B - Operations – Transporting – 32 – B
Patent
B - Operations, Transporting
32
B
B32B 3/12 (2006.01) B64C 1/12 (2006.01) B64C 1/40 (2006.01) F16L 59/065 (2006.01)
Patent
CA 2649899
The invention relates to an aircraft side fairing, with a component (9) in the form of individual hollow chambers (12, 13, 14) which are arranged essentially in a preferably curved plane and are arranged between two cover layers (1, 2), wherein a gastight film which completely encases the component (9) with the hollow chambers (12, 13, 14) is provided and, after application of a vacuum to evacuate the hollow chambers (12, 13, 14), surrounds the component (9) with the hollow chambers in a gastight manner.
L'invention concerne un carénage latéral d'aéronef, ayant un composant (9) sous la forme de chambres creuses individuelles (12, 13, 14) qui sont arrangées essentiellement dans un plan de préférence courbe et qui sont arrangées entre deux couches de revêtement (1, 2), un film étanche aux gaz enfermant entièrement le composant (9) à chambres creuses (12, 13, 14) étant mis en AEuvre et, après l'application d'un vide pour évacuer les chambres creuses (12, 13, 14), entourant le composant (9) à chambres creuses d'une manière étanche aux gaz.
Muehlthaler Georg
Mueller Rainer
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
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