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An integrated structure of a nose skin antenna and a manufacturing method thereof

A skin and antenna technology, which is applied to the structural connection of the antenna grounding switch, antenna, and antenna components, etc., can solve problems such as affecting the detection accuracy of the system and increasing the difficulty of the telecommunication correction and compensation system, so as to reduce the weight of the installation structure and improve the power. Effect

Active Publication Date: 2018-12-21
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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  • Description
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AI Technical Summary

Problems solved by technology

[0008] The deformation of the antenna microstrip will cause the distortion of the front to affect the detection accuracy of the system and increase the difficulty of the telecommunication correction and compensation system. Therefore, ensuring the positioning accuracy of the antenna microstrip is the key to the success of the entire load structure integration scheme.

Method used

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  • An integrated structure of a nose skin antenna and a manufacturing method thereof

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Embodiment Construction

[0030] 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.

[0031] Such as figure 1 As shown, the production process of this embodiment is as follows:

[0032] (1) Carry out three-dimensional modeling on the skin of the nose, and determine the position of the positioning hole of the antenna microstrip 1;

[0033] (2) Before the antenna microstrip 1 is installed, the second skin 3 is cut out, and the center line of the cutting position is the position of the positioning hole of the antenna microstrip 1;

[0034] (3) Lay the second skin 3 layers, the first skin 2 five layers, the fourth skin 5 three layers, each skin and the junction of the transition plate 6 do not have ai...

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Abstract

The invention discloses an integrated structure of a nose skin antenna and a manufacturing method thereof, comprising a nose skin, an antenna microstrip, a transition plate and an SMA connector. The nose skin comprises a first skin, a second skin, a third skin and a fourth skin, wherein the first skin is positioned on one side of the transition plate, the fourth skin is positioned on the other side of the transition plate, the second skin is wrapped outside the first skin, the antenna microstrip is embedded in the first skin, the third skin is positioned on both ends of the transition plate, and the transition plate is positioned on the back surface of the antenna microstrip; the SMA connector passes through a fourth skin, a transition plate, and the antenna microstrip is welded on the antenna microstrip after the antenna microstrip is welded. The invention realizes the integrated design of the antenna microstrip and the head skin, controls the antenna shape through the shape of the head skin, effectively reduces the mounting structure weight of the antenna microstrip, realizes the fusion of the antenna microstrip and the head skin, and improves the power of the detection system.

Description

technical field [0001] The invention relates to a method for installing and designing an aircraft nose conformal antenna, in particular to an integrated structure and a manufacturing method of an aircraft nose skin antenna. Background technique [0002] In the five-dimensional war of "land, sea, air, sky, and electricity" under modern high-tech conditions, UAVs are widely used. They can not only perform various non-lethal tasks, but also perform various soft, Hard kill missions, including battlefield reconnaissance, surveillance, patrol, electronic reconnaissance, mine detection, anti-nuclear, biological and chemical detection, communication, electronic jamming, combat assessment, radar decoy, artillery fire calibration, laser guidance, target designation, anti-armor, anti-radiation and Anti-ship and other integrated sensor unmanned early warning aircraft systems can make full use of resources such as platform load, power consumption, and space to maximize the performance of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01Q1/42H01Q1/50
CPCH01Q1/42H01Q1/427H01Q1/50
Inventor 郭崇颖李岩张新苗郭琳强云飞
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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