Oppositely-opened folding carbon fiber cabin cover of large cabin body

Abstract

The invention discloses an oppositely-opened folding carbon fiber cabin cover of a large cabin body. The oppositely-opened folding carbon fiber cabin cover is characterized in that the oppositely-opened folding carbon fiber cabin cover is integrally molded by adopting a carbon fiber composite material and comprises a left cabin cover, a right cabin cover, hinge assemblies, cabin cover locking mechanisms, folding mechanisms and cover opening and closing mechanisms; the left cabin over and the right cabin cover each comprise an upper cabin cover and a lower cabin cover, the lower cabin covers are connected with the cabin body through the multiple groups of hinge assemblies, and the cover opening and closing mechanisms are arranged between the lower cabin covers and the cabin body and controlled to achieve cabin cover opening and closing; the upper cabin covers and the lower cabin covers are connected in a hinged mode and connected to the folding mechanisms correspondingly, and the folding mechanisms are controlled to achieve left cabin cover and right cabin cover folding; and the cabin cover locking mechanisms are arranged at the butt joints of the upper cabin covers of the left cabin cover and the right cabin cover. The cabin cover has the characteristics of oppositely-opened folding, radar concealment, bullet preventing and destruction resisting, electromagnetic shielding, small self weight, large load capacity, good thermal insulation properties, long life and the like.

Description

technical field [0001] The invention belongs to the field of hatch covers, and in particular relates to a split and foldable carbon fiber hatch cover for a large cabin body, which is used as the hatch cover of a thermal insulation cabin. Background technique [0002] At present, the hatch cover of the insulation cabin is a side opening cover (such as Figure 10 As shown), there is no split-folding hatch cover. The molding process used is skeleton welding and skin sticking riveting. Its strength design belongs to the "hard shell box" structure. The materials used are basically selected from aluminum plates and aluminum profiles as parts. Manufacturing materials cannot integrate features such as radar stealth, bulletproof and indestructible, electromagnetic shielding, light weight, and large load capacity. Contents of the invention [0003] Aiming at at least one of the above defects or improvement needs of the prior art, the present invention provides a large-scale cabin wi...

AI Technical Summary

Problems solved by technology

[0002] At present, the hatch cover of the insulation cabin is a side opening cover (such as Figure 10 As shown), there is no split-folding hatch cover. The molding process used is skeleton welding and skin sticking riveting. Its strength design belongs to the "hard shell box" structure. The materials used are basically selected from aluminum plates and aluminum profiles as parts. Manufacturing materials cannot integrate features such as radar stealth, bulletproof and indestructible, electromagnetic shielding, light weight, and large load capacity

Images