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A composite material pressure-resistant structure rectome and its manufacturing method

A pressure-resistant structure and rectifying antenna technology, applied in the direction of the radiation unit cover, can solve the problems of low reliability, short service life, poor water pressure resistance of the cover layer, etc., to improve the pressure bearing capacity and sealing performance, increase Large safety factor and reliability, and the effect of improving corrosion resistance

Active Publication Date: 2020-04-24
HARBIN TOPFRP COMPOSITE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims to solve the problems of heavy radome of existing submersibles, low precision of streamlined curved surface, poor corrosion resistance and low reliability of the bolt connection of the cover body, poor water pressure resistance between layers of the cover body, and short service life. Now provide a composite material pressure-resistant structure radome and its manufacturing method

Method used

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  • A composite material pressure-resistant structure rectome and its manufacturing method
  • A composite material pressure-resistant structure rectome and its manufacturing method
  • A composite material pressure-resistant structure rectome and its manufacturing method

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specific Embodiment approach 1

[0045] Specific implementation mode one: refer to Figure 1 to Figure 3 Specifically explaining this embodiment, a composite material pressure-resistant structure rectenome 1 described in this embodiment includes a housing 11, a supporting structure 12 and a fixing structure 13,

[0046] The shell 11 is a streamlined curved surface end cover structure, and the open end of the shell 11 is sealed with the bow surface of the submersible 2,

[0047] The support structure 12 is trumpet-shaped, the large end of the support structure 12 is fixedly connected to the inner surface of the shell 11, and the small end of the support structure 12 is fixedly connected to the bow surface of the submersible 2,

[0048] The fixed structural member 13 is ring-shaped, and the outer circumference of the fixed structural member 13 is fixedly connected with the inner wall of the supporting structural member 12,

[0049] The angle range between the side wall of the support structure 12 and the centr...

specific Embodiment approach 2

[0053] Specific embodiment 2: This embodiment is a further description of a composite material pressure-resistant structure rectenome described in specific embodiment 1. In this embodiment, the side wall of the supporting structure 12 is the abdomen of the supporting structure 12. plate 22, a wing plate 21 is respectively fixed at both ends of the supporting structure 12,

[0054] The wing plate 21 located at the large end of the web 22 is trumpet-shaped, and the wing plate 21 located at the small end of the web 22 is circular.

specific Embodiment approach 3

[0055] Specific implementation mode three: refer to Figure 4 Describe this embodiment in detail. This embodiment is a further description of a composite material pressure-resistant structure rectenome described in Embodiment 1. In this embodiment, the outer shell 11, the supporting structure 12 and the fixed structure 13 The structure of the material layer is the same, and the material layer is the outer surface layer, the outer surface isolation layer 105, the structural layer 104, the inner surface isolation layer 103, and the inner surface layer from the outside to the inside.

[0056] The outer surface layer from the outside to the inside is the outer surface anti-aging layer 107, the outer surface short fiber layer 106,

[0057] The inner surface layer is the inner surface short fiber layer 102 and the inner surface anti-aging layer 101 sequentially from outside to inside.

[0058] In this embodiment, the materials of the shell 11 , the supporting structure 12 and the f...

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Abstract

The invention, which relates to the fields of a sneaking device antenna dome and a manufacturing method thereof, provides a composite-material pressure-resistant-structure rectifying antenna dome and a manufacturing method thereof, so that problems of large antenna dome weight, poor streamline type curved surface precision, poor anti-corrosion performance of dome and bolt connection, low reliability, poor interlamination water-pressure-resistant performance of dome body, and short service life can be solved. A housing has a streamline type curved-surface end cover structure; and an opening end of the housing is connected with a stem surface of a sneaking device in a sealing manner. A support structural member is in a horn shape; a large end of the support structural member is fixedly connected with the inner surface of the housing; and a small end of the support structural member is fixedly connected with the stem surface of the sneaking device. A fixed structural member is in annular shape; the external circumference of the fixed structural member is fixedly connected with the inner wall of the support structural member; the range of the included angle between the side wall of the support structural member and the centre shaft of the housing is from 40 degrees to 45 degrees; and the support structural member and the fixed structural member are arranged in an integrated manner. The composite-material pressure-resistant-structure rectifying antenna dome and manufacturing method thereof can be applied to the manufacturing field of the sneaking device antenna dome.

Description

technical field [0001] The invention belongs to the field of a submersible radome and a manufacturing method thereof. Background technique [0002] At present, with the survey of deep-sea resources and the needs of military use, the detection depth of the submersible is getting deeper and deeper, the cruising speed is getting faster and faster, and the overall performance requirements are getting higher and higher. The antenna shield installed on the submersible In terms of shape, it not only needs to perform the function of drag reduction and rectification, but also needs to meet the wave-transparency performance requirements of the antenna. [0003] The radome of existing submersible mostly is that metal alloy frame and radome shell are formed by screwing, and this kind of product weight is bigger. The radome shell and metal frame need to be released from the mold for subsequent assembly. Due to the poor rigidity of the radome shell itself, it is easy to deform after it i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/42B29C70/30B29C70/34
CPCB29C70/30B29C70/342H01Q1/42
Inventor 梅延宁孙东岩孙宝华王贵军林敏唐亮孟松于福斌
Owner HARBIN TOPFRP COMPOSITE