Installation of pneumatic de-icers with vertically aligned carbon nanotubes
US-2019292420-A1 · Sep 26, 2019 · US
US2023121788A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2023121788-A1 |
| Application number | US-202218059745-A |
| Country | US |
| Kind code | A1 |
| Filing date | Nov 29, 2022 |
| Priority date | Dec 16, 2018 |
| Publication date | Apr 20, 2023 |
| Grant date | — |
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A method of making an adhesive for an ice protection assembly includes transferring Z-CNTs from a substrate carrier into the adhesive. De-bonding of the adhesive for ice protection assembly inspection or repair or repositioning at initial installation includes heating the Z-CNTs in the adhesive to soften the adhesive and allow for easy removal.
Opening claim text (preview).
1 . A method of bonding an ice protection assembly to an aircraft component comprising: applying a primer on a surface of the aircraft component, wherein the primer is configured to increase adhesion of the adhesive on the surface; applying an adhesive on the primer on the surface of the aircraft component, wherein the adhesive is loaded with vertically aligned carbon nanotubes (Z-CNTs); and attaching a de-icer to the aircraft component by the adhesive. 2 . The method of claim 1 , wherein the aircraft component is selected from the group consisting of an airfoils, nacelles, nosecones, engine cowls, and leading edges. 3 . The method of claim 1 , wherein the adhesive comprises a thermoplastic adhesive. 4 . The method of claim 3 , wherein the thermoplastic adhesive is pressure sensitive adhesive, selected from the group consisting of include acrylates, silicones, nitriles, and styrenes. 5 . The method of claim 3 , wherein the thermoplastic adhesive is hot melt adhesive. 6 . The method of claim 1 , wherein the Z-CNTs are no more than 50% by weight of the adhesive. 7 . The method of claim 1 , wherein the de-icer is pneumatic de-icer or an electrothermal de-icer. 8 . The method of claim 1 , wherein the Z-CNTs are aligned at a 90 degree angle relative to the adhesive surface. 9 . The method of claim 1 , wherein the Z-CNTs are parallel to the adhesive surface. 10 . A method of preparing an adhesive comprising infiltrating the adhesive with vertically aligned carbon nanotubes (Z-CNTs). 11 . The method of claim 11 , wherein infiltrating the adhesive comprises applying a substrate with Z-CNTs to the adhesive. 12 . The method of claim 10 , wherein the adhesive comprises a thermoplastic adhesive. 13 . The method of claim 12 , wherein the thermoplastic adhesive is pressure sensitive adhesive, selected from the group consisting of include acrylates, silicones, nitriles, and styrenes. 14 . The method of claim 12 , wherein the thermoplastic adhesive is hot melt adhesive. 15 . The method of claim 10 , wherein the Z-CNTs are no more than 50% by weight of the adhesive. 16 . A method of de-bonding an adhesive from a component comprising: electrically connecting the adhesive to a power source; running voltage through the adhesive so that Z-CNTs in the adhesive heat and soften the adhesive; and removing the softened adhesive. 17 . The method of claim 16 , further comprising repositioning the adhesive. 18 . The method of claim 17 , wherein the Z-CNTs comprise no more than 50% by weight of the adhesive. 19 . The method of claim 16 , wherein removing the softened adhesive comprises scrapping, pulling, or peeling the adhesive off the component. 20 . The method of claim 16 , wherein the adhesive comprises a thermoplastic adhesive and the Z-CNTs are no more than 50% by weight of the adhesive.
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