• Title/Summary/Keyword: 축동력

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Molecular Dynamics Simulation to compare Turbine Rotational Power based on Nozzle Shapes (노즐 형상에 따른 터빈 축동력 형성 비교를 위한 분자동력학 시뮬레이션)

  • Kim, Su-Hee
    • The Journal of the Korea institute of electronic communication sciences
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    • v.14 no.2
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    • pp.425-432
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    • 2019
  • Molecular dynamics simulations were carried out to analyze the impact on turbine rotational power based on nozzle shapes. y varying two parameters, turbine rotational velocity w and initial velocities ($V_x,V_y$) for generating molecules, turbine rotation velocities of molecules in turbine entrance arc region and turbine exit arc region were calculated. Average momentums were calculated over two regions, respectively and the differences (AMD) were compared and analyzed. The optimal range of w values to enhance AMD was investigated over 4 different nozzle shapes used, and an excellent nozzle shape to achieve more turbine rotational power was drawn.

카메라를 이용한 선박의 축동력 계측에 관한 연구

  • Jeong, Jeong-Sun;Kim, Yeong-Bok;Choe, Myeong-Su;Choe, Se-Cheol
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2010.04a
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    • pp.297-298
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    • 2010
  • 선박 추진축계의 동력을 계측하기 위해서는 일반적으로 스트레인 게이지를 이용한 방법이 널리 사용된다. 이러한 방법의 경우 스트레인 게이지 외에도 많은 부품들을 축에 장착해야 하며 전원을 공급하기 위해 별도의 장치를 필요로 하는 등 설치 시 매우 복잡하고 섬세한 작업이 요구된다, 뿐만 아니라 계측신호를 취득하고 분석하기 위해서도 고도의 전문성이 요구되기 때문에 운전 중의 실시간 계측을 통한 모니터링 목적이 아니라 시험 및 검증을 위해 사용될 뿐이다. 따라서 본 연구에서는 이와 같은 단점들을 보완하면서도 추진축계의 동력을 비교적 용이하게 계측하기 위한 새로운 방법을 제안하고자 한다. 본 연구에서 제안하는 계측기법은 카메라를 사용하여 축동력을 계측하는 방법으로 실험결과를 통해 유효성을 확인하였으며 항해 중 실시간 모니터링이 가능한 감시 시스템을 구축할 수 있는 새로운 계측기술이라 할 수 있다.

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Effect of Fluid Viscosity on Centrifugal Pump Performance (유체의 점성이 원심펌프 성능에 미치는 영향)

  • Kim, Noh-Hyeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.6
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    • pp.599-605
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    • 2013
  • The characteristics of centrifugal pump performance according to fluid viscosity change were studied experimentally. A small volute pump with low specific speed was tested by changing the viscosity of an aqueous solution of sugar and glycerin, which is considered a Newtonian fluid. After finishing the test, the total head, shaft horsepower, and pump efficiency were compared with those of a water pump. The results are summarized as follows: (1) when the fluid viscosity is increased, the shut-off head shows very little change but the total head decreases gradually as the flow increases, and this makes the H-Q curve leaning rapidly, and (2) when the fluid viscosity is increased, the shaft horsepower shows very little change at the shutoff condition; however, the shaft horsepower increases more rapidly with an increase in the flow and viscosity.

A Study on the Performance Prediction of Automotive Water Pump with Double Discharge Single Suction (자동차용 양토출 단흡입 워터펌프의 성능 예측에 관한 연구)

  • 허형석;박경석;이기수;원종필
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.3
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    • pp.27-36
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    • 2004
  • A Numerical analysis has been used to predict the performance in the automotive water pump with double discharge single suction. The influence of parameters such as coolant flow rate, rotational speed, ratio of blade height and clearance has been investigated. Also, the prediction of hydraulic performances such as static pressure rise, shaft power, hydraulic power and pump efficiency is carried out on the water pump including an impeller and a volute casing. A full size water pump test bench has been developed to validate the CFD flow model. Discharge flow rate, suction pressure, discharge pressure, rotational speed and torque measurements are provided. Coolant temperature is 8$0^{\circ}C$, water tank pressure is 1 kgf/$\textrm{cm}^2$ and flow rates vary.

ORC System Performance Analysis upon R-245fa and Novec 649 (R-245fa 및 NOVEC 649 작동유체에 따른 ORC 시스템 성능 변화)

  • Chang, Hong-Soon;Han, Young-Sub;Song, Yeong-Kil;Kim, Sung-Hyun
    • Journal of the Korean Society for Geothermal and Hydrothermal Energy
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    • v.12 no.3
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    • pp.17-23
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    • 2016
  • A test unit for Organic Rankine Cycle (ORC) power generation system was developed and experimentally reviewed the performance of the ORC system. Two different organic fluids (R-245fa & Novec 649) were tested as working fluids for the system. System behavior was measured and analyzed along with the variables, such as temperature, pressure, rpm and shaft power. It is one of the findings that Novec 649 fluid is to be less pressurized than R-245fa in order to up to the heat source (boiler) capacity, that limits the experiment as high as 2 kW in shaft power.

Performance Analysis of a Combined Scroll Expander-compressor unit for a Fuel Cell System (연료전지용 스크롤 팽창기-압축기 성능해석)

  • Kim, S.J.;Ahn, J.M.;Kim, H.J.
    • Journal of Power System Engineering
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    • v.13 no.3
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    • pp.11-19
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    • 2009
  • This paper introduces a conceptual design of a combined scroll expander-compressor unit for a fuel cell. Since air discharged out of the fuel cell stack has still high pressure energy, some power can be extracted from the air by directing it to pass through an expanding device. Such extracted power can be used to drive an auxiliary compressor. For this purpose, a scroll type expander coupled to a scroll type compressor was designed for a 1kW-class fuel cell. The orbiting scroll members of the expander and the compressor were made to share three of common drive shafts installed in the mid frame plate. Performance analysis for the combined expander-compressor unit showed that the installation of this unit could reduce the auxiliary power consumption in the fuel cell by about 42%.

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Performance Characteristics of an Axial Propeller Small-hydro Turbine with Various Cambers of Runner Blade (캠버각 변화에 따른 소수력 축류 프로펠러 수차의 유동 특성 연구)

  • Byeon, Sun-Seok;Kim, Tae-Youn;Han, Sang-Meok;Kim, Jeong-Hwan;Kim, Youn-Jea
    • New & Renewable Energy
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    • v.8 no.2
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    • pp.44-51
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    • 2012
  • The aim of this paper is to examine the hydraulically optimized camber of a blade. Prior studies have tried to determine the sound method of design on small-hydro turbines. These have appeared to realize a reasonably efficient small-hydro turbine. Nonetheless, specific and accurate design data have not as yet been established for the shape of the runner blade. Hence, this study examines the performance characteristic of an axial propeller turbine with 0~8% camber variations. The results of output power, efficiency, and pressure distribution of the turbine are graphically depicted. The definition of camber refers to the NACA airfoil. The commercial finite element analysis (FEA) packages, ANSYS, and CFX are used in this study. The results revealed the performance characteristics on small-hydro turbine and suggested a highly efficient section shape of the runner.

Design and Construction of a Bottoming Organic Rankine Cycle System for an Natural Gas Engine (가스엔진용 유기랭킨사이클의 설계 및 제작)

  • Lee, Minseog;Baek, Seungdong;Sung, Taehong;Kim, Hyun Dong;Chae, Jung Min;Cho, Young Ah;Kim, Hyoungtae;Kim, Kyung Chun
    • Journal of the Korean Institute of Gas
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    • v.20 no.6
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    • pp.65-72
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    • 2016
  • ORC system was designed and constructed for utilizing the heat of the exhaust gas and coolant released from the gas engine which was modified to use natural gas as a fuel. In this paper the components of the ORC system were designed and manufactured based on measured data of the gas engine. The components are composed of two plate heat exchanger, the 5kW-class expander and multi stage centrifugal pump. The thermodynamic performance of the ORC system was analyzed by using the electric heater. Also, the developed ORC system was implemented to modified natural gas engine. Two gas engines were used to supply heat to the ORC system. As a result of test bench, when the heat source temperature is $110^{\circ}C$ expander shaft power, the pressure ratio and cycle efficiency is 5.22kW, 7.41, 9.09%. As a result of field test, when the heat source temperature is $86^{\circ}C$ expander shaft power, the pressure ratio and cycle efficiency is 2kW, 3.75, 6.45%.

A Study on the Design of Fuel Transfer Pumps Gear Part for the Aircraft (항공기용 연료이송펌프 기어부 설계에 관한 연구)

  • Lee, Jung-hoon;Kim, Joon-tae
    • Journal of Aerospace System Engineering
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    • v.14 no.1
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    • pp.1-7
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    • 2020
  • This paper discusses a series of procedures and results for designing the gear part of a fuel transfer pump for an aircraft, developed as an independent technology for the first time in Korea. A gear pump type is selected because the design requirements of the fuel transfer pump are met by a gear pump with a characteristics of less leakage inside than a vane pump with superior overall performance. The gear housing is designed with suitable clearance, considering the outer diameter of the gear, which is the main factor on which the flow can be determined. Additionally, the calculation of the required hydraulic and axial force for the motor to drive the fuel transfer pump was performed.

A Study of the Shaft Power Measuring System Using Cameras (카메라를 이용한 축계 비틀림 계측 장치 개발)

  • Jeong, Jeong-Soon;Kim, Young-Bok;Choi, Myung-Soo
    • Journal of Ocean Engineering and Technology
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    • v.24 no.4
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    • pp.72-77
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    • 2010
  • This paper presents a method for measuring the shaft power of a marine main engine. Usually, in traditional systems for measuring shaft power, a strain gauge is used even though it has several disadvantages. First, it is difficult to set up the strain gauge on the shaft and acquire the correct signal for analysis. Second, it is very expensive and complicated. For these reasons, we investigated alternative approaches for measuring shaft power and proposed a new method that uses a vision-based measurement system. For this study, templates for image processing and CCD cameras were installed at the both ends of the shaft. Then, in order for the cameras to capture the images synchronously, we used a trigger mark and a optical sensor. The position of each template between the first and the second camera images were compared to calculate the torsion angle. The proposed measurement system can be installed more easily than traditional measurement systems and is suitable for any shaft because it does not contact the shaft. With this approach, it is possible to measure the shaft power while a ship is operating.