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Vacuum forming preparation method of helicopter fuselage composite material

A composite material and vacuum forming technology, which is applied to household appliances, other household appliances, household components, etc., can solve the problems such as the molding preparation process needs to be optimized, the product quality is difficult to meet the manufacturing requirements, and the molding effect of the composite material is affected, so as to improve the molding process. effect, ensure product quality, and optimize the effect of the preparation process

Pending Publication Date: 2022-07-15
上海喆航航空科技有限公司
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Problems solved by technology

[0003] The object of the present invention is to provide a kind of vacuum forming preparation method of composite material of helicopter fuselage, to solve the problem that the traditional composite material forming preparation process proposed in the above-mentioned background technology needs to be optimized, which affects the forming effect of the composite material, and the quality of the product prepared by the composite material is difficult. Problems meeting manufacturing requirements

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  • Vacuum forming preparation method of helicopter fuselage composite material

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Embodiment Construction

[0021] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0022] see figure 1 As shown, a kind of technical scheme provided by the present invention:

[0023] A method for preparing a composite material of a helicopter fuselage by vacuum forming, comprising the following steps:

[0024] Sp1: Equipped with the required amount of prepreg, equipped with a vacuum bag with vacuum fittings and an air pump with a control vacuum gauge;

[0025] Sp2: Open the vacuum bag, place the prepreg in the va...

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Abstract

The invention relates to the technical field of composite material product manufacturing, in particular to a helicopter fuselage composite material vacuum forming preparation method which comprises the following steps: Sp1, preparing a required amount of prepreg, a vacuum bag with a vacuum pipe fitting and an air pump with a control vacuum gauge, Sp2, opening the vacuum bag, placing the prepreg in the vacuum bag, and carrying out vacuum forming on the prepreg; sp3, pasting and laying a drainage fabric on the perforated film layer, sealing a vacuum bag, and communicating a joint of a vacuum pipe fitting with a joint of a control vacuum gauge, Sp4, opening an air pump to vacuumize the vacuum bag, checking the sealing performance of the vacuum bag, and finally, sealing the vacuum bag. The composite material forming preparation process can be carried out under the optimal condition, the composite material vacuum forming preparation process is optimized, the forming effect of the composite material is improved, and the quality of a product prepared from the composite material is guaranteed.

Description

technical field [0001] The invention relates to the technical field of composite material product manufacturing, in particular to a vacuum forming preparation method for a composite material of a helicopter fuselage. Background technique [0002] Helicopter has the characteristics of vertical lifting, hovering, and flying forward or backward at low speed. It is a typical dual-use product for military and civilian use. The disadvantages are low speed, high fuel consumption and short range. It can be widely used in transportation, patrolling , tourism, ambulance and other fields, helicopter design focuses on reducing aircraft weight and improving structural strength, manufacturing complex fuselage and other parts of aircraft, need to use lighter and stronger materials, these materials are composite materials, The molding preparation process of traditional composite materials needs to be optimized, which affects the molding effect of composite materials, and the quality of prod...

Claims

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Application Information

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IPC IPC(8): B29C70/34B29C70/54B29L31/30
CPCB29C70/342B29C70/54B29L2031/3082
Inventor 孙志武
Owner 上海喆航航空科技有限公司
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