航空航天用高温聚合物电容器

C. Landrock, B. Kaminska
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引用次数: 21

摘要

由于需要在提高性能的同时减小系统尺寸和重量,当今许多军事和商业系统都需要高温电子设备来运行执行器、高速电机或发电机。在满足完整的高温系统所需的许多无源器件中,没有一个比电容器更有问题,特别是对于需要几个微或毫法拉值的较大器件。在这里,我们介绍了我们最近开发的一种聚合物金属复合材料,该材料满足典型的航空航天设计要求,即高可靠性、坚固性、轻量化以及高温(高达300°C)操作。我们最近发现了夹在金属电极之间的全氟磺酸聚合物的电容性行为,这导致了高温高密度被动存储元件的令人兴奋的发展。这些复合材料的单位平面面积电容为~ 1.0 mF cm - 2,对于~ 100 μ m厚的聚合物衬底,电容为40 mF/g,在加热到100°C后,电容只会立即出现可预测的小幅度下降,然后电容保持恒定,直至300°C。在这里,我们报告了这种夹在两层金属薄膜之间的聚合物复合材料的单步微加工金属电极的设计和测试,以及它们在高温下的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High temperature polymer capacitors for aerospace applications
Due to the need for reducing system size and weight while increasing performance, many military and commercial systems today require high-temperature electronics to run actuators, high-speed motors or generators. Of the many passive devices required to satisfy the needs for a complete high temperature system, none has been more problematic than the capacitor, particularly for larger devices requiring values of several micro- or milli-farads. Here we introduce a polymer metal composite we have recently developed that meets typical aerospace design constraints of high reliability, robustness, light-weight, as well as high temperature (up to 300°C) operation. Our recent discovery of the capacitive behaviour in perfluorinated sulfonic acid polymers sandwiched between metal electrodes has lead to the exciting development of high temperature capable high density passive storage components. These composites exhibit capacitance per unit planar area of ∼1.0 mF cm−2 or 40 mF/g for a ∼100 µm-thick polymer substrate, with only a small predictable decrease in capacitance immediately after heating to 100°C followed by constant capacitance up to 300°C. Here we report the design and testing of single step microfabrication of metal electrodes to these polymer composites sandwiched between two thin metal films along with their performance at high temperatures.
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