CPC B29C 48/05 (2019.02) [B29B 15/14 (2013.01); B29C 48/28 (2019.02); B29C 48/885 (2019.02); B29C 48/911 (2019.02); B29C 64/314 (2017.08); B29C 70/523 (2013.01); B29C 70/525 (2013.01); B33Y 40/10 (2020.01); B33Y 70/10 (2020.01); B29K 2071/00 (2013.01); B29K 2105/08 (2013.01); B29K 2307/04 (2013.01)] | 6 Claims |
1. An on-orbit composite filament forming device for space 3D printing, comprising: a constant tension unwinding module, a replaceable resin filament rotary wrapping module, a melt preheating chamber, a curved channel impregnation chamber, a variable aperture resin recovery device, a heat protective housing, a convective cooling device, a traction device, and a winding device arranged sequentially, wherein the melt preheating chamber, the curved channel impregnation chamber, and the variable aperture resin recovery device are located in the heat protective housing; the replaceable resin filament rotary wrapping module comprises at least one active unwinding reel placed on a circular rail centered on a carbon fiber; a first metal scraper opening and closing mechanism, a second metal scraper opening and closing mechanism, and a third metal scraper opening and closing mechanism are provided sequentially inside the variable aperture resin recovery device; a circumferential heating resistor is provided in a housing of the variable aperture resin recovery device, and a lateral push device is provided at an upper part of the housing of the variable aperture resin recovery device.
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