FIELD: radio engineering.
SUBSTANCE: invention relates to radio engineering, in particular to composite materials for heat-shielding coatings and antenna radomes installed on aircraft. The effect is achieved by the fact that the antenna heat-shielding multilayer insert containing radio-transparent heat-shielding first and second layers, the first layer is made of a material that retains its structural integrity and electrodynamic parameters in a given range of high temperatures, and the second is made of a material with low thermal conductivity, is characterized in that the first layer is external, and the second layer is internal, while the first layer retains its structural integrity at a heating temperature up to 2000°C and is made in the form of a cylinder having parts of large, small and medium diameters.
EFFECT: expansion of the operating temperature range, preservation of the integrity of the outer surface of the antenna inserts, reliable fastening of materials to each other into a single antenna heat-shielding multilayer insert.
1 cl, 1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| AUXILIARY HEAT SHIELD OF AIRBORNE ANTENNA IN HEAD ANTENNA FAIRING OF FLYING VEHICLE | 2004 | 
 | RU2277737C1 | 
| ANTENNA FAIRING | 2018 | 
 | RU2694132C1 | 
| ANTENNA DOME | 2013 | 
 | RU2536360C1 | 
| ANTENNA FAIRING | 2020 | 
 | RU2738428C1 | 
| ANTENNA FAIRING | 2017 | 
 | RU2662250C1 | 
| ANTENNA DOME | 2017 | 
 | RU2644621C1 | 
| ANTENNA FAIRING | 2018 | 
 | RU2679483C1 | 
| ANTENNA FAIRING | 2020 | 
 | RU2738430C1 | 
| ANTENNA DOME | 2017 | 
 | RU2659586C1 | 
| AERIAL FAIRING OF MISSILE | 2003 | 
 | RU2256262C1 | 
Authors
Dates
2023-02-01—Published
2022-04-28—Filed