METHOD AND APPARATUS FOR GROUNDING A COMPOSITE AIRCRAFT STRUCTURE
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United States of America Patent
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Issued Date -
Jan 26, 2012
app pub date -
Feb 3, 2011
filing date -
Jun 14, 2010
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Abandoned
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Abstract
Method and apparatus for installing a grounding fastener in a composite aircraft structure includes structure and/or function for (i) drilling a hole in the composite aircraft structure, the hole dimensioned to provide a clearance fit with respect to the composite structure and the grounding fastener; (ii) coating the grounding fastener with a conductive fluid; (iii) inserting the grounding fastener into the hole such that the grounding fastener is in electrical contact with conductive fibers within the composite structure; (iv) securing the grounding fastener to the composite structure; and (v) attaching a conductive device to the grounding fastener such that the conductive device is in electrical contact with the grounding fastener.
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