• Title/Summary/Keyword: Fuel cell propulsion

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Power Management of Fuel Cell Propulsion System for Unmanned Aerial Vehicles (무인기용 연료전지 추진 시스템의 동력 관리)

  • Kim, Tae-Gyu;Shim, Hyun-Chul;Kwon, Se-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.13-16
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    • 2007
  • Fuel cell was used as a propulsion system for unmanned aerial vehicles (UAV) in the present study. Fuel cell propulsion system are an ideal alternative power source with high energy density for high-endurance UAV. Fuel cell power system provides UAV up to five times the energy densiη of existing batteries. Sodium borohydride, stored in liquid state, was selected as a hydrogen source. Hydrogen generation system consists of catalytic reactor, pump, fuel cartridge, and separator. Hybrid power management system (PMS) between fuel cell and lithium-polymer ba야ery was developed. Motor, pump, and fans, operated on battery power controlled by feedback signals of fuel cell system. Battery was recharged by surpuls powr of fuel cell.

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Development Method of a Fuel Cell System for Small Unmanned Aerial Vehicles (소형 연료전지 무인기용 연료전지 추진체계 개발방안)

  • Kim, Tae-Gyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.219-221
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    • 2011
  • This paper reports the development trend of small fuel cell unmanned aerial vehicles. Development method of a fuel cell propulsion system for small unmanned aerial vehicles is proposed and discussed, such as the lightweight fuel cell stack development, liquid fuel-based hydrogen storage/generation, and fuel cell system technology.

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Hardware passive power control simulation of hybrid propulsion system for electric propulsion aircraft (전기추진 비행기용 하이브리드 추진시스템 패시브 전력제어 하드웨어 시뮬레이션)

  • Park, Poo-Min;Lee, Kang-Yeop;Hwang, Oh-Sik;Kim, Young-Mun;Kim, Chun-Taek
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.544-547
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    • 2011
  • This paper describes on hardware simulation of passive power control of propulsion system for electric propulsion aircraft of KARI. The propulsion system uses hybrid power system that is composed of solar cell, fuel cell and battery. The fuel cell is replaces by simulator due to its difficulty in handling while the other components are the same as that will be used on board. As the result, reliable power supply for propulsion is confirmed and each power source is well operated showing its characteristics.

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Air-independent Fuel Cell Power System (공기 불요 연료전지 동력 시스템)

  • Kim, Tae-Gyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.331-334
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    • 2009
  • An air-independent propulsion (AIP) system based on fuel cell technologies was developed for space and underwater applications in the present study. Hydrogen peroxide was selected as an oxidizer for space and underwater power applications where air independence is a must. Catalytic decomposition of hydrogen peroxide was used to generate oxygen and water. The pure oxygen was provided to a fuel cell and the water was stored separately. Sodium borohydride in the solid state was used as a hydrogen source in the present study. Pure hydrogen can be generated by a catalytic hydrolysis reaction. A fuel cell system was fabricated to validate the fuel cell based air-independent power system and was evaluated at the various conditions.

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Efficiency Evaluation of a Hybrid Propulsion Fuel Cell Ship Based on AIS Data (항적 데이터에 기반한 하이브리드 추진 연료전지 선박의 효율 평가)

  • Donghyun Oh;Dae-Seung Cho
    • Journal of the Society of Naval Architects of Korea
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    • v.60 no.3
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    • pp.146-154
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    • 2023
  • Efforts have been made to reduce the greenhouse gas emissions from ships by limiting the energy efficiency index, and net zero CO2 emission was proposed recently. The most ideal measure to achieve zero emission ship is electrification, and fuel cells are considered as a practical power source of the electrified propulsion system. The electric efficiency in the electrochemical reaction of fuel cells can be achieved up to 60% practically. The remaining energy is converted to heat energy but most of them are dissipated by cooling. In the author's previous research, a hybrid propulsion system utilizing not only electricity but also heat was introduced by combining electric motor and steam turbine. In this article, long term efficiency is evaluated for the introduced hybrid propulsion system by considering a virtual 24,000 TEU class container carrier model. To reflect a more practical operating condition, the actual navigation data of a similar real ship in the real world were collected from automatic identification system data and applied. From the result, the overall efficiency of the hybrid propulsion system is expected to be higher than a conventional electric propulsion fuel cell ship by 30%.

A Study on the Submarine Air Independent Propulsion System: Focused on Submarines Currently in Operation (잠수함 공기불요 추진체계에 대한 연구: 현재 운용 중인 잠수함을 중심으로)

  • Jang, Junseop
    • Journal of the Korea Institute of Military Science and Technology
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    • v.24 no.4
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    • pp.418-425
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    • 2021
  • Submarines are weapons systems that have been proven to be useful in battle since World War I and have continued to improve the efficiency of propulsion systems in order to be used efficiently on the battlefield. In particular, countries that unable to utilize nuclear propulsion systems make efforts to increase the efficiency of Air Independent Propulsion systems, and typical examples are fuel cells, Stirling engines and MESMA. It is also expected that the development of new propulsion systems such as hydrogen-reformer fuel cells, metal-air fuel cell and direct combustion propulsion systems will continue, so the characteristics of these will be examined and the performance based on the published data be checked in this thesis.

Fuel Cell Powered UAV with NaBH4 as a Hydrogen Source

  • Kim, Tae-Gyu;Shim, Hyun-Chul;Kwon, Se-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.579-582
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    • 2008
  • PEM Fuel cell system was designed and constructed to use as a power source of unmanned aerial vehicles(UAV) in the present study. Sodium borohydride was selected as a hydrogen source and was decomposed by catalytic hydrolysis reaction. Fuel cell system consists of a fuel cell stack, a hydrogen generation system(HGS), and power management system(PMS). HGS was composed of a catalytic reactor, micropump, fuel cartridge, and separator. Hybrid power system between lithium-polymer battery and fuel cell was developed. The fuel cell system was integrated and packaged into a blended wing-body UAV. Energy density of the total system was 1,000 $W{\cdot}hr/kg$ and high endurance more than 5 hours was accomplished in the ground tests.

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Modeling and Simulation of Secondary Battery-Fuel Cell Propulsion System for Underwater Vessel to Estimate the Operation Time (수중함용 2차전지-연료전지 추진체계의 성능 예측을 위한 M&S 연구)

  • Ji, Hyunjin;Cho, Sungbaek;Bae, Joongmyeon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.17 no.5
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    • pp.694-702
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    • 2014
  • One of the most important devices in an underwater vessel is a propulsion system. It should be a quiet and efficient system for stealthy operations in the large mission area. Hence lead-acid battery system has been used to supply the energy to electric motor. Recent technological developments and improvements, such as polymer electrolyte membrane(PEM) fuel cell and lithium polymer battery and have created the potential to improve overall power and propulsion performance. An underwater vessel always starts their mission with a limited energy and is not easy to refuel. Therefore design of energy elements, such as fuel cell and battery, and their load distribution are important to increase the maximum operating time of underwater vessel. In this paper, the lead-acid battery/PEM fuel cell and lithium polymer battery/PEM fuel cell were suggested as propulsion system and their performances were analyzed by modeling and simulation using Matlab/Simulink. Each model concentrated on representing the characteristics of energy element depending on demand current. As a result the effect of load distribution between battery and fuel cell was evaluated and the operation time of each propulsion system was able to be estimated exactly.

Development of a 25kW-Class PEM Fuel Cell System for the Propulsion of a Leisure Boat (선박 추진용 25kW급 고분자전해질 연료전지 시스템 개발)

  • Han, In-Su;Jeong, Jeehoon;Kho, Back-Kyun;Choi, Choeng Hoon;Yu, Sungju;Shin, Hyun Khil
    • Transactions of the Korean hydrogen and new energy society
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    • v.25 no.3
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    • pp.271-279
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    • 2014
  • A 25kW-class polymer electrolyte membrane (PEM) fuel cell system has been developed for the propulsion of a leisure boat. The fuel cell system was designed to satisfy various performance requirements, such as resistance to shock, stability under rolling and pitching oscillations, and durability under salinity condition, for its marine applications. Then, the major components including a 30kW-class PEM fuel cell stack, a DC-DC converter, a seawater cooling system, secondary battery packs, and balance of plants were developed for the fuel cell system. The PEM fuel cell stack employs a unique design structure called an anodic cascade-type stack design in which the anodic cells are divided into several blocks to maximize the fuel utilization without hydrogen recirculation devices. The performance evaluation results showed that the stack generated a maximum power of 31.0kW while maintaining a higher fuel utilization of 99.5% and an electrical efficiency of 56.1%. Combining the 30-kW stack with other components, the 25kW-class fuel cell system boat was fabricated for a leisure. As a result of testing, the fuel cell system reached an electrical efficiency of 48.0% at the maximum power of 25.6kW with stable operability. In the near future, two PEM fuel cell systems will be installed in a 20-m long leisure boat to supply electrical power up to 50kW for propelling the boat and for powering the auxiliary equipments.

Ground Integrated Test for the Hybrid Electric Propulsion System (하이브리드 전기추진 시스템 지상통합시험)

  • Lee, Bo-Hwa;Kim, Young-Mun;Park, Poo-Min;Kim, Keun-Bae;Cha, Bong-Jun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.772-776
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    • 2011
  • EAV-2, which has a solar cell, fuel cell and battery as its power sources, is under development by KARI. Electric power sources are selected through voltage matching without power converter and controller and tested. The ground integrated test for integrated system is performed during 5 hr. it is confirmed that battery's power response is faster than other power sources at starting and transient condition, fuel cell and solar cell are a major electrical power during cruise condition. It is revealed that the used energy portions of fuel cell, solar cell and battery are 68%, 29%, 2.5% respectively.

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