2 0 0 0 OA 宇宙機における船内ドローンへのワイヤレス給電
- 著者
- 嶋田 修平 川崎 治 本田 さゆり 鈴木 宏和
- 出版者
- The Japan Society of Applied Electromagnetics and Mechanics
- 雑誌
- 日本AEM学会誌 (ISSN:09194452)
- 巻号頁・発行日
- vol.30, no.1, pp.39-44, 2022 (Released:2022-04-20)
- 参考文献数
- 7
Wireless Power Transfer (WPT) for spacecraft can be contributed various merits, such as workload reduction, safety improvement, high heat insulation, long lifetime. Our team developed WPT prototype for space drone. WPT used mag-netic field resonance, and class E inverter (switching frequency = 6.78MHz). We performed some critical tests (electrical and EMI). As a result of the electric test, the secondary circuit was the highest, which reached thermal equilibrium at about 50 ° C (< Tj). As a result of EMI test, WPT confirmed the range of MIL-STD-461C RE02(excluding switching frequency and its harmonics).