Circuit joining assembly materials for multi-layer lightning protection systems on composite aircraft
An exemplary embodiment provides a multi-layer circuit joining assembly material configured to repair multi-layer flex circuits deployed on or in a composite surface as a lightning protection system. The multi-layer circuit joining assembly material includes a first conductive layer having a first end portion, a second conductive layer having a second end portion, and a dielectric material between the first conductive layer and the second conductive layer.
1. A lightning protection system for a composite structure, the system comprising:
a lightning protection article including first and second metallic circuits separated by a polymeric film, the article having a damaged portion that defines first and second opposing edges, the metallic circuits patterned to divert lightning current; and
a repair connector including a first conductive layer for bridging the first and second edges of the first metallic circuit, a second conductive layer for bridging the first and second edges of the second metallic circuit, and a strip of dielectric material between the first and second conductive layers for electrically isolating a central portion of the first conductive layer from a central portion of the second conductive layer.
2. The system of claim 1 , wherein a perimeter region of the first conductive layer and the second conductive layer is configured to register with a stepped-layer perimeter of the damaged portion of the lightning protection article.
3. An aircraft component including a composite structure and the lightning protection system of claim 1 on the composite structure.
4. An aircraft comprising a composite structure having metal fasteners, and the lightning protection system of claim 1 , the metallic circuits configured to divert lightning current away from the metal fasteners.
5. The system of claim 1 , wherein each metallic circuit is also patterned with a plurality of conductive paths to provide connectivity for multi-function apparatus.
6. A lightning protection system for a composite structure comprising a first lightning protection article including first and second metallic circuits separated by a polymeric film; and a second lightning protection article including first and second metallic circuits separated by a polymeric film, the metallic circuits configured to divert lightning current; the system further comprising a connector consisting of a first conductive layer for joining the first metallic circuits; a second conductive layer for joining the second metallic circuits; and a strip of dielectric material electrically isolating a central portion of the first conductive layer from a central portion of the second conductive layer; wherein the first and second conductive layers are coextensive and wherein the dielectric strip extends transversely across a central portion of both layers to give the connector a substantially H-shape.
7. The system of claim 6 , wherein each metallic circuit is also patterned with a plurality of conductive paths to provide connectivity for multi-function apparatus.
8. An aircraft component including a composite structure and the lightning protection system of claim 6 on the composite structure.
9. An aircraft comprising a composite structure having metal fasteners, and the lightning protection system of claim 6 , the metallic circuits configured to divert lightning current away from the metal fasteners.