Light aircraft wing hollow structure forming method and intelligent mold thereof
The invention relates to the technical field of composite material forming processes, in particular to a forming method for a hollow structure of a light aircraft wing and an intelligent mold thereof.The forming method comprises the following steps that S1, a sleeve is arranged on the intelligent mo...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention relates to the technical field of composite material forming processes, in particular to a forming method for a hollow structure of a light aircraft wing and an intelligent mold thereof.The forming method comprises the following steps that S1, a sleeve is arranged on the intelligent mold in a sleeving mode and fixed; s2, carbon fiber fabric is laid on a lower mold body of the metal mold, the intelligent mold is placed on the carbon fiber fabric, and the molded surface of the intelligent mold is covered with the carbon fiber fabric; s3, the upper die and the lower die of the metal die are aligned and closed; the vacuum bag penetrates through a mold cavity of the intelligent mold and is sealed and fixed; then assembling and fixing the metal mold; according to the forming method for the hollow structure of the light aircraft wing, the forming quality of a composite material part is guaranteed, the problems that in the forming process, a closed cavity part is difficult to lay up, and demolding is di |
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