Articles for manipulating impinging liquids and methods of manufacturing same

US9254496B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9254496-B2
Application numberUS-201113300022-A
CountryUS
Kind codeB2
Filing dateNov 18, 2011
Priority dateAug 3, 2011
Publication dateFeb 9, 2016
Grant dateFeb 9, 2016

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  1. Title

    What the patent document calls the invention.

  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

This invention relates generally to an article that includes a non-wetting surface having a dynamic contact angle of at least about 90°. The surface is patterned with macro-scale features configured to induce controlled asymmetry in a liquid film produced by impingement of a droplet onto the surface, thereby reducing time of contact between the droplet and the surface.

First claim

Opening claim text (preview).

What is claimed is: 1. An article comprising a non-wetting surface having a dynamic contact angle of at least about 90°, said surface comprising non-wetting features, said surface patterned with macro-scale features having a length scale L m that is larger than a length scale L n of the non-wetting features, the macro-scale features being configured to induce controlled asymmetry in a liquid film produced by impingement of a droplet onto the surface, thereby reducing contact time t c between the droplet and the surface to a value lower than 2.2(( ρR^ 3)/γ)^(½)(1+φ/4) where the droplet has a radius R, density ρ, surface tension γ, and the patterned surface having a pinning fraction φ of zero. 2. The article of claim 1 , wherein the non-wetting surface is superhydrophobic. 3. The article of claim 1 , wherein the non-wetting surface is superoleophobic. 4. The article of claim 1 , wherein the non-wetting surface is supermetallophobic. 5. The article of claim 1 , wherein the non-wetting features are nanoscale pores. 6. The article of claim 1 , wherein the surface is heated above its Leidenfrost temperature. 7. The article of claim 1 , wherein the macro-scale features comprise ridges having height A r and spacing λ r , with A r /h greater than about 0.01 and λ r /A r greater than or equal to about 1, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 8. The article of claim 1 , wherein the macro-scale features comprise ridges having height A r and spacing λ r , with A r /h from about 0.01 to about 100 and λ r /A r greater than or equal to about 1, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 9. The article of claim 1 , wherein the macro-scale features comprise ridges having height A r and spacing λ r , with A r /h from about 0.1 to about 10 and λ r /A r greater than or equal to about 1, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 10. The article of claim 1 , wherein the article is a wind turbine blade, the macro-scale features comprise ridges having height A r and spacing λ r , and wherein 0.0001 mm<A r and λ r ≧0.0001 mm. 11. The article of claim 1 , wherein the article is a rainproof product, the macro-scale features comprise ridges having height A r and spacing λ r , and wherein 0.0001 mm<A r and λ r ≧0.0001 mm. 12. The article of claim 1 , wherein the article is a steam turbine blade, the macro-scale features comprise ridges having height A r and spacing λ r , and wherein 0.00001 mm<A r and λ r ≧0.0001 mm. 13. The article of claim 1 , wherein the article is an exterior aircraft part, the macro-scale features comprise ridges having height A r and spacing λ r , and wherein 0.00001 mm<A r and λ r ≧0.0001 mm. 14. The article of claim 1 , wherein the article is a gas turbine blade, the macro-scale features comprise ridges having height A r and spacing λ r , and wherein 0.00001 mm<A r and λ r ≧0.0001 mm. 15. The article of claim 1 , wherein the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , with A p /h>0.01 and λ p /A p ≧2, wherein h is lamella thickness of the droplet upon impingement onto the surface. 16. The article of claim 1 , wherein the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , with 100>A p /h>0.01 and λ p /A p ≧2, wherein h is lamella thickness of the droplet upon impingement onto the surface. 17. The article of claim 1 , wherein the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , with 10>A p /h>0.1 and λ p /A p ≧2, wherein h is lamella thickness of the droplet upon impingement onto the surface. 18. The article of claim 1 , wherein the macro-scale features are hemispherical protrusions. 19. The article of claim 1 , wherein the article is a wind turbine blade, the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , and wherein 0.0001 mm<A p and λ p ≧0.0002 mm. 20. The article of claim 1 , wherein the article is a rainproof product, the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , and wherein 0.0001 mm<A p and λ p ≧0.0002 mm. 21. The article of claim 1 , wherein the article is a steam turbine blade, the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , and wherein 0.00001 mm<A p and λ p ≧0.00002 mm. 22. The article of claim 1 , wherein the article is an exterior aircraft part, the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , and wherein 0.00001 mm<A p and λ p ≧0.00002 mm. 23. The article of claim 1 , wherein the article is a gas turbine blade, the macro-scale features comprise protrusions having height A p and whose centers are separated by a distance λ p , and wherein 0.00001 mm<A p and λ p ≧0.00002 mm. 24. The article of claim 1 , wherein the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , with A c /h>0.01 and λ c /A c ≧2, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 25. The article of claim 1 , wherein the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , with 100>A c /h>0.01 and 500≧λ c /A c ≧2, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 26. The article of claim 1 , wherein the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , with 50>A c /h>0.1 and 500≧λ c /A c ≧2, wherein h is lamella thickness of the droplet upon droplet impingement onto the surface. 27. The article of claim 1 , wherein the article is a rainproof product, the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , and wherein 0.0001 mm<A c and λ c ≧0.0002 mm. 28. The article of claim 1 , wherein the article is a wind turbine blade, the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , and wherein 0.0001 mm<A c and λ c ≧0.0002 mm. 29. The article of claim 1 , wherein the article is a steam turbine blade, the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , and wherein 0.00001 mm<A c and λ c ≧0.00002 mm. 30. The article of claim 1 , wherein the article is an exterior aircraft part, the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , and wherein 0.00001 mm<A c and λ c ≧0.00002 mm. 31. The article of claim 1 , wherein the article is a gas turbine blade, the macro-scale features comprise a sinusoidal profile having amplitude A c and period λ c , and wherein 0.00001 mm<A c and λ c ≧0.00002 mm. 32. The article of claim 1 , wherein the surface comprises an alkane. 33. The article of claim 1 , wherein the surface comprises a fluoropolymer. 34. The article of claim 1 , wherein the surface comprises at least one member selected from the group consisting of teflon, trichloro(1H,1H,2H,2H-perfluorooctyDsilane (TCS

Assignees

Inventors

Classifications

  • Nanotechnology for materials or surface science, e.g. nanocomposites · CPC title

  • Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.] · CPC title

  • the surface having a microscopic surface pattern to achieve the same effect as a lotus flower · CPC title

  • to obtain a matt or rough surface · CPC title

  • B05B1/26Primary

    with means for mechanically breaking-up or deflecting the jet after discharge, e.g. with fixed deflectors; Breaking-up the discharged liquid or other fluent material by impinging jets · CPC title

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What does patent US9254496B2 cover?
This invention relates generally to an article that includes a non-wetting surface having a dynamic contact angle of at least about 90°. The surface is patterned with macro-scale features configured to induce controlled asymmetry in a liquid film produced by impingement of a droplet onto the surface, thereby reducing time of contact between the droplet and the surface.
Who is the assignee on this patent?
Dhiman Rajeev, Bird James C, Kwon Hyukmin, and 2 more
What technology area does this patent fall under?
Primary CPC classification B05B1/26. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Feb 09 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).