• 제목/요약/키워드: Electric Power Take-off

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전기 수직이착륙 항공모빌리티용 동력플랫폼 개발을 위한 이착륙 실험시스템 연구 (A Study on Take-off and Landing Experimental System for Development of Power Platforms for Electric Vertical Take-Off and Landing Air Mobility)

  • 원준성;노광현
    • 한국산업융합학회 논문집
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    • 제26권4_2호
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    • pp.639-648
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    • 2023
  • In modern society, UAM (Urban Air Mobility) transportation system is being developed as an alternative to urban traffic congestion and environmental problems, and electric vertical take-off and landing (eVTOL) is a combination of vertical take-off and landing function and electric power. It is attracting attention as an innovative next-generation transportation method as an eco-friendly alternative that reduces noise and air pollution by providing efficient mobility within the city. Since eVTOL development requires designing and implementing airframes suitable for various mission purposes, the power system needs to be developed as a platform concept before airframe development. In this study, we empirically proposed a test bench concept equipped with a stable power supply and an efficient control system, essential in developing a power platform with a combined function in the form of a fuselage and module type specialized for various mission purposes. The proposed drivetrain platform test bench consists of a system verifying the stable take-off and landing software and a power platform adjusting the motor's thrust. It will serve as a verification system that can be developed.

농업용 전기차량의 전기식 동력인출장치용 전력변환시스템 (Power Conversion System for Electric Power Take-off of Agricultural Electric Vehicle)

  • 곽봉우;김종훈
    • 전기전자학회논문지
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    • 제23권3호
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    • pp.994-1002
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    • 2019
  • 본 논문은 농업용 전기차량의 전기식 동력인출장치용 전력변환시스템에 대해 제안한다. 대부분의 전기식 동력인출장치(Electric Power Take-Off : e-PTO)는 상용전원 $220V_{AC}$를 사용한다. 농업용 전기차량의 낮은 배터리 전압을 사용하여 높은 출력 전압을 공급하기 위한 DC-DC 컨버터와 DC-AC 인버터로 구성된 2단 구조를 갖는 양방향 전력변환시스템이 적합하다. 제안하는 전력변환시스템은 1단의 Dual Active Bridge(DAB)컨버터와 2단의 양방향 풀 브릿지 인버터로 구성된다. 또한, 초기 구동시 DC 버스단 커패시터 충전에 의해 발생되는 돌입 전류 저감을 위해 소프트 스타트 알고리즘을 제안한다. 3kW급 전력변환시스템 시제품 및 알고리즘을 구현하고 실험을 통해서 실용성을 입증하였다.

Declutching control of a point absorber with direct linear electric PTO systems

  • Zhang, Xian-Tao;Yang, Jian-Min;Xiao, Long-Fei
    • Ocean Systems Engineering
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    • 제4권1호
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    • pp.63-82
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    • 2014
  • Declutching control is applied to a hemispherical wave energy converter with direct linear electric Power-Take-Off systems oscillating in heave direction in both regular and irregular waves. The direct linear Power-Take-Off system can be simplified as a mechanical spring and damper system. Time domain model is applied to dynamics of the hemispherical wave energy converter in both regular and irregular waves. And state space model is used to replace the convolution term in time domain equation of the heave oscillation of the converter due to its inconvenience in analyzing the controlled motion of the converters. The declutching control strategy is conducted by optimal command theory based on Pontryagin's maximum principle to gain the controlled optimum sequence of Power-Take-Off forces. The results show that the wave energy converter with declutching control captures more energy than that without control and the former's amplitude and velocity is relatively larger. However, the amplification ratio of the absorbed power by declutching control is only slightly larger than 1. This may indicate that declutching control method may be inapplicable for oscillating wave energy converters with direct linear Power-Take-Off systems in real random sea state, considering the error of prediction of the wave excitation force.

전투함 하이브리드 전기추진 시스템의 PTO 운전모드 적용 및 연료절감 효과 연구 (A Study on the Adoption of Power Take Off Operation Mode and Fuel-Saving Effect in the Hybrid Electric Propulsion System for a Warship)

  • 김소연
    • 전력전자학회논문지
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    • 제24권1호
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    • pp.40-48
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    • 2019
  • Hybrid electric propulsion systems (H-EPSs) are an intermediate step for integrated full electric propulsion warships. H-EPSs are a dynamic combination of mechanical and electrical propulsion systems to achieve the required mission performances. The system modes could adapt to meet the requirement of the various operation conditions of a warship. This paper presents a configuration and operating modes of H-EPSs considering the operation conditions of a destroyer class warship. The system has three propulsion modes, namely, motoring mode, generating mode [power take off (PTO) mode], and mechanical mode. The PTO mode requires a careful fuel efficiency analysis because the fuel consumption rate of propulsion engines may be low compared with the generator's engines depending on the loading power. Therefore, the calculation of fuel consumption according to the operating modes is performed in this study. Although the economics of the PTO mode depends on system cases, it has an advantage in that it ensures the reliability of electric power in case of blackout or minimum generator operation.

Wave energy converter by using relative heave motion between buoy and inner dynamic system

  • Cho, I.H.;Kim, M.H.;Kweon, H.M.
    • Ocean Systems Engineering
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    • 제2권4호
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    • pp.297-314
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    • 2012
  • Power-take-off through inner dynamic system inside a floating buoy is suggested. The power take-off system is characterized by mass, stiffness, and damping and generates power through the relative heave motion between the buoy and inner mass (magnet or amateur). A systematic hydrodynamic theory is developed for the suggested WEC and the developed theory is illustrated by a case study. A vertical truncated cylinder is selected as a buoy and the optimal condition of the inner dynamic system for maximum PTO (power take off) through double resonance for the given wave condition is systematically investigated. Through the case study, it is seen that the maximum power can actually be obtained at the optimal spring and damper condition, as predicted by the developed WEC theory. However, the band-width of high performance region is not necessarily the greatest at the optimal (maximum-power-take-off) condition, so it has to be taken into consideration in the actual design of the WEC.

Tilt-rotor 항공기 동력계통 중량 추정에 대한 상쇄연구 (Trade-off Study of Propulsion Systems Weight Estimation for Tilt-rotor Personal Air Vehicle)

  • 이정훈
    • 항공우주시스템공학회지
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    • 제8권4호
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    • pp.1-6
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    • 2014
  • This paper presents the trade-off study of conducting a survey of the weights for various kind of propulsion systems installed in the Smart Unmanned Aerial Vehicle TR-100, a tilt-rotor vehicle, which is developed by Korea Aerospace Research Institute, in order to predict the appropriate propulsion system for present and future Personal Air Vehicle, which has single mode and vertical take-off & landing. In order to perform the trade-off study, we set the requirements that the vehicle hovers for 1 hour with 1,000 kg maximum take off weights. In this study, the power systems are classified engine, which uses the fossil fuel - turboshaft engine, piston engine, diesel engine and rotary engine, and electric motor with fuelcell or Li-Ion battery. The results of trade-off study shows the power systems using fossil fuel are superior to using fuelcell or Li-Ion battery for weight of propulsion system. Also turboshaft engine is the best power system for the aspects of system weight, and the nexts are rotary engine, piston engine, diesel engine, electric motor with Li-Ion battery, and electric motor with fuelcell.

Enhancement of wave-energy-conversion efficiency of a single power buoy with inner dynamic system by intentional mismatching strategy

  • Cho, I.H.;Kim, M.H.
    • Ocean Systems Engineering
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    • 제3권3호
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    • pp.203-217
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    • 2013
  • A PTO (power-take-off) mechanism by using relative heave motions between a floating buoy and its inner mass (magnet or amateur) is suggested. The inner power take-off system is characterized by a mass with linear stiffness and damping. A vertical truncated cylinder is selected as a buoy and a special station-keeping system is proposed to minimize pitch motions while not affecting heave motions. By numerical examples, it is seen that the maximum power can actually be obtained at the optimal spring and damper condition, as predicted by the developed WEC(wave energy converter) theory. Then, based on the developed theory, several design strategies are proposed to further enhance the maximum PTO, which includes the intentional mismatching among heave natural frequency of the buoy, natural frequency of the inner dynamic system, and peak frequency of input wave spectrum. By using the intentional mismatching strategy, the generated power is actually increased and the required damping value is significantly reduced, which is a big advantage in designing the proposed WEC with practical inner LEG (linear electric generator) system.

Comparative Analysis of the PWM of an Inverter for an Electric Aircraft Thrust Motor

  • Koo, Bon-soo;Jo, Seong-hyeon;Choi, In-ho
    • 항공우주시스템공학회지
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    • 제15권4호
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    • pp.21-29
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    • 2021
  • As global environmental regulations have been strengthened, the eco-friendly market has grown rapidly. In the field of aircraft, research on electric vertical take-off and landing aircraft that can enter city centers and perform personal air transportation using electric propulsion is ongoing. For aircraft using electric propulsion methods to operate reliably, electric power thrust systems are a key factor. Electric aircraft require a high power density for propulsion systems with strict limits on volume and weight. The efficient control of inverter systems is essential for achieving high power density. Therefore, in this paper, the characteristics of inverters and motors were analyzed through simulations based on the space vector pulse width modulation (PWM) and discontinuous PWM methods for controlling inverter systems.

Automatic Turn-off Angle Control for High Speed SRM Drives

  • Nashed Maged N.F.;Ohyama Kazuhiro;Aso Kenichi;Fujii Hiroaki;Uehara Hitoshi
    • Journal of Power Electronics
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    • 제7권1호
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    • pp.81-88
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    • 2007
  • This paper presents a new approach to the automatic control of the turn-off angle used to excite the Switched Reluctance Motor (SRM) employed in electric vehicles (EV). The controller selects the turn-off angle that supports and improves the performance of the motor drive system. This control scheme consisting of classical current control and speed control depends on a lookup table to take the best result of the motor. The turn-on angle of the main switches of the inverter is fixed at $0^{\circ}C$ and the turn-off angle is variable depending on the reference speed. The motor, inverter and control system are modeled in Simulink to demonstrate the operation of the system.