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Cover antenna integrated device

An antenna and cover technology, which is applied in the field of aircraft antenna structure design, achieves the effect of solving installation and maintenance problems and facilitating disassembly and assembly

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

AI Technical Summary

Problems solved by technology

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

Method used

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  • Cover antenna integrated device

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Embodiment Construction

[0012] 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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Abstract

The invention relates to airplane antenna structure design, in particular to a cover antenna integrated device which comprises an antenna, a cover and a supporting rod. A grating is arranged inside the cover, the antenna comprises multiple antenna oscillators, the supporting rod is fixed on one side face of the grating, and the antenna oscillators are detachably and fixedly arranged on the supporting rod along the axis direction of the supporting rod and perpendicular to the side face of the grating. Multiple antenna oscillators of the antenna are fixedly arranged on the supporting rod in thecover in an individually demountable manner, so that mounting and demounting is more convenient, and the problems of mounting and maintaining of antennas in semi-closed space are solved.

Description

technical field [0001] The invention relates to the structural design of an aircraft antenna, in particular to a cover antenna integration device. 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 a cover antenna integrated device to solve at least one problem existing in the installation of the existing aircraft antenna. [0004] Technical scheme of the present invention is: [0005] A cover-antenna integration device, comprising an antenna and a cover, the cover has a grid inside, the antenna includes a plurality of antenna vibrators, and the cover-antenna integration device further includes: [0006] A support rod is fixed on one...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q1/42H01Q1/12
CPCH01Q1/42H01Q1/12
Inventor 余磊王晓辉伍小亮李厚顺
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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