Front radome for aircraft

Abstract

The invention relates to the technical field of aviation structural parts, in particular to a front radome for an aircraft, which comprises an aircraft body, an outer dome body, an electric control hydraulic support rod and an inner mounting frame for mounting a radar. The front radome for the aircraft is fixedly connected with the front end of the aircraft body through the movable mounting bracket and the bottom limiting device, and the first reset spring and the lateral locking bolt are matched with each other, so that the number of external bolts is reduced, the invisibility is improved, later maintenance is facilitated, and the later use cost is greatly reduced; the electric control hydraulic supporting rod extrudes the elastic flow guide blades to turn over through the heat conduction copper plate, an inclined negative pressure turbulence mechanism is formed on the outer side of the lateral adjusting opening, the heat dissipation modes of the radome are more diverse, the heat dissipation effect is adjustable, the operation environment of the aviation radar is better, long-time efficient operation can be guaranteed conveniently, and the service life is prolonged.

Description

technical field [0001] The invention relates to the technical field of aeronautical structural parts, in particular to a front radome for an aircraft. Background technique [0002] Aviation radar refers to the general term of various radars installed on aviation aircraft. It is mainly used to control and guide weapons, implement air security and reconnaissance, and ensure accurate navigation and flight safety. The basic principle and composition of aviation radar are the same as other military radars, and its characteristics are: generally have antenna platform stabilization system or data stabilization device; usually use a band below 3 cm; small size, light weight; good shockproof performance. [0003] Traditional aeronautical radar is mainly installed at the front of the aircraft, inside the radome, and fixed by a built-in installation method. When the radar is used at full power, a large amount of heat energy will be generated. If it cannot be quickly discharged, it wil...

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is: in order to solve the problems existing in the above-mentioned background technology, an improved aircraft front radome is provided to solve the problem that the traditional radome used for installing aviation radar cannot quickly discharge internal heat, which will cause The heat gathers inside the radome, which not only easily affects the working efficiency of the aeronautical radar, but also leads to the attenuation of the service life of the aeronautical radar, and the loading and unloading of the radome is mainly controlled by the fixing bolts arranged in an external ring, and the loading and unloading operation is troublesome, resulting in The post-maintenance efficiency is not high and the cost is high

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