With the measures herein, a composite layer material structure (20) comprising structural fuel cell cells (30), structural supercapacitors (60) and structural cells (80) is described. Each individual one of these parts (30, 60, 80) is designed to play a self-supporting role so that an aircraft component, such as an outer panel (22), can be manufactured therefrom. The aircraft components can generate electrical energy by means of structural fuel cell cells (30) and can be distributed throughout the aircraft (10) without wiring. In addition, a short-term power peak (98) is supplied by a structural supercapacitor (60), while a base load (96) is provided by a structural battery (80).
利用此处的措施,说明了复合层材料结构(20),该复合层材料结构包含结构燃料电池单体(30)、结构超级电容器(60)和结构电池(80)。这些部件(30,60,80)中的各个单独的部件被设计成起自承载作用,从而可以由其制造飞行器构件、例如外面板(22)。飞行器构件能够借助结构燃料电池单体(30)来产生电能,并且在没有布线的情况下将其分布在整个飞行器(10)上。此外,短期的功率峰值(98)由结构超级电容器(60)供应,而基本负载(96)由结构电池(80)提供。
Load-bearing composite layer material structure of aircraft component, aircraft component and aircraft produced therefrom
飞行器构件的起承载作用的复合层材料结构、用其制造的飞行器构件和飞行器
2022-06-17
Patent
Elektronische Ressource
Chinesisch
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