Cooling device with an endothermic chemical reaction
US-2021396447-A1 · Dec 23, 2021 · US
US9346994B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9346994-B2 |
| Application number | US-201113642821-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 19, 2011 |
| Priority date | Apr 22, 2010 |
| Publication date | May 24, 2016 |
| Grant date | May 24, 2016 |
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 heat protection material for a surface, made of a mixture comprising a resin, cork granules and refractory fibers; the proportion of cork granules in the mixture is 50 to 80% by mass, wherein the corresponding proportion of refractory fibers in the mixture is 1 to 11% by mass.
Opening claim text (preview).
The invention claimed is: 1. A heat protection ablative material for protecting a surface of a space vehicle from heat, having a mixture comprising a phenolic resin with a content of coke above 50% when heated to 1,000° C. in an inert atmosphere such as nitrogen, cork granules and refractory fibers, in which the proportion of cork granules in the mixture is a percentage from 70 to 73% by mass, wherein the percentage by mass in the mixture of refractory fibers is between 1 and 3% while the percentage by mass in the mixture of resin is the range of 23-25% and the material being so designed to withstand heat flows ranging from 0.5 to 10 MW/m2, and the material contains no microspheres. 2. Heat protection material according to claim 1 , comprising 0.5 to 1.5% percentage by mass of fungicide. 3. Heat protection material according to claim 1 , wherein the cork is flame-proofed cork. 4. Heat protection material according to claim 1 , comprising a density between 0.35 and 0.41 kg/L after degassing. 5. Heat protection material according to claim 1 , comprising a density of 0.38 kg/L after degassing. 6. Heat protection material according to claim 1 , wherein the refractory fibers are carbon fibers between 0.4 and 4 mm long. 7. Heat protection material according to claim 1 , wherein the refractory fibers are alumina fibers between 0.4 and 4 mm long. 8. A heat protection ablative material for protecting a surface of a space vehicle from heat, having a mixture comprising a phenolic resin with a content of coke above 50% when heated to 1,000° C. in an inert atmosphere such as nitrogen, cork granules and refractory fibers, in which the proportion of cork granules in the mixture is a percentage from 65 to 68% by mass, wherein the percentage by mass in the mixture of refractory fibers is between is between 9 and 11% while the percentage by mass in the mixture of resin is the range of 21-24% the material being so designed to withstand heat flows ranging from 0.5 to 10 MW/m2, the material containing no microspheres. 9. Heat protection material according to claim 8 , comprising 0.5 to 1.5% percentage by mass of fungicide. 10. Heat protection material according to claim 8 , wherein the cork is flame-proofed cork. 11. Heat protection material according to claim 8 , comprising a density between 0.35 and 0.41 kg/L after degassing. 12. Heat protection material according to any claim 8 , comprising a density of 0.38 kg/L after degassing. 13. Heat protection material according to claim 8 , wherein the refractory fibers are carbon fibers between 0.4 and 4 mm long. 14. Heat protection material according to claim 8 , wherein the refractory fibers are alumina fibers between 0.4 and 4 mm long.
Related publications grouped by family.
Answers are generated from the same data shown on this page.