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
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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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