Abstract:In the field of aviation and aerospace, high-altitude low temperature environments have a significant impact on the performance of high-pressure gas cylinders in aircraft-mounted pressure actuation systems. This leads to internal pressure decreases in the gas cylinders, which poses risks to the normal operation of aircraft actuator components. This study presents a novel design of a rapid heating device based on Graphene-skinned Glass Fiber (GSGF). By optimizing the three-electrode layout and innovating the design of a 3-mm aerogel thermal insulation layer, the challenges of heating efficiency and uniformity have been addressed. Based on the heat flux density calculation (power density of 0.8 W/cm2) and temperature field simulation by ANSYS Fluent, combined with the experimental verification under the -55℃ working condition, the results show that the device can heat a single gas cylinder from -55℃ to 25℃ in 6 minutes and 58 seconds, with the electro-thermal conversion efficiency reaching 94.2% and the heat loss reduced to 30 W. This scheme provides an efficient solution for the stable operation of high-pressure gas cylinders in low-temperature environments and has significant application value in aerospace and polar equipment fields.