Moulding process for fuselage of UAV (Unmanned Aerial Vehicle)

The invention relates to a moulding process for a fuselage of a UAV (Unmanned Aerial Vehicle). The moulding process comprises the following steps: step 1, 1-2 layers of 3K carbon fiber prepregs are attached to a preheated moulding upper mould; then 2-4 layers of 30-50 DEG C 25-60g angle carbon fiber...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZHANG SISHUN, ZHU JIAQIANG, ZHANG HAO, LUO JIANLAN, XIE CHANGZHI, WANG BIN
Format: Patent
Sprache:chi ; eng
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