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Regenerative Fuel Cell (RFC) for High Power Space System Applications

机译:用于大功率空间系统应用的可再生燃料电池(RFC)

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The future large scale and high power systems for the space and aviation applications will require sources that are capable of generating and storage of large amount of power. Recent advancements in solar cells and solar array technologies have enabled options for providing lightweight and compact solar power generation capability in the 100 - 500kW range. However, in the cases where very high-energy storage capability is required, the energy density of the available energy storage technologies, like NiH_2 and Li-Ion batteries, limits the overall mission capabilities. In such cases, new energy storage devices, which have a much higher energy density capability, are essential to reduce the overall mass of the energy storage system. One such option is the use of "Regenerative Fuel Cell (RFC)" concept. "RFC" is combined with the solar electric power system or the jet-engine driven generator, which are the main electric power source of the spacecraft and the airplane, respectively. RFC system consists of the fuel cell, the electrolyzer and the fuel storage tanks. The fuel cell provides the electric power using the stored fuels, and the electrolyzer refuels the fuel tanks using the solar electric power. The advantage of RFC is its higher energy density capability compared with other energy storage devices. During past ten years, IHI Aerospace (IA) of Japan, in collaboration with Japanese Space Exploration Agency (JAXA), has been developing very high efficiency RFC technology to provide electric power for high altitude and long endurance airship and commercial airplanes applications. The RFC system, currently under development at IA, is capable of achieving ~ 300Wh/kg and has a growth path to ~ 450 Wh/kg. This technology was recently flight-demonstrated on the Boeing ecoDemonstrator program. This paper explores the Solar-RFC electric power system concept for high power space system applications such as the future Lunar and Mars base power systems. IA and Boeing are studying the feasibility of high power space system applications.
机译:未来用于太空和航空应用的大规模高功率系统将需要能够产生和存储大量功率的电源。太阳能电池和太阳能电池阵列技术的最新发展为提供100至500kW范围的轻巧紧凑的太阳能发电能力提供了可能。但是,在需要非常高的能量存储能力的情况下,可用的能量存储技术(如NiH_2和锂离子电池)的能量密度会限制总体任务能力。在这种情况下,具有更高能量密度能力的新储能设备对于减少储能系统的整体质量至关重要。一种这样的选择是“可再生燃料电池(RFC)”概念的使用。 “ RFC”与太阳能电力系统或喷气发动机驱动的发电机相结合,后者分别是航天器和飞机的主要电源。 RFC系统由燃料电池,电解槽和燃料储罐组成。燃料电池利用所存储的燃料提供电力,而电解器利用太阳能为燃料箱加油。 RFC的优点是与其他储能设备相比,其能量密度更高。在过去的十年中,日本的IHI航空航天(IA)与日本太空探索局(JAXA)合作,一直在开发非常高效的RFC技术,以为高海拔和长寿命的飞艇和商用飞机应用提供电力。 IA目前正在开发的RFC系统能够达到〜300Wh / kg,并有可能增长到〜450 Wh / kg。该技术最近在波音ecoDemonstrator计划中进行了飞行演示。本文探讨了针对高功率空间系统应用(例如未来的月球和火星基础电源系统)的Solar-RFC电力系统概念。 IA和波音正在研究高功率空间系统应用的可行性。

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