FIELD: antenna technology.
SUBSTANCE: proposed antenna fairing, which includes a ceramic shell connected by an internal and end surfaces with an elastic heat-resistant adhesive-sealant with a frame, consisting of a metal transitional frame, matched according to TCLE with the shell material, a metal butt ring and a transitional ring installed in the annular groove of the rear end frame of the sealing ring, characterized in that the design of the frame is a bayonet connection of a closed type, in which the parts of the frame are connected to each other telescopically by axial movement and rotation of the bayonet teeth of the frame of the transitional relative to the bayonet teeth of the butt ring with filling gaps and voids with elastic adhesive-sealant, at that, the end surface of the shell, by means of adhesive-sealant, rests on a solid annular butt element of the frame.
EFFECT: increase in the bearing capacity of the structure under conditions of increased thermal and power loading while simultaneously ensuring a given level of tightness.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTENNA FAIRING FOR HIGH-SPEED MISSILES | 2020 |
|
RU2733916C1 |
ANTENNA FAIRING | 2020 |
|
RU2735381C1 |
CONE | 2002 |
|
RU2225664C2 |
ANTENNA DOME | 2011 |
|
RU2464679C1 |
HEAD ANTENNA DOME | 2016 |
|
RU2631917C1 |
FAIRING | 2017 |
|
RU2654953C1 |
ANTENNA DOME | 2012 |
|
RU2494504C1 |
ANTENNA FAIRING | 2018 |
|
RU2690040C1 |
ANTENNA NOSE FAIRING | 2004 |
|
RU2273077C1 |
FAIRING | 2017 |
|
RU2650085C1 |
Authors
Dates
2023-03-31—Published
2022-06-03—Filed