【24h】

RD Status of RFC Technology for SPF Airship in Japan

机译:日本SPF飞艇RFC技术的研发状况

获取原文

摘要

The first phase R&D program of the regenerative fuel cell (RFC) technology for the unmanned solar-powered stratospheric platform (SPF) airship of Japan Aerospace Exploration Agency (JAXA) has been conducted during 1998 and 2009. The SPF airship has an important role on provision of a new infrastructure for telecommunication services and the earth observations. For this high altitude and long-term station keeping (long endurance) airship realization, a combined power technology of solar cells (SC) and RFC is viewed as one of the most important technical challenges which shall be solved on a R&D road to the SPF airship feasibility in near future. The design targets for "solar-RFC" power technology demonstration have been definitely specified through ground-based research tasks after the SPF airship feasibility study in 1998. The ground test RFC model of 1KW output was developed in 2001, and the RFC technology was evaluated to provide more detailed data in closed-circuit RFC operations. And the on-board type RFC model of 3KW maximum output was developed in 2004 and the performance, cycle operations and environment (low temperature, low frequency motion, attitudes and low pressure) testing of this model had been conducted during 2005 and 2008. Based on these testing results, the on-board solar-RFC system was evaluated to achieve the energy density of 450 Wh/kg for 30KW output system after several key technologies for the system weight reduction were developed. Summarized herein are technical achievements available to date from these solar-RFC research activities in JAXA and IHI Aerospace (IA), and our future R&D planning is also described. The RFC technology is an attractive energy storage device, so this will be expected to be utilized in many aerospace systems.
机译:日本航空航天局(JAXA)的无人驾驶平流层平台(SPF)飞艇的再生燃料电池(RFC)技术的第一阶段研发计划已于1998年和2009年进行。为电信服务和地球观测提供新的基础设施。为了实现这种高海拔和长期保持站位(长寿命)的飞艇,太阳能电池(SC)和RFC的组合动力技术被视为最重要的技术挑战之一,必须在SPF的研发道路上加以解决飞艇在不久的将来具有可行性。在1998年SPF飞艇可行性研究之后,通过地面研究任务明确确定了“太阳能RFC”电力技术演示的设计目标。2001年开发了1KW输出的地面测试RFC模型,并对RFC技术进行了评估在闭路RFC操作中提供更详细的数据。 2004年开发了最大输出功率为3KW的车载RFC模型,并于2005年和2008年进行了该模型的性能,循环操作和环境(低温,低频运动,姿态和低压)测试。根据这些测试结果,在开发了几种减轻系统重量的关键技术之后,对车载太阳能RFC系统进行了评估,以使30KW输出系统的能量密度达到450 Wh / kg。本文总结了迄今为止在JAXA和IHI Aerospace(IA)进行的Solar-RFC研究活动中可获得的技术成就,并且还描述了我们未来的研发计划。 RFC技术是一种有吸引力的能量存储设备,因此有望在许多航空航天系统中使用它。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号