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Inductive Power Transfer for Spaceflight Systems

机译:空间系统的电感电力传输

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NASA Goddard Space Flight Center has developed technology that uses inductive power transfer (IPT) for wireless power interfaces between spaceflight elements (such as the payload, vehicle, and pad). Current spaceflight systems require traditional hardwire connections for power interfaces. This introduces risk of failure due to such factors as bent pins and contact contamination, as well as other disadvantages. IPT enables power interfaces that do not require physical access or interconnection. It also provides power interfaces that are more reliable and safer than traditional, hardwire connections. IPT also enables contamination-proof interfaces for terrestrial and non-terrestrial applications. The external support equipment includes a rectifier module, DC voltage regulator, and 208-Volt/480-Volt contactor or inverter for primary supply. The IPT device has no moving parts to wear out; the PSA's unit is encased in stainless steel. It is water- and oil-tight and there is no maintenance required.
机译:美国宇航局戈达德太空飞行中心已经开发了使用电感电力转移(IPT)的技术,用于空间压力元件(如有效载荷,车辆和垫)之间的无线电源接口。当前的航天器系统需要传统的硬件连接进行电源接口。这引入了由于弯曲引脚和接触污染等因素以及其他缺点而导致的失败风险。 IPT启用不需要物理访问或互连的电源接口。它还提供比传统的硬件连接更可靠和更安全的电源接口。 IPT还可以实现陆地和非陆地应用的污染界面。外部支撑设备包括整流模块,直流电压调节器和208伏/ 480伏接触器或逆变器,用于主要供应。 IPT设备没有磨损的移动部件; PSA的单元采用不锈钢包装。它是水和油腻的,无需维护。

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    《NASA Tech Briefs》 |2019年第8期|29-30|共2页
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