• Title/Summary/Keyword: 하이브리드추진시스템

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A Study on Optimal Capacity Design of Renewable Combined Power System for Energy Self-Sufficient Island (에너지 자립섬을 위한 신재생복합발전시스템의 최적용량 설계에 관한 연구)

  • Chang, Bong-Chul;Moon, Chae-Joo;Chang, Young-Hak;Park, Tae-Sik;Jeong, Moon-Seon
    • The Journal of the Korea institute of electronic communication sciences
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    • v.10 no.11
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    • pp.1271-1276
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    • 2015
  • The recent trend is that diesel power generation on islands where its prime cost for power generation is high is replaced by new and renewable energy. Therefore, south Jeolla province is progressing the construction project of self-sufficient islands for the areas where power is supplied by depending on diesel generators, which is the project that power is supplied through eco-friendly energy source using sunlight, wind power and energy storage device etc. However, it is difficult to construct new and renewable energy source with the capacity to respond to the load perfectly due to its environmental and geographical conditions regarding capacity design of new and renewable energy. Besides, Microgrid design considering appropriate capacity design of the system components and efficient operation is required through the analysis of climate conditions and load patterns from the design stage for optimal composition of a hybrid system with economic feasibility. Therefore, this study is aimed to conduct a research on optimal combination, capacity calculation and economic feasibility by comprising a hybrid power generation system which will replace 40% of power generation by diesel as new and renewable energy source for Geomun Island where has more than 300 households and requires expansion of the facility among islands located in southwest coast.

A Study on the Modeling of Ship Energy System Using Bond Graph (Bond Graph를 이용한 선박 에너지 시스템 모델링 연구)

  • Sang-Won Moon;Won-Sun Ruy
    • Journal of the Society of Naval Architects of Korea
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    • v.61 no.1
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    • pp.19-28
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    • 2024
  • Environmental regulations are becoming more stringent in response to climate change, especially concerning marine pollution caused by ship emissions. Large ships are adjusting by integrating technologies to reduce pollutant emissions and transitioning to eco-friendly fuels such as low-sulfur oil and LNG. However, small ships face space constraints for installing LNG propulsion systems and the risk of power depletion with pure electric propulsion. Consequently, there's growing interest in researching hybrid propulsion methods that combine electricity and diesel for smaller vessels. Hybrid propulsion systems utilize diverse energy sources, requiring an effective method for evaluating their efficiency. This study proposes employing Bond graph modeling to comprehensively analyze energy dynamics within hybrid propulsion systems, facilitating better understanding and optimization of their efficiency. Modeling of the ship's energy system using Bond graphs will be able to provide a framework for integrating various energy sources and evaluating their effects.

Power System Optimization for Electric Hybrid Unmanned Drone (전동 하이브리드 무인 드론의 동력 계통 최적화)

  • Park, Jung-Hwan;Lyu, Hee-Gyeong;Lee, Hak-Tae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.4
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    • pp.300-308
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    • 2019
  • For drones to be used for industrial or agricultural applications, it is necessary to increase the payload and endurance. Currently, the payload and endurance are limited by the battery technology for electric powered drones. In addition, charging or replacing the batteries may not be a practical solution at the field that requires near continuous operation. In this paper, a procedure to optimize the power system of an electric hybrid drone that consists of an internal combustion engine, a generator, a battery, and electric motors is presented. The example drone for crop dusting is sized for easy transportation with a maximum takeoff weight of 200 kg. The two main rotors that are mechanically connected to the internal combustion engine provides most of the lift. The drone is controled by four electric motors that are driven by the generator. By analyzing the flow of the energy, a methodology to select the optimum propeller and motor among the commercially available models is described. Then, a procedure of finding the optimum operational condition along with the proper gear reduction ratios for the internal combustion engine based on the test data is presented.

Characteritic Analysis of Hybrid Levitation and Propulsion System for Super-Speed Maglev (초고속 자기부상열차를 위한 하이브리드형 부상 추진 시스템의 특성 해석)

  • Cho, Han-Wook;Lee, Jong-Min;Han, Hyung-Suk
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.623_624
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    • 2009
  • This paper deals with the characteristic analysis of electro-magnet (EM)-permanent magnet (PM) hybrid levitation and propulsion device for magnetically levitated (maglev) vehicles. Several machine characteristics such as levitation force with/without control current and thrust are described. In order to verify the analysis results and feasibility of high-speed operation of the maglev vehicle, real-scale static test set is implemented and tested.

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Study of the Preliminary Design and Performance Prediction for the Hybrid Propulsion System (하이브리드 추진 시스템의 예비 설계 및 성능 예측에 관한 연구)

  • Yoon, Chang-Jin;Song, Na-Young;Yoo, Woo-Jun;Kim, Jin-Kon;Sung, Hong-Gye;Moon, Hee-Jang
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.14 no.4
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    • pp.17-23
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    • 2006
  • This paper describes the preliminary design procedure for the hybrid propulsion system. For a given mission defined by velocity increment, the design of a polyethylene/LOX hybrid rocket was implemented. In addition, Seven-cluster multi-port fuel-grain was considered. After determining the system size including the combustion chamber, the performance parameters such as specific impulse, thrust, characteristic velocity, and thrust coefficient can be predicted by using empirical regression rate correlation, though most of preliminary design code assume constant regression rate. The results of the performance prediction indicated that besides the widely used HTPB/LOX, polyethylene/LOX hybrid motor can be a viable alternative to the more widely used SRMs.

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Design of Hybrid Type Levitation and Propulsion System for High-Speed Maglev (초고속 자기부상열차를 위한 하이브리드형 부상 추진 시스템 설계)

  • Cho, Han-Wook;Han, Hyung-Suk;Lee, Jong-Min;Kim, Bong-Sup;Rho, Kyu-Suk;Kim, Dong-Sung
    • Proceedings of the KIEE Conference
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    • 2009.04b
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    • pp.94-96
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    • 2009
  • This paper deals with the design considerations of electro-magnet (EM)-permanent magnet (PM) hybrid levitation and propulsion device for magnetically levitated (maglev) vehicles. Several design considerations such as machine structure, manufacturing, and control strategy are described. In order to verify the design scheme and feasibility of control strategy, dynamic test set is implemented and tested.

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Trade-off Evaluation due to Application of Mixing Chamber for Hybrid Rocket-Propulsion System (하이브리드 로켓 추진 시스템의 혼합 연소실 적용에 따른 Trade-off 평가)

  • Kim, Hakchul;Moon, Keunhwan;Moon, Heejang;Kim, Jinkon
    • Journal of Aerospace System Engineering
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    • v.10 no.3
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    • pp.23-31
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    • 2016
  • The intermediate mixing chamber is one of various methods for improving the regression rate and combustion efficiency of the hybrid rocket. The mixing chamber with its non-combustible material makes the propulsion performance increase, but it leads to a low fuel-loading density in the combustion chamber; therefore, this performance-related trade-off between the mixing chamber and the low fuel-loading density was studied. In this study, the trade-off was conducted by comparing the intermediate-mixing-chamber case with a w/o-mixing-chamber case. The small hybrid-sounding rocket is designed with internal ballistics for comparing the rocket length to the weight. In addition, an external ballistic analysis was conducted for comparing the performances of the w/- and w/o-mixing-chamber cases. As a result, the intermediate-mixing-chamber case shows that the length and the weight were decreased to 12 % and 8 %, respectively; furthermore, when compared with the normal cases, the estimated altitude result of the w/-mixing-chamber case was increased to approximately 75 m.

Fuel Rich Gas O/F Ratio Characteristics of HDPE and Paraffin Fuel in Low Range of the Oxidizer Mass Flux (저 산화제유속 구간에서의 HDPE 및 Paraffin 연료의 연료농후가스 O/F비 특성)

  • Han, Seongjoo;Ryu, Sunghoon;Kim, Jinkon;Kang, Teagon;Moon, Heejang;Kim, Junhyung;Ko, Seung Won
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.6
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    • pp.54-60
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    • 2016
  • Multi-port HDPE and Paraffin firing tests are conducted for hybrid gas generator application of a ducted rocket in the low oxidizer mass flux range. A fuel rich gas of O/F ratio from 0.3 to 0.8, a typical O/F operating range of a ducted rocket gas generator, have been achieved with paraffin fuel implying that the hybrid system can be a potential candidate. It was also found that an almost constant O/F ratio regime exists under $35kg/m^2s$ of the oxidizer mass flux, opening a possibility for the paraffin fuel toward the VFDR gas generator application.

The Evaluation of an Electric Hybrid Power System for the High Endurance Drone (장기체공 드론용 하이브리드 전기 추진시스템 성능 평가)

  • Gang, Byeong Gyu;Kim, Keun-Bae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.5
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    • pp.539-544
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    • 2022
  • This research shows the test performance of a 6 kW-scale hybrid electric power system for the high endurance drone. The power system is composed of a two-stroke reciprocal engine, starter-generator and battery, and they are integrated as one power unit. The engine is designed to provide the house for holding the starter-generator at the end of a crankshaft in turn the engine and starter-generator can maintain the same speed during the operational period. In this way, the generated power is readily controlled by just manipulating an engine throttle movement. Moreover, the starter-generator can initiate an engine operation with an aid of battery power until the combustion process becomes stabilized. In consequence, integration mechanism between an engine and generator is simplified, which results in weight reduction achieved. The duty of back-up battery is to provide a starting power to generator via a system controller in addition to covering momentarily power shortage. Therefore, the electric power system is vindicated to provide 6 kW power through a ground test.

A Study on Energy Savings of a DC-based Variable Speed Power Generation System (직류기반 가변속 발전 시스템을 이용한 에너지 절감에 관한 연구)

  • Kido Park;Gilltae Roh;Kyunghwa Kim;Changjae Moon;Jongsu Kim
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.29 no.6
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    • pp.666-671
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    • 2023
  • As international environmental regulations on ship emissions are gradually strengthened, interest in electric propulsion and hybrid propulsion ships is increasing, and various solutions are being developed and applied to these ships, especially stabilization of the power system and system efficiency. The direct current distribution system is being applied as a way to increase the power. In addition, verification and testing of safety and performance of marine DC distribution systems is required. As a result of establishing a DC distribution test bed, verifying the performance of the DC distribution (variable speed power generation) system, and analyzing fuel consumption, this study applied a variable speed power generation system that is applied to DC power distribution for ships, and converted the power output from the generator into a rectifier. A system was developed to convert direct current power to connect to the system and monitor and control these devices. Through tests using this DC distribution system, the maximum voltage was 751.5V and the minimum voltage was 731.4V, and the voltage fluctuation rate was 2.7%, confirming that the voltage is stably supplied within 3%, and a variable speed power generation system was installed according to load fluctuations. When applied, it was confirmed through testing that fuel consumption could be reduced by more than 20% depending on the section compared to the existing constant speed power generation system.