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Active conformal array antenna applied to unmanned aerial vehicle platform

A conformal array, unmanned aerial vehicle technology, applied to antennas, antenna unit combinations with different polarization directions, antenna supports/installation devices, etc. The effect of small space, meeting aerodynamic requirements and maintaining low profile characteristics

Inactive Publication Date: 2018-05-15
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to overcome the disadvantages of the prior art that occupy a large space and be susceptible to electromagnetic interference, and provide an active conformal array antenna applied to the UAV platform

Method used

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  • Active conformal array antenna applied to unmanned aerial vehicle platform
  • Active conformal array antenna applied to unmanned aerial vehicle platform
  • Active conformal array antenna applied to unmanned aerial vehicle platform

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Embodiment Construction

[0033] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0034] Such as Figure 1-4As shown, this embodiment takes an active conformal array antenna working at 8-11GHz as an example, and the array size is taken as 8×8, which specifically includes the fuselage skin (not shown in the figure), antenna array 1, multiple Functional board 2 and tiled TR assembly 3 .

[0035] The antenna front 1 includes an antenna patch unit 11, an antenna radiation layer 12, a thermal control and support layer 13, and an SMP blind matching hole 14. The antenna patch unit 11 conforms to the structure of the fuselage skin, and the antenna array Surface 1 uses SMP blind-mating connectors to pa...

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PUM

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Abstract

The invention discloses an active conformal array antenna applied to an unmanned aerial vehicle platform, and sequentially comprises an antenna array surface, a body skin, a multifunctional board, anda tile-type TR assembly that are integrated and conformal from the outside to the inside, a patch is adopted as a radiation unit on the antenna array surface and is conformal with the structure of the body skin, wherein the antenna array surface comprises an antenna radiation layer, and a thermal control and support layer which are sequentially arranged from the outside to the inside, the antennaarray surface adopts an SMP blind matching connector to penetrate through the thermal control and support layer and the multifunctional board to be connected with the tile-type TR component. According to the invention, the integrated integration of the active module, the antenna array and the body skin is realized by combining rigid and flexible printed boards, the defects that a traditional design cannot realize the integrated integration of the active module and the body are overcome, and meanwhile, the occupied space is small, the anti-electromagnetic interference resistance is strong, andthe aerodynamic requirements of the aircraft is met.

Description

technical field [0001] The invention relates to the technical field of radar antennas, in particular to an active conformal array antenna applied to an unmanned aerial vehicle platform. Background technique [0002] A large number of single-function antennas are used on modern aircraft, which are installed around the aircraft. They mainly serve electronic equipment such as radars, electronic warfare receivers, jammers, missile incoming warning equipment, navigation equipment, and radar altimeters. These antennas are generally distributed in The aircraft head, above or below the front, and covered with a radome. With the development of future aircraft in the direction of miniaturization, light weight, and unmanned, the requirements for the volume, weight, and performance of electronic systems are becoming more and more stringent, especially for airborne, spaceborne, and various weapon systems. The required electronic components and components are developing rapidly in the di...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q1/22H01Q1/38H01Q21/24H01Q23/00
CPCH01Q21/24H01Q1/22H01Q1/38H01Q23/00
Inventor 张德智何朝升郑林华陈文兰郭琳郭崇颖
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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