AIRCRAFT INTERIOR TRIM PANEL, AND AIRCRAFT FITTED WITH SUCH PANELS

AIRCRAFT INTERIOR TRIM PANEL, AND AIRCRAFT FITTED WITH SUCH PANELS

A trim panel (10) for the interior (11) of an aircraft (E), the panel having a multilayer structure and including an outer layer (12) made of material impervious to air, and which is positioned in use facing the fuselage of the aircraft (E); an inner layer (13) made of trim material, and which in us...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: PERAZZOLO, ALESSANDRO, SCAINI, SARA
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
LAYERED PRODUCTS
LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A trim panel (10) for the interior (11) of an aircraft (E), the panel having a multilayer structure and including an outer layer (12) made of material impervious to air, and which is positioned in use facing the fuselage of the aircraft (E); an inner layer (13) made of trim material, and which in use defines the interior (11); a structural layer (14) interposed between the inner and outer layer (13, 12); and acoustic energy dissipating material (17, 21), also interposed between the inner (13) and outer (12) layer; the inner layer (13) being made of porous material allowing airflow towards the acoustic energy dissipating material (17, 21).