A hydrogen storage tank for a hydrogen aircraft includes an outer tank, an inner tank, a first strap, and a second strap. The inner tank is disposed inside the outer tank with a space therebetween, and has a shape having a longitudinal direction. The first strap includes a first end connected to an inner surface of the outer tank and a second end connected to an outer surface of the inner tank. The second strap includes a third end connected to the inner surface of the outer tank and a fourth end connected to the outer surface of the inner tank. The first strap and the second strap extend along the longitudinal direction of the inner tank, and in the longitudinal direction, a distance between the second end and the fourth end is shorter than a distance between the first end and the third end.
HYDROGEN STORAGE TANK FOR HYDROGEN AIRCRAFT
2025-05-29
Patent
Electronic Resource
English
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