VACUUM INSULATION PANELS FOR AIRCRAFT INTERIORS
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...
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Format: | Patent |
Sprache: | eng ; fre |
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Zusammenfassung: | 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 oevre 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. |
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