Uniform Heat Distribution in Resistive Heaters For Anti-Icing and De-Icing
US-2016221680-A1 · Aug 4, 2016 · US
US11382181B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11382181-B2 |
| Application number | US-201615368271-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 2, 2016 |
| Priority date | Dec 2, 2016 |
| Publication date | Jul 5, 2022 |
| Grant date | Jul 5, 2022 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method for creating a carbon nanotube heater assembly includes creating a carbon nanotube heater with varying resistances and attaching the carbon nanotube heater to both carrier and encapsulating materials. Creating the carbon nanotube heater with varying resistances is accomplished by applying a carbon nanotube mixture to a substrate, adjusting the thickness or width of the carbon nanotube mixture, and drying the nanotube mixture.
Opening claim text (preview).
The invention claimed is: 1. A carbon nanotube heater assembly comprising: a carbon nanotube heater comprising a carbon nanotube coating applied to a substrate such that the thickness and width of the carbon nanotube coating vary along the substrate to vary the resistance of the carbon nanotube coating along the substrate; a carrier material attached to the carbon nanotube heater; an encapsulating material attached to the carbon nanotube heater opposite the carrier material; and an adhesive layer bonding the encapsulating material to an aircraft part. 2. The assembly of claim 1 , wherein the carbon nanotube heater is contoured to curves of an aircraft part. 3. The assembly of claim 1 , wherein the carrier material is selected from the group consisting of a film adhesive, a pre-impregnated fabric, a polyimide, and a neoprene. 4. The assembly of claim 1 , wherein the encapsulating material is selected from the group consisting of a film adhesive, a pre-impregnated fabric, a polyimide, and a neoprene.
Manufacture or treatment of nanostructures · CPC title
Carbon nanotubes, CNTs · CPC title
Two layers · CPC title
Heaters specially designed for de-icing or protection against icing · CPC title
Heaters using resistive films or coatings · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.