FIELD: aircraft and rocket equipment.
SUBSTANCE: invention relates to aircraft and rocket equipment and can be used in designing and designing antenna cowlings of promising highly maneuverable hypersonic missiles of various hull classes with shells from heat-resistant ceramic materials. Antenna fairing including ceramic shell connected by elastic adhesive with frame consisting of adapter made of metal matched TCLE with shell material, and titanium butt element, interconnected by pins and collars, and sealing elements, on cowl there is a shell from heat-resistant material with clearance relative to outer surfaces of ceramic shell, which together with belts from rubber-like heat-resistant material form a closed air cavity, characterized in that in cavity formed by inner shell surface and shell outer surface, transition element of heat-resistant fiber glass is installed, surface of contact with shell of which repeats shape of external surface of shell.
EFFECT: technical result consists in improvement of bearing capacity of structure, achieved by expansion of zone of redistribution of forces from ceramic shell to attached elements with simultaneous reduction of heating of internal elements with corresponding reduction of spacer interaction between dissimilar elements.
3 cl, 1 dwg
Title | Year | Author | Number |
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|
RU2464679C1 |
ANTENNA FAIRING FOR HIGH-SPEED MISSILES | 2020 |
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RU2742294C1 |
BLISTER | 2011 |
|
RU2451372C1 |
FAIRING | 2017 |
|
RU2654953C1 |
ANTENNA FAIRING | 2022 |
|
RU2793304C1 |
ANTENNA FAIRING | 2020 |
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RU2738430C1 |
ANTENNA FAIRING | 2018 |
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CONE | 2002 |
|
RU2225664C2 |
ANTENNA DOME | 2013 |
|
RU2536361C1 |
Authors
Dates
2020-10-30—Published
2020-04-24—Filed