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Active and passive radar seeker radome and aircraft

A technology of radar seeker and aircraft, applied in the direction of antenna and radiation unit cover suitable for movable objects, to achieve the effect of high integration, good heat resistance and wave transmission performance, simple and compact structure

Active Publication Date: 2021-08-03
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

How to realize the radome design of the active and passive composite seeker, and meet the requirements of heat protection, wave penetration, load bearing and light weight at the same time, is very difficult to design

Method used

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  • Active and passive radar seeker radome and aircraft
  • Active and passive radar seeker radome and aircraft
  • Active and passive radar seeker radome and aircraft

Examples

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Embodiment Construction

[0042] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0043] see Figure 1 to Figure 3 As shown, the embodiment of the present invention provides an active and passive radar seeker radome, which includes a cover body 1 , a casing 2 , a heat shield 3 and a heat insulation layer 4 .

[0044] Wherein, the casing 2 is fixed inside the cover body 1 , and the casing 2 includes a front frame 21 and a rear frame 22 arranged at intervals, and a compartment for fixing the passive antenna 7 is arranged between the front frame 21 and the rear frame 22 .

[0045] The heat shield 3 is located in the cover body 1 and fixed on the front frame 21 .

[0046] The heat insulation layer 4 is attached between the inner side of the cover body 1 and the outer side of the casing 2 .

[0047] In this embodiment, the cover body 1 and the heat shield 3 are used to jointly realize the heat protection and wave transmission ...

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Abstract

The invention discloses an active and passive radar seeker radome and an aircraft, and relates to the field of aircraft radome, comprising: an enclosure; a shell, which is fixed inside the enclosure, and the shell includes a front frame and a rear frame arranged at intervals, A cabin section for fixing the passive antenna is provided between the front frame and the rear frame; the heat shield is located in the cover and fixed on the front frame; and the heat insulation layer is attached to the inside of the cover and the shell. between the outer sides. The active and passive radar seeker radome in the invention can realize heat protection, wave penetration, conformal installation of the antenna array and the radome, and vibration reduction installation of the active seeker.

Description

technical field [0001] The invention relates to the field of aircraft radome, in particular to an active and passive radar seeker radome and an aircraft. Background technique [0002] Aircraft often fly at high speed in harsh thermal and mechanical environments. In order to ensure the normal operation of the seeker and maintain the aerodynamic shape, it is necessary to design a radome outside the seeker. The radome needs to meet the functions of wave transmission, load bearing and heat protection at the same time. The structural design of the radome is the focus and difficulty of the aircraft structural design. [0003] According to different use environments, choose different materials to design the radome cover body. Generally speaking, resin-based composite materials can be selected for environments with low thermal environment, such as glass fiber reinforced plastics, polytetrafluoroethylene-based composite materials, etc.; for harsh thermal environments It is necessary...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/42H01Q1/28
CPCH01Q1/28H01Q1/42
Inventor 刘庆石江波丁帅王松元陈伟吴敏
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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