• Title/Summary/Keyword: Battery Aging

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Study on Fuel Economy Characteristics of Plug-In Hybrid Electric Vehicle by Cumulative Distance (누적 주행거리에 따른 플러그인 하이브리드 자동차의 연비 특성 연구)

  • PARK, JINSUNG;LIM, JAEHYUK;KIM, KIHO;LEE, JUNGMIN
    • Transactions of the Korean hydrogen and new energy society
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    • v.29 no.6
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    • pp.661-667
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    • 2018
  • Electric vehicles are taken a long time to charge and are restricted driving where charging infrastructure was not sufficiently constructed. The vehicle developed to solve these problems is a plug-in hybrid vehicle. It is possible to drive a certain distance by using electric motor and when the battery runs out, it operate the engine. Plug-in hybrid vehicle have a complicated structure and a lot of parts comparing a general vehicle because the electric parts and the internal combustion engine are installed together. Therefore, as the aging (mileage) of the plug-in hybrid vehicle, the influence which change of fuel consumption is expected to be larger than a general vehicle, but an experimental data are lacking. In this paper, we cumulate a mileage of the plug-in hybrid vehicle about 15,000 km and measured the fuel economy when the cumulated distance reached within 160 km, 6,500 km, 15,000 km respectively, by using domestic public test method. For measuring fuel economy of the vehicle, CD mode (driving distance on a single charge) which use only motor and the CS mode which operate motor and combustion engine were measured respectively. As a result, the fuel economy slightly increased at cumulated mileage of 6,500 km compared to the 160 km and the fuel economy of 15,000 km was similar to 160 km.

Research on fault analysis and reliability improvement of APU start motor for Korea Utility Helicopter (한국형 기동헬기 APU 시동모터 결함원인 분석 및 신뢰성 개선)

  • Kang, Tae-Woo;Yeom, Hyo-Won;Lee, Hee-Rang;Ahn, Jong-Moo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.6
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    • pp.703-709
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    • 2017
  • Korea Utility Helicopter(KUH) is a project to replace the aging helicopter presently being operated by the military with a domestic helicopter. The auxiliary power unit is a device that supplies emergency power to the system by an alternator installed when the main generator fails and the start motor converts the electrical energy of the battery into mechanical rotational energy to rotate the auxiliary power unit engine. With continuing power and operation, defects of the starting motor were found and improvements were carried out to solve it. In the failure mode analysis, the causes of possible defects were classified into 5 categories. Analysis of the 5 factors revealed that the main cause of defects is mechanical wear, which was found to be related to spring pressure. 250 tests were conducted through the theoretically determined pressure and regression analysis was performed with 4 sampling.The results showed that pressure was related to wear rate. In conclusion, early wear and breakage due to wear can be controlled through spring force and test showed the prediction of wear and the validity of the result were confirmed.