STRUCTURAL COMPONENT FOR AN AIRCRAFT

A structural component (2) for an aircraft comprises at least one heatable component portion (4), the heatable component portion (4) comprising a layered construction having an inner base structure (6), a first insulating layer (8) arranged outside the inner base structure (6), a functional layer (1...

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Bibliographische Detailangaben
Hauptverfasser:	KARCH, CHRISTIAN, BONACCURSO, ELMAR, LINDE, PETER
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS ELECTRIC HEATING ELECTRIC LIGHTING NOT OTHERWISE PROVIDED FOR ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A structural component (2) for an aircraft comprises at least one heatable component portion (4), the heatable component portion (4) comprising a layered construction having an inner base structure (6), a first insulating layer (8) arranged outside the inner base structure (6), a functional layer (10) of carbon allotropes embedded in a matrix material, which functional layer is arranged outside the first insulating layer (8), and at least one protective layer (16) arranged outside the functional layer (10). The structural component (2) further comprises an electrical connection device (12) connected to the functional layer (10) for selectively applying an electrical current to the functional layer (10) for heating the functional layer (10).