Manufacturing method of composite material cabin door of foam sandwich structure

A technology of composite material and sandwich structure, which is applied in the field of manufacturing composite hatch doors with foam sandwich structure, can solve the problems of no foam sandwich, high manufacturing and installation costs, complicated operation of molding methods, etc., and achieve stable shape and size, The effect of low manufacturing and installation costs and strong designability

Inactive Publication Date: 2017-06-20
AVIC COMPOSITES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Foam materials have excellent thermal insulation properties and have the function of sound insulation and noise reduction. They can not only effectively reduce weight and improve the rigidity of the product, but also realize the function of thermal insulation and noise reduction. However, there is no foam sandwich structure composite material hatch in the prior art. , in the prior art, the outer surface smoothness, thermal insulation performance, damping and noise reduction performance, corrosion resistance and fatigue resistance performance all need to be improved, the molding method is complicated to operate, and the manufacturing and installation costs are high

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] A method for manufacturing a foam sandwich structure composite material hatch, comprising the following steps, the first step is to design and optimize the overall structure and layup of the hatch; the second step is to complete the design and manufacture of the mold; the third step , select the fiber cloth and cut the material according to the size and demand of the actual product; the fourth step is to select the foam material and embedded parts, cut the foam material into thin plates and punch holes in the thin plates; The skin cloth, the foam core, the embedded parts and the inner skin cloth are laid to complete the preparation of the prefabricated body; the sixth step is to lay the release cloth, the flow guide net and the glue injection support on the inner skin cloth in sequence; Seven steps, fix the air duct around the prefabricated body, spread the sealing tape and vacuum bag film, connect the exhaust pipe and carry out process combination, vacuumize at room tem...

Embodiment 2

[0033] A method for manufacturing a foam sandwich structure composite material hatch, comprising the following steps, the first step is to design and optimize the overall structure and layup of the hatch; the second step is to complete the design and manufacture of the mold; the third step , select the fiber cloth and cut it according to the size and demand of the actual product. The fiber can be any one or several composites of glass fiber, carbon fiber, aramid fiber, basalt fiber, and natural plant fiber. The state of the fiber material It is in the form of unidirectional yarn or fabric; the fourth step is to select the foam material and embedded parts, cut the foam material into a thin plate and punch holes in the thin plate, the thickness of the cut plate is 5-20mm, and the interval of the through holes It is 50-100mm, and described foam is any one in polyurethane foam, polyvinyl chloride foam, polystyrene foam, epoxy foam and PMI foam; The 5th step, outer skin cloth and fo...

Embodiment 3

[0035] A method for manufacturing a foam sandwich structure composite material hatch, comprising the following steps, the first step is to design and optimize the overall structure and layup of the hatch; the second step is to complete the design and manufacture of the mold; the third step , select the glass fiber cloth and cut it according to the size and demand of the actual product. Thin plate and make holes on the thin plate. The thickness of the cut thin plate is 5mm, and the interval of the through holes is 50mm; the fifth step is to lay or lay the outer skin cloth, foam core, embedded parts and inner skin cloth on the mold Fixing, one layer of outer skin cloth, one layer of foam core, and one layer of inner skin cloth to complete the preparation of the prefabricated body; the sixth step is to lay the release cloth, flow guide net and injection molding on the inner skin cloth in sequence. Rubber support; the seventh step, fix the air guide tube around the prefabricated b...

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Abstract

A manufacturing method for a foam sandwich structure composite material hatch, the technical points of which include designing and optimizing the overall structure and layering of the hatch, completing the design and manufacture of molds, selecting fiber cloth and according to the size of the actual product According to the requirements, the material is cut, the foam material and embedded parts are selected, and the preparation of the prefabricated body is completed. The release cloth, the flow guide net and the glue injection support are laid in sequence on the inner skin cloth, and the air duct is fixed around the prefabricated body. Cover with sealing tape and vacuum bag film, connect the exhaust pipe and carry out process combination, vacuumize at room temperature, prepare the required resin in the material barrel, introduce the resin into the prefabricated body, and after the resin infiltrates the fiber, according to the curing process of the resin, room temperature or Heating and curing, after curing, cool down to room temperature naturally, turn off the vacuum system, and post-process the parts after demoulding; this technical solution has obvious weight reduction effect, strong designability, stable product shape and size, excellent thermal insulation performance, and good damping The noise reduction performance is obvious.

Description

technical field [0001] The invention relates to the technical field of manufacturing methods for composite material hatches, in particular to a manufacturing method for composite material hatches with a foam sandwich structure. Background technique [0002] The doors, hatches and body panels of traditional cars are mainly made of aluminum alloy materials. With the introduction of the concepts of lightweight vehicles, energy saving and emission reduction, and the gradual clarification of goals, weight reduction of new energy vehicle bodies has become an urgent problem to be solved. . [0003] Since the density of the aluminum alloy material is about 2.54g / cm 3 , so it has gradually failed to meet the weight reduction requirements of the car body. In comparison, composite materials have the characteristics of strong designability, high specific strength, high specific modulus, and corrosion resistance. Different material systems are used, and the density is designed at 1.5 g...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/44B29C70/54
CPCB29C70/443B29C70/54
Inventor 王晋纪双英仝建峰张洪邢军张子龙梁子青
Owner AVIC COMPOSITES
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