Printed hollow bodies and systems and methods for printing hollow bodies
Systems and methods for 3D printing hollow bodies, such as bodies having an exterior cylindrical shape with a hollow interior, are described. Such systems and methods utilize rotatable hollow print base supports having an interior size and/or shape that matches the desired exterior shape of the final printed structure. The printed bodies, methods, and systems enable printing of the desired hollow printed body from the outside-to-inside. They also allow easy production, customization, and modification of internal structures within the printed hollow body.
1. A method of printing, comprising:
placing a print head including a print nozzle within an interior of a hollow mandrel;
positioning the print nozzle at a location adjacent a surface located within the interior of the hollow mandrel;
dispensing print media material through the print nozzle onto the surface at the location;
rotating the hollow mandrel about a rotational axis;
moving the print head in a first direction substantially parallel to the rotational axis, wherein at least one of the steps of rotating the hollow mandrel and moving the print head in the first direction occurs while the print media material is being dispensed; and
moving the print head in a second direction substantially perpendicular to and away from the surface onto which the print media material is being dispensed,
wherein the print media material forms a hollow body for a rocket, a fuselage, a missile, or a torpedo.
2. The method of claim 1 , wherein the step of moving the print head in the first direction occurs while the print media material is being dispensed.
3. The method of claim 2 , wherein the step of rotating the hollow mandrel occurs while the print media material is being dispensed.
4. The method of claim 1 , wherein the step of rotating the hollow mandrel occurs while the print media material is being dispensed.
5. The method of claim 1 , wherein the interior of the hollow mandrel constitutes a cylindrical surface, wherein the rotational axis is a central axis of the cylindrical surface, wherein the first direction is substantially horizontal, and wherein the second direction is substantially vertical.
6. The method of claim 1 , further comprising:
separating the hollow mandrel from the print media material deposited on the interior thereof.
7. The method of claim 1 , wherein the print head is controlled to move and dispense the print media material to form a 100% printed hollow structure having an exterior surface with at least one of a tapered region, a frusto-conical structure, or a frusto-ogive structure.
8. The method of claim 1 , wherein the hollow body comprises a hollow body for a rocket.
9. The method of claim 1 , wherein the hollow body comprises a hollow body for a fuselage.
10. The method of claim 1 , wherein the hollow body comprises a hollow body for a missile.
11. The method of claim 1 , wherein the hollow body comprises a hollow body for a torpedo.
12. A method of printing a hollow body, comprising:
placing a print head including a print nozzle within an interior of a hollow mandrel, the hollow mandrel including an exterior surface and an interior surface opposite the exterior surface, the interior surface defining the interior of the hollow mandrel;
forming a first printed layer of the hollow body, including the steps of:
(a) positioning the print nozzle at a location adjacent the interior surface of the hollow mandrel;
(b) dispensing print media material through the print nozzle onto the interior surface at the location;
(c) moving the print head along the interior surface; and
(d) rotating the hollow mandrel, wherein at least one of the steps of moving the print head and rotating the hollow mandrel occurs while print media material is being dispensed onto the interior surface,
wherein the step of forming the first printed layer forms an exterior surface of the hollow body positioned in contact with the interior surface of the hollow mandrel, wherein the first printed layer includes an interior surface, and wherein the first printed layer extends continuously around 360 degrees of the interior surface of the hollow mandrel;
moving the print head in a direction away from a print media material deposit location at the interior surface of the first printed layer;
forming a second printed layer of the hollow body, including the steps of:
(a) positioning the print nozzle at a location adjacent the interior surface of the first printed layer;
(b) dispensing print media material through the print nozzle onto the interior surface of the first printed layer at the location adjacent the interior surface of the first printed layer;
(c) moving the print head in a direction along the interior surface of the first printed layer; and
(d) rotating the hollow mandrel, wherein, when forming the second printed layer, at least one of these steps of moving the print head and rotating the hollow mandrel occurs while the print media material is being dispensed onto the interior surface of the first printed layer,
wherein the step of forming the second printed layer forms the second printed layer in contact with and at least partially covering the interior surface of the first printed layer, wherein the second printed layer includes an interior surface, and wherein the second printed layer extends continuously around 360 degrees of the interior surface of the first printed layer, and
wherein the print media material forms the hollow body as a hollow body for a rocket, a fuselage, a missile, or a torpedo.
13. The method of claim 12 , further comprising:
printing one or more additional printed layers inside of the second printed layer, wherein the step of printing each additional layer includes:
(a) moving the print head in a direction along an interiormost surface of an immediately preceding printed layer; and
(b) dispensing print media material through the print nozzle onto the interiormost surface of the immediately preceding printed layer while the print head is moving and/or the hollow mandrel is rotating to form a new layer inside of and at least partially covering the immediately preceding printed layer.
14. The method of claim 13 , wherein the step of printing the one or more additional printed layers prints at least 5 additional printed layers inside the second printed layer.
15. The method of claim 13 , wherein the interior of the hollow mandrel constitutes a cylindrical surface, wherein the steps of rotating the hollow mandrel rotate the hollow mandrel along a central axis of the cylindrical surface, and wherein the steps of moving the print head in the direction along the interior or interiormost surface includes moving the print head in a direction parallel to the central axis.
16. The method of claim 12 , wherein at least one of the steps of rotating the hollow mandrel occurs while the print media material is being dispensed.
17. The method of claim 12 , wherein at least one of the steps of moving the print head occurs while the print media material is being dispensed.
18. The method of claim 12 , wherein at least one of the steps of rotating the hollow mandrel occurs at a time when print media material is not being dispensed.
19. The method of claim 12 , wherein at least one of the steps of moving the print head occurs at a time when print media material is not being dispensed.
20. The method of claim 12 , further comprising:
separating the hollow mandrel from the first printed layer, wherein the first printed layer, the second printed layer, and any other present printed layers form a printed hollow body.
21. The method of claim 12 , wherein the exterior surface of the hollow body includes at least one of a tapered region, a frusto-conical structure, or a frusto-ogive structure.
22. The method of claim 12 , wherein the hollow body is a 100% printed hollow body.
23. The method of claim 12 , wherein the hollow body comprises a hollow body for a rocket.
24. The method of claim 12 , wherein the hollow body comprises a hollow body for a fuselage.
25. The method of claim 12 , wherein the hollow body comprises a hollow body for a missile.
26. The method of claim 12 , wherein the hollow body comprises a hollow body for a torpedo.
27. A printing system, comprising:
a rotatable print support base including a hollow mandrel having an exterior surface and an interior surface, the hollow mandrel defining an interior and being rotatable about a rotational axis, wherein the interior surface of the hollow mandrel is configured to receive a deposit of print media material to form a hollow body for a rocket, a fuselage, a missile, or a torpedo;
a guide rail;
a guide rail support configured to support the guide rail such that the guide rail extends at least partially through the interior of the hollow mandrel, wherein the guide rail support is configured to move the guide rail within the interior of the hollow mandrel in a direction away from a region of the interior surface where print media material is deposited;
a print head mounted on the guide rail and movable in a direction along the guide rail, wherein the print head includes a print nozzle oriented to dispense print media material onto a surface located within the interior of the hollow mandrel; and
a control system configured to control the printing system to deposit the print media material to form the hollow body.