INTERIOR TRIM COMPONENT FOR AN AIRCRAFT CABIN
An interior trim component (10) for an aircraft cabin comprises a supporting structure which is formed by a first chamber system (12) which is sealable against the outside atmosphere. The first chamber system (12) forming the supporting structure is adapted to be loaded with an internal pressure whi...
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| Format: | Patent |
| Sprache: | eng ; fre |
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| Zusammenfassung: | An interior trim component (10) for an aircraft cabin comprises a supporting structure which is formed by a first chamber system (12) which is sealable against the outside atmosphere. The first chamber system (12) forming the supporting structure is adapted to be loaded with an internal pressure which is necessary for producing the desired structural load-bearing capacity of said supporting structure.
Cette invention concerne un élément de garniture intérieure (10) pour une cabine d'aéronef, lequel élément comprend une structure de support constituée d'un premier système de chambres (12) pouvant être isolé hermétiquement de l'atmosphère ambiant. Le premier système de chambre (12) formant la structure de support est conçu pour être chargé au moyen d'une pression interne nécessaire pour générer la force portante structurelle souhaitée de la structure de support. |
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