The invention relates to a storage tank system for an aircraft, comprising a storage tank (160), a chassis and attachment means (300), the storage tank (160) comprising an inner enclosure comprising an inner skin intended to store dihydrogen and an outer enclosure (186) comprising an outer skin surrounding the inner enclosure; the chassis includes a front frame (180) at a front end of the tank (160); an attachment device (300) attaches an outer skin of the outer enclosure (186) to the front frame (180). This system enables the reaction of forces by the outer skin, thereby reducing the complexity of the chassis.
本发明涉及一种用于飞行器的储罐系统,包括储罐(160)、底盘和附接装置(300),储罐(160)包括内封壳和外封壳(186),内封壳包括意在储存二氢的内蒙皮,外封壳(186)包括环绕内封壳的外蒙皮;底盘包括处于储罐(160)的前端处的前框架(180);附接装置(300)将外封壳(186)的外蒙皮附接到前框架(180)。这种系统使得能够通过外蒙皮对力进行反作用,从而降低底盘的复杂性。
Tank system comprising chassis, dihydrogen tank and means for attaching tank to chassis
包括底盘、二氢储罐和将储罐附接到底盘的装置的储罐系统
2022-11-22
Patent
Electronic Resource
Chinese
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