公开(公告)号：US20230035247A1

公开(公告)日：2023-02-02

申请号：US17872702

申请日：2022-07-25

Applicant: Airbus Operations S.L.U.

Inventor： Guillermo HERNAIZ LOPEZ ,  Jorge BALLESTERO MÉNDEZ ,  Jesus Javier VAZQUEZ CASTRO ,  Ana FERNANDEZ RAMIREZ

IPC: F17C1/02

Abstract: A hydrogen tank for aircraft, including an inner vessel configured to contain hydrogen, first and second outer jacket domes having a semi-spherical shape and first L-shaped ends, a first cylindrical outer jacket established on top of the first and second outer jacket domes, a second cylindrical outer jacket established in the bottom of the first and second outer jacket domes. The first and second cylindrical outer jackets include second L-shaped ends. The first and second L-shaped ends form L-shaped junctions to attach the first and second outer jacket domes to the first and second cylindrical outer jackets.