo
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.25 no.1
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    • pp.42-47
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    • 2016
  • This paper presents the development of a floating outboard type of compact water jet propulsion system. The planning case of the water jet system is developed by performing precision processing after manufacturing FRP (Fiber Reinforced Plastics) from plug mold casting. This system is composed of an intake, impeller, diffuser, reverse bucket, and main shaft. In addition, a rebuilt engine was applied through marine engineering. The water jet propulsion system performance was verified to discharge a maximum $0.29m^3/s$ of flow rate and 37 m/s of flow velocity in a test pool on land. A field test was performed by installing the water jet propulsion device on board a ship that was tested off the coast of Korea. The weight of the hull, engine, and other equipment was approximately 1.2 tons, and the sailing speed was a maximum 22 knots at 3,600 rpm.

An Experimental Study of the Performance Characteristics with Four Different Rotor Blade Shapes on a Small Mixed-Type Turbine

  • Cho Soo-Yong;Cho Tae-Hwan;Choi Sang-Kyu
    • Journal of Mechanical Science and Technology
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    • v.19 no.7
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    • pp.1478-1487
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    • 2005
  • A small mixed-type turbine with a diameter of 19.9 mm has been substituted for a rotational part of pencil-type air tool. Usually, a vane-type rotor is applied to the rotational part of the air tool. However, the vane-type rotor has some problems, such as friction, abrasion, and necessity of accurate assembly etc.,. These problems make the life time of the vane-type air tool short, but air tools operated by mixed-type turbines are free of friction and abrasion because the turbine rotor dose not contact with the casing. Moreover, it is assembled easily because of no axis offset. These characteristics are merits for using air tools, but loss of power is inevitable on a non-contacting type rotor due to flow loss, tip clearance loss, and profile loss etc.,. In this study, four different rotors are tested, and their characteristics are investigated by measuring the specific output power. Additionally, optimum nozzle location against the rotor is studied. Output powers are obtained through measured pressure, temperature, torque, rotational speed, and flow rate. The experimental results obtained with four different rotors show that the rotor blade shape greatly influences to the performance, and the optimum nozzle location exists near the mid span of the rotor.

Transient Characteristics of Separately Excited d-c Motor Driven by Thyristor d-c Chopper (Thyristor 직류 Chopper방식으로 구동되는 직류타여자식 전동기의 과도특성해석법)

  • Hee Young Chun
    • 전기의세계
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    • v.21 no.2
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    • pp.9-19
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    • 1972
  • The transient characteristics of separately excited d-c motor driven by thyristor d-c chopper is studied in this paper. The armature controlled system is applied. As a result of theoretrical analysis the following conculsions were drawn: (1) For the transient analysis, it is recognized that the state transition analysis is a more general method and powerful tool than the state equation method or signal flow graph method, although it includes iterative matrix calculations. And the system is dealt with a finite width sampled-data system in the state transition analysis. (2) The transient characteristics of the motor angular velocity and its torque to the sampling duration variation are compared with those due to the amplitude variation of d-c chopper voltage as follows. The attenuation rate of the transient characteristics is equal in both cases, but the initial value of the transient characteristics in former case is greater than in latter case. (3) The roots of characteristics equation of the system lie inside the unit circle of the Z-plane. Therefor the system is stable. Further it is found that as the sampling duration is decreased the relative stability is lessened.

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A Numerical Study on the Effects of Ring Rolling on Materials (링 롤링 공정이 재료에 미치는 영향에 대한 수치해석적 연구)

  • Seo, Youngjin
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.8
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    • pp.22-27
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    • 2020
  • Ring rolling is a type of forging for manufacturing large-diameter rings. Products manufactured by ring rolling are useful in the aerospace industry because of their excellent mechanical properties and high dimensional accuracy. The major components of the ring rolling process are a mandrel and main roll that shape the inside and outside of the ring, an axial roll that shapes the top and bottom of the ring, and a side rolls to position the ring. In this study, a simulation of ring rolling using finite element method (FEM) was performed. DEFORM, a commercial machining analysis program, was used. Based on the simulations, the mandrel feed force required for machining and the drive torque of the main roll were predicted. It was also possible to identify the metal flow caused by machining.

Thermal Analysis of Traction Motor in the High Speed Train with various Flow Rate (고속 전철용 매입형 영구자석 전동기의 풍량에 따른 열해석)

  • Lim, Jae-Won;Yi, Kyung-Pyo;Jung, Hyun-Kyo
    • Proceedings of the KSR Conference
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    • 2010.06a
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    • pp.165-170
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    • 2010
  • Recently, Interior Permanent Magnet Machine(IPM) is widely used for traction motor in the high speed train. Higher efficiency and power density are the superb performance of IPM. Due to the high power density, however, it has lots of heat source which are originated from copper losses and core losses. These heat source can cause the permanent demagnetization in magnet and the loss of torque and power. To prevent the undesirable loss in the traction motor, the accurate loss calculation and the thermal analysis should be preceded. Especially, the end-winding area and permanent magnet area should be examined correctly. In this paper, the electromagnetic fields were examined by finite element method to analyze the electromagnetic properties of IPM and thermal analysis are carried out with pre-calculated losses. To validate the analysis result, the experiment set with forced air cooling system is manufactured.

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Performance Analysis of an Orbiter Air Compressor (오비터 공기 압축기 성능해석)

  • Kim, Hyun-Jin;Cho, Kwang-Myoung;Ko, Won
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.17 no.8
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    • pp.754-763
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    • 2005
  • This paper introduces a new concept compressor in which piston orbits in the cylinder having an annular space formed between two concentric circular walls. In this configuration, two gas pockets are formed with $180^{\circ}$ phase difference: one between the wrap of the orbiting piston and the inner cylinder wall and the other between the piston wrap and the outer cylinder wall. This alternating feature of gas compression and discharge processes yields several advantages such as low torque variation and low gas pulsation. Computer simulation program has been developed to evaluate the compressor performance. The volumetric, adiabatic, and mechanical efficiencies of the orbiter compressor are calculated to be $85.6\%,\;97.2\%,\;and\;95.2\%$, respectively, when it is used as an air compressor.

Energy saving technique of Refrigeration warehouse Cold Water Pump (냉동.냉장창고용 냉수펌프의 에너지절감 기법)

  • Chung, Chung-Byeong;Jeon, Kee-Young;Lee, Sang-Chip;Kim, Dae-Gyun;Lee, Hoon-Goo;Han, Kyung-Hee
    • Proceedings of the Korean Institute of IIIuminating and Electrical Installation Engineers Conference
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    • 2005.11a
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    • pp.409-414
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    • 2005
  • We are interaction refrigeration warehouse cold water pump system and photovoltaic generation system. At this time, a target pressure is able to control in spite of change of the pressure according to pump head and rate of flow of pump. Also, we carry out the vector control of BLDC moor with the maximum torque operation and a high reliability from territory of each operation speed. Therefore, in this paper, we conclude energy saving technique of refrigeration warehouse cold water pump system.

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A Study on the Optimum Design Parameters of the Thermostat for Coolant Temperature Control of an Automotive Engine (자동차용 기관의 냉각수 온도조절을 위한 서머스탯의 최적설계 변수설정에 관한 연구)

  • 박경석;신진식;원종필
    • Transactions of the Korean Society of Automotive Engineers
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    • v.1 no.2
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    • pp.1-16
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    • 1993
  • It is widely recognized that exhaust emissions, fuel economy and engine torque are affected by engine temperature, and logic would suggest that a cooling system offering a better compromise of engine temperature would improve both overall engine performance and economy. Author measured coolant temperature of some parts and flow rate which are necessary to heat transfer in a engine. And Author determined parameters necessary for the optimum design of a thermostat to keep the best engine performance ; determined the optimum operating temperature of electric cooling fan. A summary of this study is followed. 1. Study of the effects of cooling condition to combustion character in a engine. 2. Analyze of heat transfer surrounding engine cylinders. 3. Study of the effects of cooling character to engine heat rejection, determination of the optimum collant temperature for keeping the optimum engine performance and determination of the optimum design of a thermostat for keeping that temperature.

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Analysis of profile ring rolling for rings having V-groove of trapezoidal protrusion by the upper-bound elemental technique (사다리꼴 모양의 돌기나 V형 홈을 갖는 형상 환상압연에 대한 UBET 해석)

  • Hahn, Young-Ho;Yang, Dong-Yol
    • Journal of the Korean Society for Precision Engineering
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    • v.10 no.2
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    • pp.40-47
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    • 1993
  • To diversify the area of application of UBET to the analysis of ring rolling which produces rings having more complex cross-sectional configuration, an element of triangular cross-section has been introduced and the corresponding kinematically admissible velocity field has been derived while considering the material flow between neighboring elements. The theoretical perdictions in roll torque and profile formation show good agreement with the experiments. The effect of process parameters such as feed rate and taper angle of the roll groove has been discussed.

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A Study About the Effect of Supercharging and Intake Charge on Engine Performance in Spark Ignition Gasoline Engine (SI 가솔린 엔진의 과급 및 흡기가 엔진 성능에 미치는 영향에 대한 연구)

  • Kim, Gi-Bok;Jin, Seok-Jun;Kim, Chi-Won;Yoon, Chang-Sik;Han, Sung-Hyun
    • Journal of the Korean Society of Industry Convergence
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    • v.18 no.2
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    • pp.110-118
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    • 2015
  • In this study, it is designed and used the test engine bed which is installed with turbocharger, and in addition to equipped using by oxygen adder. It has been controlled the oxygen volumetric fraction of intake air chrge, and supercharged flow rate into the cylinder of SI 4-stroke engine, and then, has been analyzed engine performance, combustion characteristics, and exhaust emission as analysis parameters. The tested parameters were the oxygen fraction and the variation of engine speed and air-fuel ratio.