DISTRIBUTING POWER IN SYSTEMS HAVING A COMPOSITE STRUCTURE

A particular method includes exposing a plurality of fibers of a composite skin of an aircraft component by providing an opening in a layer of a first resin overlaying the plurality of fibers at an interior surface of the composite skin. The method also includes bonding a conductive patch in electri...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	ROBB, Andrew M
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS CURRENT COLLECTORS ELECTRICITY HELICOPTERS LINE CONNECTORS PERFORMING OPERATIONS TRANSPORTING
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