Chronological Project Progression
Timeline overview:
I designed the printer via. CAD in January 2021, began cutting and drilling the aluminum rails sometime around March, and have been sporadically printing components when needed via. both FDM and SLA throughout the entirety of the project. I spent time this summer implementing the tensioners and more mechanical aspects. There was also a learning curve involved in setting up the software hardware interfaces, and learning to configure for RepRap using GCODE commands.
By and large, when 3D printing an assembly, more parts means more attachment points, more attachment points means more surfaces, more surfaces mean greater volume, and finally, greater volume means greater weight. Therefore, the less parts, the lighter the aircraft, and the more control I have over weight distribution. Due to this, I have designed and recently begun constructing a printer capable of producing parts in the range of 960x600x960mm. Printers of this size are often coreXY as opposed to cartesian due to the efficiency disadvantages of mobilizing large and heavy parts on the Y axis. I went for a cartesian design for cost and construction reasons. CoreXY printers require more advanced control boards and the frames generally require a great deal more slotted framing.