AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN
Aircraft window with variable power density heater film
Aircraft Window with Variable Power Density Heater Film
AN ELECTRIC CIRCUIT AND SENSOR FOR DETECTING ARCING AND A TRANSPARENCY HAVING THE CIRCUIT AND SENSOR
AN ELECTRIC CIRCUIT AND SENSOR FOR DETECTING ARCING AND A TRANSPARENCY HAVING THE CIRCUIT AND SENSOR
COATING INCLUDING ELECTRICALLY CONDUCTIVE LINES DIRECTLY ON ELECTRICALLY CONDUCTIVE LAYER
Coating including electrically conductive lines directly on electrically conductive layer
COATING SYSTEMS, FILMS, AND ARTICLES FOR RADAR TRANSMISSION, METHODS OF MANUFACTURE AND USE THEREOF
COATING SYSTEMS, FILMS, AND ARTICLES FOR RADAR TRANSMISSION, METHODS OF MANUFACTURE AND USE THEREOF
Electric circuit and sensor for detecting arcing and a transparency having the circuit and sensor
METHOD OF APPLYING AN ELECTRIC CONDUCTIVE LAYER TO SELECTED PORTIONS OF A MOUNTING FRAME
Outboard durable transparent conductive coating on aircraft canopy
OUTBOARD DURABLE TRANSPARENT CONDUCTIVE COATING ON AIRCRAFT CANOPY
OUTBOARD DURABLE TRANSPARENT CONDUCTIVE COATING ON AIRCRAFT CANOPY
SYSTEM AND METHOD FOR LIFE PREDICTION OF A RESISTIVE COATING