Aircraft wing with electrothermal deicing and/or anti-icing device

An aircraft wing comprising a structural member forming the wing's leading edge skin, a Kreuger flap which moves relative to the structural member between a stowed position and a deployed position, and an electrothermal device mounted (e.g., internally mounted) to the structural member. An aft...

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Bibliographische Detailangaben

1. Verfasser:	Giamati, Michael J
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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