3D PRINTING APPARATUS
20240109243 ยท 2024-04-04
Assignee
Inventors
Cpc classification
B29C64/236
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/371
PERFORMING OPERATIONS; TRANSPORTING
B29C64/393
PERFORMING OPERATIONS; TRANSPORTING
B29C64/118
PERFORMING OPERATIONS; TRANSPORTING
B29C64/25
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/34
PERFORMING OPERATIONS; TRANSPORTING
B29C35/02
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y50/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C64/118
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y50/02
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/236
PERFORMING OPERATIONS; TRANSPORTING
B29C64/25
PERFORMING OPERATIONS; TRANSPORTING
B29C64/393
PERFORMING OPERATIONS; TRANSPORTING
B29C64/371
PERFORMING OPERATIONS; TRANSPORTING
B29C35/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
In general terms the present invention proposes a 3D printing apparatus 100 for printing a satellite component. The 3D printing apparatus comprises a housing 102, a seal 104 arranged movably inside the housing such that the seal partitions the housing into first and second chambers 106A, 106B that are fluidically isolated from each other, and a nozzle 108 in fluid connection with the second chamber 106B. The first chamber 106A comprises a gas having a pressure P.sub.1 and the second chamber 106B comprises a printing material. When the 3D printing apparatus 100 is exposed to an external environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the gas in the first chamber 106A, the gas in the first chamber 106A exerts a force on the seal 104 which in turn exerts a force on the printing material thereby extruding the printing material out of the second chamber 106B through the nozzle 108 to print the satellite component.
Claims
1. A 3D printing apparatus for printing a satellite component, the 3D printing apparatus comprising: a housing; a seal arranged movably inside the housing such that the seal partitions the housing into first and second chambers that are fluidically isolated from each other, the first chamber comprising a gas having a pressure P.sub.1; the second chamber comprising a printing material; and a nozzle in fluid connection with the second chamber; wherein when the 3D printing apparatus is exposed to an external environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the gas in the first chamber, the gas in the first chamber exerts a force on the seal which in turn exerts a force on the printing material thereby extruding the printing material out of the second chamber through the nozzle to print the satellite component.
2. A 3D printing apparatus of claim 1, wherein the nozzle comprises a temperature control module, optionally wherein the temperature control module comprises a Peltier module.
3. A 3D printing apparatus of claim 2, wherein the temperature control module is arranged to control the temperature of the printing material being extruded from the nozzle in a range of from ?50? C. to 150? C., optionally in a range of from ?20? C. to 150? C.
4. A 3D printing apparatus of claim 1, wherein the printing material comprises a liquid photopolymer.
5. A 3D printing apparatus of claim 1, wherein the gas comprises a noble gas, optionally wherein the gas comprises one or more of neon, argon, krypton, and/or xenon.
6. A 3D printing apparatus of claim 1, wherein the pressure P.sub.1 of the gas is less than 1 atm.
7. A 3D printing apparatus of claim 1, comprising a printing platform for receiving printing material extruded out of the second chamber through the nozzle, wherein the printing platform is positioned adjacent to the nozzle.
8. A 3D printing apparatus of claim 7, comprising a motor arranged to rotate the 3D printing apparatus with respect to the printing platform.
9. A 3D printing apparatus of claim 7, comprising a linear pushing mechanism arranged to move the printing platform away from the nozzle.
10. A 3D printing apparatus of claim 9, wherein the linear pushing mechanism comprises one or more motor driven wheels.
11. A 3D printing apparatus of claim 1, comprising a curing device for curing printing material extruded out of the second chamber through the nozzle.
12. A 3D printing apparatus of claim 11, wherein the curing device comprises an ultraviolet light source, and wherein the curing device comprises an opaque screen for shading at least a portion of the nozzle from the ultraviolet light source.
13. A 3D printing apparatus of claim 1, comprising a sealing element for reversibly sealing an end of the nozzle, wherein the sealing element comprises a plug.
14. A 3D printing apparatus of claim 1, comprising a first inlet in fluid connection with the first chamber for introducing the gas having a pressure P.sub.1 into the first chamber; and a second inlet in fluid connection with the second chamber for introducing the printing material into the second chamber.
15. A system for positioning a satellite component, the system comprising a 3D printing apparatus according to claim 1 and a satellite component attached between the printing platform and a fixed attachment point, wherein the 3D printing apparatus is arranged to print an elongate structure, and wherein printing of the elongate structure is arranged to move the printing platform away from the fixed attachment point to position the satellite component.
16. A system of claim 15, wherein positioning the satellite component comprises unfolding or unrolling the satellite component.
17. A system of claim 15, wherein the satellite component comprises a folded solar panel, and wherein printing of the elongate structure is arranged to move the printing platform away from the fixed attachment point to unfold the folded solar panel; or a stowed antenna, and wherein printing of the elongate structure is arranged to move the printing platform away from the fixed attachment point to unfold or unroll the stowed antenna.
18. A system of claim 15, wherein the printed elongate structure is a cylinder.
19. A method of 3D printing a satellite component, the method comprising the steps of providing an 3D printing apparatus according to claim 1; introducing a gas having a pressure P.sub.1 into the first chamber; introducing a printing material into the second chamber; exposing the 3D printing apparatus to an environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the gas in the first chamber, such that the gas in the first chamber exerts a force on the seal, which in turn exerts a force on the printing material, thereby extruding the printing material out of the second chamber through the nozzle.
20. A method of claim 19, comprising controlling the temperature of the printing material being extruded from the nozzle in a range of from ?50? C. to 150? C., optionally in a range of from ?20? C. to 150? C.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0048] One or more embodiments of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION
[0055] Referring to
[0056] The first chamber 106A comprises a gas having a pressure P.sub.1 and the second chamber 106B comprises a printing material 110. When the 3D printing apparatus 100 is exposed to an external environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the gas in the first chamber 106A, the gas in the first chamber 106A expands. This exerts a force on the seal 104 which in turn exerts a force on the printing material 110, thereby extruding the printing material 110 out of the second chamber 106B through the nozzle 108.
[0057] Referring to
[0058] The first chamber 206A comprises argon gas having a pressure P.sub.1 and the second chamber 206B comprises a liquid photopolymer 210. In this example, the liquid photopolymer 210 comprises a mixture of styrene and benzophenone. When the 3D printing apparatus 200 is exposed to an external environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the argon gas in the first chamber 206A, the argon gas in the first chamber 206A expands. This exerts a force on the seal 204 which in turn exerts a force on the liquid photopolymer 210, thereby extruding the liquid photopolymer 210 out of the second chamber 206B through the nozzle 208.
[0059] The 3D printing apparatus 200 further comprises a printing platform 212, a motor 214, a linear pushing mechanism 215 comprising two motor driven wheels 216A, 216B, a Peltier module 218, a UV light source 220, a plug 222, a first inlet 224 for introducing argon gas having a pressure P.sub.1 into the first chamber 206A, and a second inlet 226 for introducing the liquid photopolymer 210 into the second chamber 206B. The printing platform 212 is positioned adjacent to the nozzle 208 for receiving the liquid photopolymer 210 that is extruded out of the second chamber 206B through the nozzle 208, when the 3D printing apparatus 200 is in use.
[0060] The 3D printing apparatus 200 may be used to print a cylindrical beam (not shown in the
[0061] Furthermore, the Peltier module 218 is used to control the temperature of the nozzle 208, which in turn controls the viscosity of the liquid photopolymer 210 extruded through the nozzle 208. The viscosity of the liquid photopolymer 210 is inversely proportional to the temperature of the nozzle 208. Hence, when the viscosity of the liquid photopolymer 210 is lower than a required viscosity, then the Peltier module 218 is used to increase the temperature of the nozzle 208 to increase the viscosity of the liquid photopolymer 210. Alternatively, when the viscosity of the printing material 210 is greater than a required viscosity, the Peltier module 218 decreases the temperature of the nozzle 108 to increase the viscosity of the liquid photopolymer 210.
[0062] Significantly, the Peltier module 218 can be used to cool the nozzle to temperatures below 0? C., which allows the viscosity of the liquid photopolymer 210 to be increased sufficiently in order to make it solid enough to be extruded via the nozzle 208 and for it to stay in place on the printing platform 212 after extrusion so that it can be hardened in its extruded form.
[0063] The UV light source 220 emits ultraviolet light, thereby curing (i.e. hardening) the liquid photopolymer 210 extruded out of the second chamber 206B through the nozzle 208. The UV light source 220 is arranged to be directed towards a region in proximity of an end of the nozzle 208 from which the printing material 210 is extruded. The UV light source 220 is partially covered by an opaque screen 228. The opaque screen 228 is positioned to provide a partially shaded region around the end of the nozzle 208 from the UV light source 220, when the 3D printing apparatus 200 is in use.
[0064] The plug 222 is used to reversibly seal an end of the nozzle 208. When the plug 222 is sealing an end of the nozzle 208, extrusion of the printing material from the second chamber 206B out of the nozzle 208 is prevented when the 3D printing apparatus is exposed to an external environment having a pressure P.sub.2 being less than the pressure P.sub.1 of the gas in the first chamber.
[0065] Referring to
[0066] Referring to
[0067] Referring collectively to
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