Composite material cover body and antenna integration device

A composite material cover and antenna technology, applied in the direction of antenna support/installation device, antenna, antenna parts, etc., to achieve the effect of easy disassembly and assembly, and solve the problems of installation and maintenance

Inactive Publication Date: 2019-02-12
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The object of the present invention is to provide an integrated device of composite cover and antenna to solve at least one problem existing in the installation of the existing aircraft antenna

Method used

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  • Composite material cover body and antenna integration device

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Embodiment Construction

[0013] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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PUM

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Abstract

The invention relates to an aircraft antenna structure design, in particular to a composite material cover body and antenna integration device. The composite material cover body and antenna integration device comprises an antenna and a cover body, wherein the cover body internally has a grille; the antenna comprises multiple antenna vibrators and a support rod arranged on one side surface of the grille in a sliding manner; the multiple antenna vibrators are arranged on the support rod along the axial direction of the support rod; and the antenna vibrators are perpendicular to the side surfaceof the grille. According to the composite material cover body and antenna integration device disclosed by the invention, the support rod fixedly provided with the antenna vibrators is arranged on thegrille in the cover body in the sliding manner, thereby facilitating assembling and disassembling and solving the problem on installation and maintenance of the antenna in a semi-closed space.

Description

technical field [0001] The invention relates to the structural design of an aircraft antenna, in particular to an integrated device for a composite cover and an antenna. Background technique [0002] The installation of traditional antennas in the enclosure requires mounting brackets. However, the enclosure is usually a semi-enclosed space, and the installation of the antenna requires sufficient operating space, and the antenna is heavy, making maintenance very inconvenient. Contents of the invention [0003] The object of the present invention is to provide an integrated device of composite cover and antenna to solve at least one problem existing in the installation of the existing aircraft antenna. [0004] Technical scheme of the present invention is: [0005] An integrated device for a composite cover and an antenna, including an antenna and a cover, the cover has a grid inside, the antenna includes a plurality of antenna vibrators, and the integrated device for a com...

Claims

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Application Information

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IPC IPC(8): H01Q1/42H01Q1/12H01Q1/22
CPCH01Q1/42H01Q1/1242H01Q1/22
Inventor 余磊李厚顺王晓辉伍小亮
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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