The invention relates to a cryogenic tank and an aircraft including the same. In one aspect, a cryogenic tank (10) for an aircraft (30) is described, the cryogenic tank (10) providing a tank access for service of maintenance and repair of equipment inside the onboard tank of the aircraft (30). The inlet opening (44) is closed by a removable closure (48) that includes a multi-wall panel (56) that is vacuum insulated and is designed and fitted to the multi-tank wall (42) such that heat entering the cryogenic tank (10) is minimized and such that opening and closing of the removable closure (48) does not affect the vacuum.
本发明涉及低温罐和包括该低温罐的飞行器。在一个方面中,描述了一种用于飞行器(30)的低温罐(10),该低温罐(10)提供了用于对飞行器(30)的机载罐内部的设备进行维护和修理服务的罐入口。进入开口(44)由可移除的封闭件(48)封闭,该封闭件包括多重壁面板(56),该多重壁面板(56)是真空绝缘的并且被设计并装配至多重罐壁(42),使得进入低温罐(10)中的热量最小化,并且使得打开和关闭可移除的封闭件(48)不会对真空造成影响。
Cryogenic tank and aircraft comprising such cryogenic tank
低温罐和包括该低温罐的飞行器
2024-12-03
Patent
Electronic Resource
Chinese
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