Optical Articles Comprising Encapsulated Microlenses and Methods of Making the Same
US-2021354410-A1 · Nov 18, 2021 · US
US2018147826A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018147826-A1 |
| Application number | US-201815879439-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 25, 2018 |
| Priority date | Apr 12, 2016 |
| Publication date | May 31, 2018 |
| Grant date | — |
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A nozzle deposits a filament of viscous, molten glass onto a print bed, while the print bed rotates about a vertical axis and translates in x, y, and z directions. The deposition is computer controlled, such that the resulting deposited filament forms a desired glass object that is solid after it anneals. One or more motors rotate the print bed such that the direction of deposition of the molten glass is constant relative to the nozzle, even though the print bed is translating in different directions relative to the nozzle. Keeping the direction of deposition constant relative to the nozzle tends to prevent the extruded filament of molten glass from experiencing large, changing, tensile and shear forces that would otherwise occur and that would otherwise damage the filament.
Opening claim text (preview).
What is claimed is: 1 . A method comprising a nozzle extruding material onto a print bed, wherein: (a) during the extruding, the material is deposited in a deposition direction; (b) one or more motors actuate the print bed in such a way that (i) during the extruding, the print bed undergoes a translation relative to the nozzle, which translation has an x-component and a y-component, the x-component being movement in a direction parallel to an x-axis, the y-component being movement in a direction parallel to a y-axis, and the x- and y-axes being perpendicular to each other, and (ii) during the translation, the print bed substantially rotates about an axis that is parallel to a z-axis, the z-axis being perpendicular to the x-axis and to the y-axis; (c) the deposition direction is substantially constant relative to the nozzle throughout the entire translation; and (d) the nozzle is stationary relative to a fixed position throughout the entire translation. 2 . The method of claim 1 , wherein: (a) the material is deposited at impact points in a deposition trajectory; and (b) the deposition trajectory has multiple inflection points. 3 . The method of claim 1 , further comprising a gas torch heating the nozzle in such a way that the heating melts material that has built up on an exterior surface of the nozzle. 4 . The method of claim 1 , wherein: (a) the speed of the nozzle relative to the print bed is constant throughout the entire translation; and (b) the angular velocity of the print bed varies during the translation. 5 . The method of claim 1 , wherein: (a) during the translation, the material is deposited at impact points in a deposition trajectory; and (b) the deposition trajectory has an overall shape that is neither a circle, nor a spiral, nor an involute of a circle, nor a segment of a straight line, nor a portion of a circle, nor a portion of a spiral, nor a portion of an involute of a circle. 6 . The method of claim 1 , wherein: (a) the extruding fabricates a 3D object; and (b) the method further comprises one or more computers transforming coordinates of points in a virtual model of the 3D object into points in a trajectory of the print bed. 7 . The method of claim 1 , wherein: (a) the translation of the print bed has an instantaneous direction, relative to the nozzle, at any given instant during the translation; and (b) the instantaneous direction is not constant throughout the entire translation. 8 . The method of claim 1 , wherein: (a) the material that is deposited during the translation comprises a filament; and (b) after the filament is deposited, the filament has a constant width, such that the width is identical at different spatial points along the filament. 9 . The method of claim 1 , wherein: (a) the material that is deposited during the translation comprises a filament; and (b) after the filament is deposited, a cross-sectional region of the filament (i) corresponds to a particular region of an orifice of the nozzle, and (ii) is in a constant cross-sectional position of the filament, in different cross-sections of the filament. 10 . The method of claim 2 , wherein the speed of the nozzle relative to the print bed is constant throughout the entire translation. 11 . A system comprising: (a) a print bed; (b) a first kiln that is configured to heat material; (c) a nozzle that is configured to extrude the material onto the print bed during a period of time, which nozzle is stationary relative to a fixed position throughout the entire period; and (d) one or more motors that are configured to actuate the print bed in such a way that (i) while the material is being extruded, the print bed undergoes a translation relative to the fixed position and to the nozzle, which translation has an x-component and a y-component, the x-component being movement in a direction parallel to an x-axis, the y-component being movement in a direction parallel to a y-axis, and the x- and y-axes being perpendicular to each other, and (ii) during the translation, the print bed substantially rotates about an axis that is parallel to a z-axis, the z-axis being perpendicular to the x-axis and to the y-axis, (iii) during the translation, the material is deposited in a deposition direction, and (iv) the deposition direction is substantially constant relative to the nozzle throughout the entire translation. 12 . The system of claim 11 , wherein: (a) the material that is deposited has a deposition trajectory; and (b) the deposition trajectory has multiple inflection points. 13 . The system of claim 11 , further comprising a gas torch that is configured to heat-the nozzle to a sufficiently high temperature to melt material that has built up on an exterior surface of the nozzle. 14 . The system of claim 11 , wherein the one or motors are configured to actuate the print bed in such a way that: (a) the speed of the nozzle relative to the print bed is constant throughout the entire translation; and (b) the angular velocity of the print bed varies during the translation. 15 . The system of claim 11 , wherein: (a) during the translation, the material is deposited at impact points in a deposition trajectory; and (b) the deposition trajectory, as a whole, has a shape that is neither a circle, nor a spiral, nor an involute of a circle, nor a segment of a straight line, nor a portion of a circle, nor a portion of a spiral, nor a portion of an involute of a circle. 16 . The system of claim 11 , wherein: (a) the extruding fabricates a 3D object; and (b) the system further comprises one or more computers that are programmed to transform coordinates of points in a virtual model of the 3D object into points in a trajectory of the print bed. 17 . The system of claim 11 , wherein: (a) the translation of the print bed has an instantaneous direction, relative to the nozzle, at any given instant during the translation; and (b) the instantaneous direction is not constant throughout the entire translation. 18 . The system of claim 11 , wherein: (a) the material that is deposited during the translation comprises a filament; and (b) after the filament is deposited, the filament has a constant width, such that the width is identical at different spatial points along the filament. 19 . The system of claim 11 , wherein: (a) the material that is deposited during the translation comprises a filament; and (b) after the filament is deposited, a cross-sectional region of the filament (i) corresponds to a particular region of an orifice of the nozzle, and (ii) is in a constant cross-sectional position of the filament, in different cross-sections of the filament. 20 . The system of claim 12 , wherein the speed of the nozzle relative to the print bed is constant throughout the entire translation.
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