DISTRIBUTING POWER IN SYSTEMS HAVING A COMPOSITE STRUCTURE

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

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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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Beschreibung
Zusammenfassung: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 electrical contact with the plurality of fibers of the composite skin at the opening using a second resin. The method further includes preparing the aircraft component to receive a connector in electrical contact with the conductive patch.