Airbus Operations Gmbh

Airbus Operations Sl

Ana Fernández Ramírez

Jorge Ballestero Méndez

Jesus Javier Vazquez Castro

Guillermo Hernaiz Lopez

Nuria Colmenarejo Matellano

Daniel Cernada Morales

Raúl José Gómez Vizcaíno

César Julián Jiménez Rodríguez

An aircraft section comprising a first fuel storage tank and a second fuel storage tank arranged in a caudal tandem configuration. The corresponding casings, housing conduits configured for distribution of fuel to and from inside the tanks, are arranged in a common section of the fuselage and spaced between them. Also an aircraft with such a section.

Aircraft fuselage section

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 semi-cylindrical outer jacket established on top of the first and second outer jacket domes, a second semi-cylindrical outer jacket established in the bottom of the first and second outer jacket domes. The first and second semi-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 semi-cylindrical outer jackets.

Hydrogen tank for aircraft

Growing community of inventors

GETAFE, Spain

Ana Fernández Ramírez