Abstract: Advanced methods, apparatuses, and systems are presented for the real-time monitoring and precise control of substances undergoing phase transitions within a vacuum system, in particular, for lyophilization processes. Utilizing sophisticated interfaces, these techniques enable the visualization of phase diagrams depicting the equilibrium conditions of temperature and pressure for distinct substances. Real-time temperature and pressure data are seamlessly integrated and graphically represented on these phase diagrams. Furthermore, the methodology incorporates advanced regression models to accurately estimate mass quantities and employs dynamic environmental control curves for system parameter adjustments. These techniques encompass real-time data analysis, responsive adjustment inputs, intuitive graphical representations that ensure meticulous control and monitoring of phase transitions, thereby optimizing process monitoring and outcomes.

Abstract: Advanced methods, apparatuses, and systems are presented for the real-time monitoring and precise control of substances undergoing phase transitions within a vacuum system, in particular, for lyophilization processes. Utilizing sophisticated interfaces, these techniques enable the visualization of phase diagrams depicting the equilibrium conditions of temperature and pressure for distinct substances. Real-time temperature and pressure data are seamlessly integrated and graphically represented on these phase diagrams. Furthermore, the methodology incorporates advanced regression models to accurately estimate mass quantities and employs dynamic environmental control curves for system parameter adjustments. These techniques encompass real-time data analysis, responsive adjustment inputs, intuitive graphical representations that ensure meticulous control and monitoring of phase transitions, thereby optimizing process monitoring and outcomes.

Abstract: A support structure of a 3D printer may include a printable surface that receives a heated bead of material and can support one or more extruded layers of material from the 3D printer. The support structure may include at least one inlet adjacent to the printable surface and one or more outlets that exit onto the printable surface. The one or more outlets are hermetically sealed to the inlet. The support structure may also include an injection mechanism operatively coupled to the at least one input.

Abstract: A support structure of a 3D printer may include a printable surface that receives a heated bead of material and can support one or more extruded layers of material from the 3D printer. The support structure may include at least one inlet adjacent to the printable surface and one or more outlets that exit onto the printable surface. The one or more outlets are hermetically sealed to the inlet. The support structure may also include an injection mechanism operatively coupled to the at least one input.

Abstract: A technique for consolidating threads of diverse materials into a cohesive consolidated composite thread that includes a channel with an entry and exit, designed to accommodate threads of both the first and second materials. Equipped with one or more heaters, the technique raises the temperature of the second material above its melting point. A driver propels the threads through the channel, while a thermal conditioner, positioned between the driver and exit of the channel, lowers the temperature of the second material below its melting point prior to entering an extruder nozzle, where it is reheated above the second material below its melting point and deposited onto a 3D printed object.

Abstract: A navigable craft that includes a fuselage with a tiltable section positioned behind a non-tiltable section opposite to a nose. A set of wing assemblies connected to the non-tiltable section of the fuselage. Each wing assembly includes an airfoil connected to the non-tiltable section of the fuselage at a first cross-sectional end of the airfoil and a non-tiltable propulsion generator connected to a second cross-sectional end of the airfoil opposite to the first cross-sectional end of the airfoil. The propulsion generator extends parallel and adjacent to the non-tiltable section of the fuselage, and one or more stabilizers connected to at least one of the non-tiltable propulsion generator, the airfoil, and the fuselage. The landing assembly is connected to the propulsion generator or the airfoil. The landing assembly is aligned aerodynamically with the second cross-sectional end and extends in a direction adjacent to the tiltable section of the fuselage.

Abstract: A support structure of a 3D printer may include a printable surface that receives a heated bead of material and can support one or more extruded layers of material from the 3D printer. The support structure may include at least one inlet adjacent to the printable surface and one or more outlets that exit onto the printable surface. The one or more outlets are hermetically sealed to the inlet. The support structure may also include an injection mechanism operatively coupled to the at least one input.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.

Abstract: A printer system may include a coaxial extruder head that extrudes a core, a bulk, and/or a core and bulk cladding to form complex structures without retooling. The coaxial extruder head may include a distribution channel with an entrance and an exit, a priming chamber that surrounds the distribution channel. The priming chamber may include an outlet and a first inlet, a heating element thermally connected to the priming chamber, and a nozzle connected to the outlet of the priming chamber. Further, the nozzle may converge from the outlet of the priming chamber to an orifice of the nozzle. In addition, the exit of the distribution channel may be disposed at the orifice of the nozzle. This structure facilitates extruding a core and cladding type composite from the extruder head.