Yarn manufacturing apparatus
US-2016201229-A1 · Jul 14, 2016 · US
US10425993B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10425993-B2 |
| Application number | US-201615373368-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 8, 2016 |
| Priority date | Dec 8, 2016 |
| Publication date | Sep 24, 2019 |
| Grant date | Sep 24, 2019 |
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A heating element includes a bottom layer, a web consisting of a carbon nanotube (CNT) yarn wherein the web is affixed to a first side of the bottom layer, and an encapsulating layer positioned on the web and the first side of the bottom layer. A method for making a heating element includes providing a bottom layer, inserting a plurality of pegs into the bottom layer such that a portion of each peg protrudes from the bottom layer, weaving a CNT yarn around the protruding portions of the plurality of pegs to form a CNT web, affixing the CNT web to the bottom layer, and encapsulating the CNT web and the bottom layer to form the heating element.
Opening claim text (preview).
The invention claimed is: 1. A heating element comprising: a bottom layer; a web consisting of a carbon nanotube (CNT) yarn, wherein the web is affixed to a first side of the bottom layer, wherein portions of the CNT yarn of the web overlap to modify electrical resistivity compare to portions with no overlap; and an encapsulating layer positioned on the web and the first side of the bottom layer. 2. The heating element of claim 1 , further comprising an adhesive connecting the web to the first side of the bottom layer. 3. The heating element of claim 1 , wherein the CNT yarn forms a plurality of loops. 4. The heating element of claim 1 , wherein the web forms a mesh network. 5. A heating element comprising: a bottom layer; a web consisting of a carbon nanotube (CNT) yarn, wherein the web is affixed to a first side of the bottom layer, wherein the web forms a generally serpentine pattern; and an encapsulating layer positioned on the web and the first side of the bottom layer. 6. The heating element of claim 1 , wherein the CNT yarn consists of a single strand of connected CNTs. 7. The heating element of claim 1 , wherein the CNT yarn comprises a plurality of strands of connected CNTs woven together. 8. The heating element of claim 4 , wherein the mesh network is non-uniform across the web. 9. A method for making a heating element, the method comprising: providing a bottom layer; inserting a plurality of pegs into the bottom layer such that a portion of each peg protrudes from the bottom layer; winding a CNT yarn around the protruding portions of the plurality of pegs to form a CNT web, wherein the CNT yarn is wound around at least one of the protruding portions of the plurality of pegs such that a first portion of the CNT yarn overlaps a second portion of the CNT yarn; affixing the CNT web to the bottom layer; and encapsulating the CNT web and the bottom layer to form the heating element. 10. The method of claim 9 , further comprising: removing the plurality of pegs from the bottom layer after the CNT web has been affixed to the bottom layer. 11. The method of claim 9 , wherein the CNT yarn is woven around the protruding portions of the plurality of pegs to form a mesh network. 12. The method of claim 9 , wherein affixing the CNT web to the bottom layer comprises applying an adhesive to at least one of the CNT web and the bottom layer. 13. The heating element of claim 1 , wherein the bottom layer comprises a film adhesive, a pre-impregnated fabric, a polyimide, or a neoprene. 14. The heating element of claim 1 , wherein the bottom layer is attached to an external surface of an aircraft component. 15. The heating element of claim 1 , wherein the encapsulating layer comprises a film adhesive, a pre-impregnated fabric, a polyimide, or a neoprene. 16. The heating element of claim 1 , wherein the encapsulating layer faces the breeze side of an aircraft component.
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