Preparation device of fiber reinforced composite material honeycomb core material
A composite material and fiber-reinforced technology, which is applied in the field of preparation devices for fiber-reinforced composite honeycomb core materials, can solve the problems of poor interfacial properties of honeycomb core materials, difficult operation, lack of transverse curing pressure, etc., and achieve excellent interface properties.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0085] Such as figure 1 and Figure 11 As shown, using the whole set of preparation equipment, according to the above-mentioned process flow of assembly-curing-demolding-post-processing-pasting panels, the preparation of semi-recessed hexagonal honeycomb sandwich structures of fiber reinforced composite materials in three different directions can be completed.
Embodiment 2
[0087] Such as Figure 12 shown in Figure 9 (j) In the ninth step, the square positioning molds 7 on both sides are disassembled, and then a single-layer or multi-layer fiber prepreg rectangular strip 14 is laid on one side of the thin panel 9, and the sizing mold and positioning mold assembled in the middle are assembled. The mold is in direct contact with the fiber prepreg rectangular strip 14, and then an in-plane pressure in the X direction is applied to the overall positioning mold and shaping mold to compress the semi-concave hexagonal honeycomb structure preform 1 covered by the fiber prepreg And keep some pressure. When the distance between the two thin side plates reaches the structural design requirements, the pressurization is stopped. After curing and demoulding, an X-direction fiber-reinforced composite honeycomb sandwich structure 18 integrally formed by co-curing of the face plate and the core material can be obtained. Compared with the fiber-reinforced comp...
Embodiment 3
[0090] Through the improvement of the positioning base plate 2, in-plane pressurization devices are added on both sides of the Y direction to complete the in-plane X-direction and Y-direction bidirectional pressurization, and the preparation of the multi-layer fiber reinforced composite honeycomb sandwich structure can be completed.
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


