| 摘要 |
FIELD: transport.SUBSTANCE: proposed device comprises multiple IR radiation elements 13, 13a, 13b arranged inside said leading edge 1 of aircraft air intake 3, radiator electric power supply 17 and power supply control means 27. Radiators are made of ceramics and feature the following parameters: radiation power-to-weight ratio approximating to 500 W per 100 g, radiation capacity approximating to 97% at 800°C making 1.5-10 mcm, radiation power surface density exceeding 70 kW/m, and efficiency exceeding 95%.EFFECT: ruled out removal of hot air from engine, compact design, ease of replacement, longer life, high radiation capacity, low thermal inertia.16 cl, 13 dwg |
