• Title/Summary/Keyword: Electric Propulsion System

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A Study On Field Test of IGBT Type Propulsion System fo Electric oilway (전동차용 IGBT형 추진제어장치의 본선시험에 관한 연구)

  • 정만규;고영철;방이석;서광덕
    • The Transactions of the Korean Institute of Power Electronics
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    • v.5 no.5
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    • pp.515-521
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    • 2000
  • This paper describes the field test results of IGBT VVVF inverter for the railway propulsion system. The 1,650kVA IGBT VVVF inverter has been developed. Therefore, the field test is performed in SMG 6 Line to confirm its the reliability and performance. The train consists of 4M4T and the electrical equipment for field test are as follows : VVVF inverter 4 sets, 16 traction motors and 2 SIVs. The propulsion system is composed with 1C4M(1-Controller 4-Motors). The results of propulsion system which have the excellent acceleration/deceleration and the jerk characteristics as well as starting ability on slope are taken through the field test.

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Wireless Energy Supply for a MAV Propulsion System

  • Shimane, Eri;Komatsu, Shuhei;Komaru, Takashi;Komurasaki, Kimiya;Arakawa, Yoshihiro
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.862-865
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    • 2008
  • Wireless energy supply for an MAV propulsion system using microwave was developed. This system consists of three sub system; the transmitter system, the rectenna system, and the tracking system. In the transmitter system five horn antennas were used as the antenna elements for the phased array system and both the beam divergence and steering angle was about 9deg. Eight rectennas were arrayed in parallel to obtain enough power to drive the electric motor on the MAV(the voltage was 250mV and the current was 6.8mA) in rectenna system. In tracking system two units of antenna system with leaf pattern which received the linearly-polarized wave despite the MAV yaw angle were set in each axis(x, y) for tracking an MAV in a 2-Dimentional space. And three output voltages $V_{com},\;V_1$ and $V_2$ were loaded in the PC to detect if the distance between transmitter and receiver was not constant. Finally when the microwave beam was steered by the phased array system the output voltage from rectenna was measured at 62cm while the MAV circled around above the transmitter system.

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The State of the Art and Application of Actuator in Aerospace (항공우주용 구동장치 개발 동향)

  • Yoon, Gi-Jun;Park, Ho-Youl;Jang, Ki-Won
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.6
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    • pp.89-102
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    • 2010
  • In this paper, a study on the future-oriented actuator introduces the future technology and future direction in aerospace and several industry fields. In particular, the mechanical linkage or hydraulic and pneumatic actuators which have the higher output-to-weight ratio have been used a lot in the past as the aircraft's flight control device. Most recently, Fly-By-Wire system has been used in aircraft and the flight control system has been changed in more electric and all electric systems. Electrohydraulic actuators and electric actuators have been developed continually, because they have better efficiency, safety and lower cost for the flight control system of aircraft. Also, to improve the weight condition, accuracy and response of actuator, new field actuators using new materials have been developed. In this paper we clearly proposed the actuator design and detailed technology development trend for next generation actuation system in aerospace and new field.

Analysis of Development Trend for the Integrated Power System of Naval Vessels to Perform the High-Power and Energy Mission Load Platform (고출력 에너지 사용 체계 플랫폼 실현을 위한 해군함정의 통합 동력 시스템 발전 경향 분석)

  • Lee, Hyung-Min;Cho, Byung-Jin
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.6
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    • pp.796-801
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    • 2011
  • The objective of this work presented here was focused on analysis of development trend for the integrated power system of naval vessels to perform the high-power and energy mission load platform. These mission loads are affected by the high level of military technologies, digitalization of the ocean battlefield, high power sensor system for maximization of the ship survivability. All electric power including propulsion power for ship should be controlled by integrated single system in order to carry various high power density weapon system such as Electromagnetic Aircraft Launch System, Electromagnetic Rail Gun[feasible precision striking at long distance 200NM(370km) or over]. As the analyzing the present state of things, mechanical propulsion system is shifted into hybrid or fully electric propulsion systems to realize integrated power system at the developed countries. Such challenges include reduced dependency on foreign-supplied fossil fuel, increasing demand for installed ship power, controlling life-cycle costs.

A Running and Transient state Test of VVVF Inverter using A Inertia Load in Electric car (관성부하를 이용한 전동차용 VVVF인버터의 모의주행 및 과도상태시험)

  • 정만규;정기찬;고영철;방이석;서광덕
    • Proceedings of the KIPE Conference
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    • 1999.07a
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    • pp.282-286
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    • 1999
  • This paper presents a vector control of parallel drive, a beatless control and a low switching PWM technique for the propulsion system of Electric car as transient state which are included interrupting line voltage, changing line voltage slowly, suddenly, regenerating light load and starting from backward running. Improved performance and a validation of proposed method is shown by the experimental results using a 1.65MVA IGBT VVVF inverter and inertia load equivalent to 160 tons electric cars through a running and transient state test.

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A Inertia Load Test using a Low Frequency Synchronous PWM Technique of high efficiency for Electric car. (전동차용 고효율 저주파 동기 PWM을 이용한 관성부하 시험)

  • 이광주;정만규;고영철;장성영;방이석
    • Proceedings of the KSR Conference
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    • 1998.11a
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    • pp.233-240
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    • 1998
  • This paper presents a high efficiency low switching PWM technique for the propulsion system of Electric car. In order to achieve the continuous voltage control to six-step and a low harmonics with low switching frequency under 500㎐, the synchronous technique is combined with a space vector overmodulation and implemented by using DSP. Improved performance and a validation of proposed method is shown by the experimental results using a 1.65MVA IGBT VVVF inverter and inertia load equivalent to 160 tons electric cars.

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Design of DC-DC Converter to Charge and Discharge Ultra-Capacitor Modules for Wireless Trains (무가선 전동차용 울트라커패시터 모듈 충·방전을 위한 DC-DC 컨버터 설계)

  • Jo, Jeong-Min;Han, Young-Jae;Kim, Jae-Won;Lee, Jang-Moo;Kim, Gil-Dong
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.64 no.12
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    • pp.1776-1781
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    • 2015
  • Electric power trains receive electric power from overhead cables via a pantograph system. Power collector system in trains increase the cross section of tunnel and require a massive coreless filter reactor in propulsion inverter because of the power disturbance by contact loss phenomenon of a train. In this paper we proposed a wireless train which can run to next station with charging energy of ultra-capacitor module block. We designed DC-DC converter to charge and discharge ultra-capacitor modules by using Next Train running test results and confirm the feasibility of the proposed system through simulation.