US2021379827A1PendingUtilityA1
In-situ curing oven for additive manufacturing system
Est. expiryJun 29, 2037(~11 yrs left)· nominal 20-yr term from priority
B22F 12/22B22F 12/53B22F 10/25B33Y 70/00B29C 64/124B29C 2035/0855B29K 2101/10B33Y 30/00B29C 2035/0877B22F 10/00B29C 35/0261B29C 70/16B33Y 50/02F16L 9/128B29C 2035/0833B29C 64/112B29C 64/209B29C 70/24B29C 64/295B29K 2105/08B29C 2035/0827B29C 64/245B29C 64/336Y02P10/25B29C 64/165B33Y 10/00B29C 2035/0838B29C 64/291B29C 70/523B29C 70/50B29C 35/0805B29C 70/06B29C 64/40B29C 48/15B29C 64/255B29K 2105/251B29C 64/218B29C 70/384B29C 64/393
83
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
A system is disclosed for additively manufacturing a composite structure. The system may include a head configured to discharge a continuous reinforcement that is at least partially coated with a matrix, and a housing trailing from the head and configured to at least partially enclose the continuous reinforcement after discharge. The system may also include a heat source disposed at least partially inside the oven, and a support configured to move the head during discharging.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A method of additively manufacturing a composite structure, comprising:
discharging from a head a continuous reinforcement that is at least partially coated with a matrix; passing the matrix-coated continuous reinforcement through an oven trailing behind on the head; exposing the matrix-coated continuous reinforcement to heat inside the oven; and moving the head during discharging to create three-dimensional trajectory in the continuous reinforcement.
2 . The method of claim 1 , further including exposing the matrix coating the continuous reinforcement to a cure energy prior to the continuous reinforcement passing into the oven.
3 . The method of claim 2 , wherein the cure energy is UV light.
4 . The method of claim 3 , wherein:
the UV light cures only an outer shell of the matrix; and the heat inside the oven cures an inner portion of the matrix.
5 . The method of claim 3 , wherein:
the UV light cures only the matrix; and the heat inside the oven cures particles suspended in the matrix.
6 . A method of additively manufacturing a composite structure, comprising:
discharging a material from a print head; moving the print head during discharging; directing cure energy toward the material from a source connected to a trailing side of the print head; and directing cure energy to the material from a cure enhancer.
7 . The method of claim 6 , wherein the cure energy directed from the source is a different type of energy than the cure energy directed from the cure enhancer.
8 . The method of claim 6 , wherein directing cure energy toward the material from the source includes directing heat toward the material.
9 . The method of claim 8 , wherein directing cure energy to the material from the cure enhancer includes directing UV light toward the material.
10 . The method of claim 9 , wherein directing UV light to the material includes directing the UV light to the material before directing the heat toward the material.
11 . The method of claim 6 , wherein an amount of the cure energy directed from the source is different than an amount of the cure energy directed from the cure enhancer.
12 . The method of claim 11 , wherein the amount of the cure energy directed from the cure enhancer is sufficient to only cure an outer shell of the material.
13 . The method of claim 12 , wherein the amount of the cure energy directed from the source is sufficient to cure an inner portion of the material.
14 . A method of additively manufacturing a composite structure, comprising:
discharging a material from a print head; moving the print head during discharging; directing cure energy toward the material from a first location at a trailing side of the print head; and directing cure energy toward the material from a second location.
15 . The method of claim 14 , wherein the cure energy directed from the first location is a different type of energy than the cure energy directed from the first location.
16 . The method of claim 15 , wherein directing the cure energy toward the material from the second location includes directing heat toward the material.
17 . The method of claim 16 , wherein directing the cure energy to the material from the first location includes directing UV light toward the material.
18 . The method of claim 17 , wherein directing UV light to the material includes directing the UV light to the material before directing the heat toward the material.
19 . The method of claim 14 , wherein an amount of the cure energy directed from the second location is different than an amount of the cure energy directed from the first location.
20 . The method of claim 19 , wherein:
the amount of cure energy directed from the first location is sufficient to only cure an outer shell of the material; and the amount of cure energy directed from the second location is sufficient to cure an inner portion of the material.Cited by (0)
No later patents cite this yet.
References (0)
No backward citations on record.