A foam mount of an aircraft window has a groove to receive an electro chromic window. The foam mount is painted by placing a blank in the groove to divide the foam mount into a first section designated to face the exterior of the aircraft and an opposite second section. The foam mount having the blank is placed in a mask or masking device to coat one section of the foam mount while covering the other section. The groove and the first section are coated with an electric conductive paint, and the second section is covered with a decorative paint. The conductive coating on the foam mount and the conductive coating of the electrodes of the electro chromic window provide an RF shielding to prevent electronic signals from personal electronic equipment from passing through the cabin and door windows of the aircraft.
METHOD OF APPLYING AN ELECTRIC CONDUCTIVE LAYER TO SELECTED PORTIONS OF A MOUNTING FRAME
VERFAHREN ZUM AUFBRINGEN EINER ELEKTRISCH LEITFÄHIGEN SCHICHT AUF GEWÄHLTE TEILE EINES ANBRINGRAHMENS
PROCÉDÉ D'APPLICATION D'UNE COUCHE CONDUCTRICE DE L'ÉLECTRICITÉ SUR DES PARTIES CHOISIES D'UN ENCRADREMENT DE MONTAGE
2018-08-29
Patent
Electronic Resource
English
Electric drive mounting method and electric drive mounting preassembled frame
European Patent Office | 2021
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