3d-printed building material system
US-2024247488-A1 · Jul 25, 2024 · US
US2026043234A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2026043234-A1 |
| Application number | US-202519199710-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 6, 2025 |
| Priority date | Aug 12, 2024 |
| Publication date | Feb 12, 2026 |
| Grant date | — |
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The present disclosure is directed to a construction element produced by additive manufacturing, an additive manufacturing system for producing the construction element and a method for manufacturing the construction element. The construction element includes an outer layer. The outer layer is configured to define or form an enclosure. The construction element further includes an inner matrix. The inner matrix is formed within the enclosure. The outer layer and the inner matrix are formed integrally, by depositing successive layers using an additive manufacturing system. The inner matrix is defined by a first layup and a second layup. The first layup is laid along a first direction and across the enclosure. The second layup is laid juxtaposing the first layup. The first layup and the second layup define a plurality of air pockets in the inner matrix. Further, a filler material is infused into at least some air pockets of the plurality of air pockets.
Opening claim text (preview).
1 - 17 . (canceled) 18 . A construction element fabricated by an additive-manufacturing process, the construction element comprising: an outer layer additively printed from a first material so as to define a closed-perimeter enclosure; an inner matrix integrally additively printed within the enclosure from successive layers deposited during the same build operation related to printing the successive layers in forming the inner matrix, the inner matrix including: a first layup of extruded filaments oriented along a first direction; and a second layup of extruded filaments oriented along a second direction different from the first direction and intersecting the first layup, whereby the first and second layups cooperatively delimit a plurality of closed air pockets; and a filler material different from the first material and selectively infused, during or after printing, into a predetermined subset of the air pockets so as to form at least one closed-loop contour entirely surrounded by unfilled air pockets. 19 . The construction element of claim 18 , wherein the first material of the outer layer and a second material of the inner matrix are the same composition. 20 . The construction element of claim 18 , wherein the first material is different from a second material that forms the inner matrix, the first and second materials being co-extruded in successive layers. 21 . The construction element of claim 18 , wherein the inner matrix is printed from a blend comprising clay, plastic particles recovered from post-consumer waste, and carbon powder. 22 . The construction element of claim 18 , wherein the filler material comprises a foamed polymer or other synthetic insulating foam. 23 . The construction element of claim 18 , wherein the selectively filled air pockets define concentric inner and outer rectangular contours. 24 . The construction element of claim 18 , further comprising at least one inner layer, printed with substantially the same cross-sectional configuration as the outer layer, the inner layer and the outer layer cooperatively defining at least one cavity within the inner matrix. 25 . The construction element of claim 24 , wherein the cavity lies adjacent to a peripheral region of the outer layer. 26 . The construction element of claim 24 , wherein the cavity lies substantially centrally of the outer layer. 27 . The construction element of claim 24 , wherein the cavity is C-shaped, S-shaped, arcuate, semi-circular or rectangular. 28 . The construction element of claim 24 , further comprising an insert received within the cavity, the insert being formed of compressed plastic waste, compressed natural fibres, or a combination thereof. 29 . The construction element of claim 28 , wherein the compressed natural fibres include at least one of dried and milled palm-trunk wood, dried palm leaves, date-palm leaves, crushed date pits or wood, the fibres being consolidated with a binder comprising okra powder and water. 30 . The construction element of claim 18 , wherein the unfilled air pockets and the selectively filled air pockets together establish a total thermal resistance greater than that obtained by a homogeneous wall of equal thickness printed from the first material alone. 31 . The construction element of claim 18 , wherein the outer layer has a thickness of one printed layer, the inner matrix directly adjoining the outer layer on an inner surface thereof. 32 . The construction element according to claim 18 , wherein the first layup and the second layup crisscross each other at an angle in a range of 40 degrees to 50 degrees. 33 . The construction element according to claim 18 , wherein the plurality of closed air pockets collectively occupies at least fifty percent of the volume bounded by the outer layer.
using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber · CPC title
using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material · CPC title
Processes of additive manufacturing · CPC title
involving additional operations performed on the added layers, e.g. smoothing, grinding or thickness control (surface shaping B29C59/00; after-treatment of articles without altering their shape B29C71/00) · CPC title
during lay-up · CPC title
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