APPLICATION OF INSULATING COATING
First Claim
Patent Images
1. A method for mitigating electrical surface discharges, comprising:
- applying an insulating primer to a metallic component; and
applying an insulating primer discontinuously to a carbon fiber reinforced plastic (CFRP) component adjacent the metallic component to form a plurality of primed portions and at least one unprimed portion,wherein the at least one unprimed portion is configured to enable electrostatic dissipation.
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Abstract
Systems and methods for discontinuously applying an insulating primer to a carbon fiber reinforced plastic (CFRP) component are disclosed. In one embodiment, a method for mitigating electrical surface discharges from a CFRP component includes first applying an insulating primer to a metallic component. Next, an insulating primer is applied discontinuously to the CFRP component adjacent the metallic component. The discontinuous application of the insulating primer forms a primed portions and unprimed portions. The unprimed portions are configured to enable electrostatic dissipation.
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Citations
20 Claims
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1. A method for mitigating electrical surface discharges, comprising:
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applying an insulating primer to a metallic component; and applying an insulating primer discontinuously to a carbon fiber reinforced plastic (CFRP) component adjacent the metallic component to form a plurality of primed portions and at least one unprimed portion, wherein the at least one unprimed portion is configured to enable electrostatic dissipation. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method for mitigating electrical surface discharges, comprising:
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applying an insulating primer to a metallic component; providing one or more electrostatically dissipative features to a carbon fiber reinforced plastic (CFRP) component adjacent the metallic component; and applying an insulating primer discontinuously to the CFRP component to form at least one primed portion and at least one unprimed portion, the at least one primed portion being disposed adjacent the electrostatically dissipative features, wherein the insulating primer is configured to at least prevent galvanic corrosion of the metallic component. - View Dependent Claims (12, 13, 14, 15, 16, 17)
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18. An aircraft comprising:
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a fuselage; a wing operatively coupled to the fuselage; a metallic component disposed inside at least one of the fuselage and the wing; a carbon fiber reinforced plastic (CFRP) component disposed adjacent the metallic component; and an insulating primer disposed discontinuously on the fuel containment surface to form a plurality of primed portions and at least one unprimed portion, wherein the at least one unprimed portions is configured to enable electrostatic dissipation. - View Dependent Claims (19, 20)
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Specification