• Title/Summary/Keyword: Vehicle cooling

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Characteristics of Dissimilar Materials Al alloy(A6005)-Mg alloy(AZ61) Under Friction Stir Welding for Railway Vehicle (철도차량 적용을 위한 Al alloy(A6005)-Mg alloy(AZ61) 이종소재 마찰교반용접 특성 연구)

  • Lee, Woo-Geun;Kim, Jung-Seok;Sun, Seung-Ju;Lim, Jae-Yong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.8
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    • pp.706-713
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    • 2016
  • In this study, the welding characteristics of friction stir welding were investigated in accordance with the tool plunge position and cooling to the base materials for the joining of dissimilar materials (A6005-AZ61). Other different welding conditions, such as the tool rotation speed and welding speed, were fixed to 500rpm-30mm/min, respectively, and welding was then carried out by placing the Mg alloy (AZ61) on the advancing side and Al alloy(A6005) on the retreating side. Welding was conducted under six different conditions. To investigate the welding characteristic, tensile test and microstructure observations using an optical microscope were carried out. As the tensile test result, the maximum strength appeared under the condition in which the tool is moved 1 mm to the Mg alloy direction and cooling to the base materials. Under the same welding conditions, the strength with cooling was approximately two times higher than that without cooling. The tool was located in each direction of 1.7 mm from the weld line. Therefore, in the excessive off-set of tool position, the welding integrity was in an extremely poor condition due to the lack of stirring. This study was confirmed by the A6005-AZ61 dissimilar friction stir welding the welding speed and the tool rotation speed. In addition, the temperature control and tool plunge position are important welding parameters.

The ETCS Convergence Terminal for Eco-driving and Vehicle Diagnostics (에코-드라이빙과 차량 진단 겸용 ETCS 융합 단말기)

  • Kim, Sam-Taek
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.12 no.2
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    • pp.29-34
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    • 2012
  • Nowadays, the problem of ETCS terminal in becoming popular gradually is that there is no services except for ETC. Therefore, we need new system that provide many type of additional services at one-terminal. In this paper, we study the additory function of ETCS terminal to afford many type of the vehicle administration beside collection and provider of traffic information. We descrived the method of Eco-driving function beside to save fuel signing instant and mean fuel-efficiency, measurement of section fuel-efficiency on OLED and then brings out the best driving habit in people and to prevent dangerous at the wheel as diagnosing engine oil, cooling water, fan belt, the point of changing consumables, diagnoses to an overheated engine, charges on generator through ECU. The multi-services terminal consist of the vehicle diagnosis module base on OBD-II and ETCS terminal.

우주발사체용 터보펌프 액체추진기관 시스템 분석

  • Seo, Kyoun-Su;Joh, Mi-Ok;Choi, Young-In;Hong, Soon-Do;Oh, Bum-Seok
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.151-156
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    • 2003
  • Liquid rocket engine system is classified into an engine of pressurization and turbo pump type by the way of fuel fed-supporting system. In the KSR-III sounding rocket, an engine of pressurization type was used, but there was lots of technical problems to be solved for a use as the first stage engine of space launch vehicle. So, an engine of turbo pump type was required to be developed to overcome the technical limitation of liquid rocket engine. In this research, the analysis of propellant of Kerosine-LOX and methane-LOX which are noticed as a future propellant was carried out for the purpose of studying the basic characteristics. And to review the basic characteristics of an engine of turbo pump type, among the sizing variant of the space launch vehicle, the ways of injecting a satellite to a direct orbit and transient orbit were discussed in this paper.

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Review of Cryogenic Propellant Densification Technology (극저온 추진제 고밀도화 기술동향 및 적용방안)

  • Cho Namkyung;Han Sangyeop;Kim Youngmog;Jeong Sangkwon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.3
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    • pp.133-144
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    • 2005
  • Enhancements to propellants provide an opportunity to either increase performance of an existing launch vehicle. One of the promising technologies is the use of densified cryogenic propellants such as liquid hydrogen and liquid oxygen. The main advantage of densified cryogenic propellants is the increase in propellant mass fraction. Increased propellant mass fraction means increased payload mass to orbit. This paper reviews the basic principles and current technology trends for cryogenic propellant densification technologies. Several promising densification methods are presented focused on liquid oxygen densification. Engine and vehicle performance analyses are also presented to quantify the potential performance benefits of densified propellants in an overall system. And suggestions of application scheme for satellite launch vehicle is made.

A Study on the Application of Phase Change Material for Electric Vehicle Battery Thermal Management System using Dymola (전기자동차 배터리팩 열관리시스템에서 상변화물질 적용에 관한 고찰)

  • Choi, Chulyoung;Choi, Woongchul
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.66 no.12
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    • pp.1889-1894
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    • 2017
  • Global automobile manufacturers are developing electric vehicles (EVs) to eliminate the pollutant emissions from internal combustion vehicles and to minimize fossil fuel consumptions for the future generations. However, EVs have a disadvantage of shorter traveling distance than that of conventional vehicles. To answer this shortfall, more batteries are installed in the EV to satisfy the consumer expectation for the driving range. However, as the energy capacity of the battery mounted in the EV increases, the amount of heat generated by each cell also increases. Naturally, a better battery thermal management system (BTMS) is required to control the temperature of the cells efficiently because the appropriate thermal environment of the cells greatly affects the power output from the battery pack. Typically, the BTMS is divided into an active and a passive system depending on the energy usage of the thermal management system. Heat exchange materials usually include gas and liquid, semiconductor devices and phase change material (PCM). In this study, an application of PCM for a BTMS was investigated to maintain an optimal battery operating temperature range by utilizing characteristics of a PCM, which can accumulate large amounts of latent heat. The system was modeled using Dymola from Dassault Systems, a multi-physics simulation tool. In order to compare the relative performance, the BTMS with the PCM and without the PCM were modeled and the same battery charge/discharge scenarios were simulated. Number of analysis were conducted to compare the battery cooling performance between the model with the aluminum case and PCM and the model with the aluminum case only.

Calculation and Comparison of Liquid Oxygen Filling System between the KSLV-I Flight Test Data and the Modeling of the KSLV-II Launch Complex (한국형발사체 발사대시스템 산화제공급계 충전 운용 설계의 검증을 위한 나로호 비행시험 실증 자료 분석)

  • Seo, Mansu;Lee, Jae Jun;Hong, Ilgu;Kang, Sunil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.107-114
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    • 2018
  • Korea Space Launch Vehicle (KSLV)-I flight test data and the modified 1-dimensional steady state modeling data from the critical design results of the KSLV-II liquid oxygen filling system operation are compared to validate the reliability of critical design modeling. A comparison of major flow rates and pressure values between test data and calculation results are conducted. The relative errors relative to maximum total flow rate for each cooling, filling, and replenishment mode are determined within 6.7%. Calculated pressure values at the outlet of the pump and the inlet of flow control valves are within 5.1%. The pressure at the inlet of the launch vehicle for each operation mode are within the measured pressure range.

Software Design about Integrated Fault Diagnosis for the Propulsion System of the Tracked Amphibious Assault Vehicle (궤도형 상륙돌격차량용 추진장치의 통합고장진단 S/W 설계)

  • Lee, Changkyu;Choi, Byeongho;Park, Daegon;Koo, Youngho;Shim, Sangchul;Chang, Kyogun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.24 no.4
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    • pp.457-466
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    • 2021
  • This paper describes the design of model-based fault diagnosis software to apply to the propulsion system in tracked amphibious assault vehicle which consists of an engine, a transmission, a cooling system, and two waterjets. This software includes specific functions to detect the failures regarding sensor malfunctions, mechanical malfunctions, control errors, and communication errors. This software generates the proper malfunction codes which are classified as the warning and caution. In order to validate the fault diagnosis software, the manual and automatic test are performed using the test program with 32 test cases. Test results show that the designed fault diagnosis software is reliable and effective for applying to the propulsion system.

Development of 200kW class electric vehicle traction motor driver based on SiC MOSFET (SiC MOSFET기반 200kW급 전기차 구동용 모터드라이버 개발)

  • Yeonwoo, Kim;Sehwan, Kim;Minjae, Kim;Uihyung, Yi;Sungwon, Lee
    • Journal of IKEEE
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    • v.26 no.4
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    • pp.671-680
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    • 2022
  • In this paper, A 200kW traction motor driver that covers most of the traction motor specification of commercial electric vehicles (EV) is developed. In order to achieve high efficiency and high power density, a next-generation power semiconductors (Silicon carbide, SiC) are applied instead of power semiconductor(IGBT), which is Si based. Through hardware analysis for optimal use of SiC, expected efficiency and heat dissipation characteristics are obtained. A vector control algorithm for an IPMSM (Interior permanent magnet synchronous motor), which is mostly used in EV(Electric vehicle) traction motor, is implemented using DSP (Digital signal processor). In this paper, a prototype traction motor driver based SiC for EV is designed and manufactured, and its performance is verified through experiments.

Microstructure analysis of pressure resistance seal welding joint of zirconium alloy tube-plug structure

  • Gang Feng;Jian Lin;Shuai Yang;Boxuan Zhang;Jiangang Wang;Jia Yang;Zhongfeng Xu;Yongping Lei
    • Nuclear Engineering and Technology
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    • v.55 no.11
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    • pp.4066-4076
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    • 2023
  • Pressure resistance welding is usually used to seal the connection between the cladding tube and the end plug made of zirconium alloy. The seal welded joint has a direct effect on the service performance of the fuel rod cladding structure. In this paper, the pressure resistance welded joints of zirconium alloy tube-plug structure were obtained by thermal-mechanical simulation experiments. The microstructure and microhardness of the joints were both analyzed. The effect of processing parameters on the microstructure was studied in detail. The results showed that there was no β-Zr phase observed in the joint, and no obvious element segregation. There were different types of Widmanstätten structure in the thermo-mechanically affected zone (TMAZ) and heat affected zone (HAZ) of the cladding tube and the end plug joint because of the low cooling rate. Some part of the grains in the joint grew up due to overheating. Its size was about 2.8 times that of the base metal grains. Due to the high dislocation density and texture evolution, the microhardnesses of TMAZ and HAZ were both significantly higher than that of the base metal, and the microhardness of the TMAZ was the highest. With the increasing of welding temperature, the proportion of recrystallization in TMAZ decreased, which was caused by the increasing of strain rate and dislocation annihilation.

Thermoelectric Power Generation System with Loop Thermosyphon (루프형 열사이폰을 이용한 열전발전 시스템)

  • Kim, Sun-Kook;Rhi, Seok-Ho;Won, Byung-Chul;Kim, Dae-Hyun;Lee, Chung-Gu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.33 no.9
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    • pp.718-721
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    • 2009
  • A new progressive advanced approach (Loop thermosyphon Thermoelectric Power generation System) is suggested to optimize heat recovery ability from vehicle exhaust gas. As an initial look at device feasibility, the present new TE system adopted the loop thermosyphon as a cooling heat exchanger. The TE system with loop thermosyphon was investigated in terms of working fluids, instability of system, amount of working fluid, and so on. Basically, the present experimental works have been focused on finding the optimum working condition of the system to improve thermoelectric power output and to obtain stable power generation to operate hybrid vehicles. The present experimental results with the loop thermosyphon TE module shows possibilities as an improved TE system for future thermoelectric hybrid vehicles.