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Polystyrene foam filling method for composite material honeycomb sandwich structure

A technology of honeycomb interlayer and composite material, applied in the field of composite material manufacturing, can solve the problems of not easy filling of styrofoam and overflow of styrofoam, and achieve the effects of convenient filling of styrofoam, avoidance of secondary foaming, and convenient cleaning.

Active Publication Date: 2021-05-25
AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

And in the traditional process, after pre-bonding, one side of the honeycomb core filling cavity is closed by the outer skin, and the air in the honeycomb core filling cavity is trapped in the process of filling the foaming glue, which makes it difficult for the foaming glue to be completely filled, and during the foaming process , the volume of the wrapped gas increases with the rise of temperature, causing the foam to overflow from the filling cavity of the honeycomb core

Method used

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  • Polystyrene foam filling method for composite material honeycomb sandwich structure

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Embodiment Construction

[0026] Embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings and examples. The detailed description and accompanying drawings of the following embodiments are used to illustrate the principles of the present invention, but cannot be used to limit the scope of the present invention, that is, the present invention is not limited to the described embodiments, without departing from the spirit of the present invention Any modification, substitution and improvement of parts, components and connection methods are covered under.

[0027] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0028] figure 1 Shown is the styrofoam filling method that is used for composite material honey...

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Abstract

The invention relates to a polystyrene foam filling method for a composite material honeycomb sandwich structure. The polystyrene foam filling method comprises the following steps of paving a layer of strip-shaped polystyrene foam on the die-attaching side of a honeycomb core, heating and extruding the strip-shaped polystyrene foam into a filling cavity of the honeycomb core, and paving a single-layer isolating membrane between the honeycomb core and a die; filling the non-die-attaching side of the honeycomb core with powdery polystyrene foam, and laying multiple layers of isolating membranes; and putting a forming die into curing forming equipment for heating and curing the polystyrene foam. According to the polystyrene foam filling method for the composite material honeycomb sandwich structure, residual stress generated by curing shrinkage of the polystyrene foam due to the fact that a composite material honeycomb sandwich structure workpiece is subjected to the procedures of pre-bonding and foaming in sequence, only the foaming face on one side is bound, and the other side is not bound can be eliminated; air wrapping in the filling cavity of the honeycomb core in the polystyrene foam filling process is avoided, and the filling quality and efficiency are improved; and the honeycomb core is independently formed, a pre-bonding process is cancelled, and the manufacturing cost of the composite material honeycomb sandwich structure is reduced.

Description

technical field [0001] The invention relates to the technical field of composite material manufacturing, in particular to a foam filling method for a composite material honeycomb sandwich structure. Background technique [0002] Composite honeycomb sandwich structure is a structural form with high specific stiffness performance, which is widely used in aerospace vehicle structures. In the honeycomb sandwich structure of composite materials, it is often necessary to fill the honeycomb core of the nail area with foam glue for assembly requirements. The traditional molding process usually adopts the pre-adhesion of the cured outer skin and the honeycomb core, and then fills the honeycomb core with foam glue to cure the foam glue, and finally glues it to the inner skin. Since the outer skin is pre-bonded with the honeycomb, the structural asymmetry will cause the part to bend toward the pre-bonded honeycomb side, and the deformation will often be corrected during the bonding pr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C44/12B29C44/34B29C44/60
CPCB29C44/12B29C44/34B29C44/3415B29C44/3403B29C44/60
Inventor 何可馨苏震宇邱启艳
Owner AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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