Airbus Operations Gmbh

Airbus Operations (s.a.s.)

Airbus (sas)

Airbus Operations Sl

Kasidit Leoviriyakit

Guillaume Gallant

Christopher Wright

Gerd Heller

Ben Commis

Till Marquardt

Philip Wright

André Anger

Jose Luis Martinez Munoz

Alberto Gallegos Elvira

Rainer Tegtmeyer

Michael Wießmeier

Matthias Wolff

Alexander Broer

Elisa Alvarez López-Herrero

Marco Dias Figueiredo

Anna-Katrin Wengorra

Kaya Sahin

An aircraft fuselage is configured to receive two tanks designed to contain liquid hydrogen. The fuselage includes a first section for a cockpit, a second section for a passenger cabin and a third section (T) distinct from the first section (T) and from the second section (T). The third section (T) includes two housings each to house a tank. The two housings are arranged symmetrically with respect to a vertical plane of symmetry (P). This arrangement of the tanks in a section distinct from the other sections allows them to be located as close as possible to the motors that they have to supply.

Aircraft fuselage intended to receive two tanks designed to contain liquid hydrogen

An aircraft () including a wing () and a winglet () at the end of the wing, the winglet including: a root (); a tip (); a transition region () extending away from the root; and a wing-like region () extending from the distal end of the transition region to the tip. When the aircraft wing () is under the worst-case static loading, the tip of the winglet is located at the maximum spanwise extent of the winglet (), but when the aircraft wing () is under the no-load condition, the wing-like region () is canted inboard such that the tip () of the winglet () is located inboard of the maximum spanwise extent of the winglet.

Winglet and method of designing a winglet

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Bristol, United Kingdom

Kasidit Leoviriyakit