Lightweight particles and compositions containing them
US-8993691-B2 · Mar 31, 2015 · US
US9951251B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9951251-B2 |
| Application number | US-201514963976-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 9, 2015 |
| Priority date | Aug 13, 2008 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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Particles that have an exterior surface coated with a thin polymer coating, such as a coating that includes a sulfur-containing polymer can be used as lightweight fillers in compositions, such as fuel resistant sealant and coating compositions. The compositions can be used to seal apertures on aerospace vehicles.
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We claim: 1. A composition comprising: a) a polymeric film-forming binder comprising reactive functional groups; and b) particles dispersed in the binder, wherein, the particles comprise expanded thermoplastic microcapsules comprising an exterior surface having a coating thereon wherein the coating comprises an aminoplast resin; the aminoplast resin-coated expanded thermoplastic microcapsules are characterized by a specific gravity of no more than 0.1; the composition comprises less than 5 wt % of the aminoplast resin-coated expanded thermoplastic microcapsules, wherein wt % is based on the total weight of the composition; and the composition is formulated as an aerospace sealant having a specific gravity of less than 1.0. 2. The composition of claim 1 , wherein the polymeric film-forming binder comprises a sulfur-containing polymer. 3. The composition of claim 2 , wherein the sulfur-containing polymer comprises a thiol-functional polythioether. 4. The composition of claim 1 , wherein the aminoplast resin comprises melamine. 5. The composition of claim 1 , further comprising a curing agent. 6. The composition of claim 5 , wherein the curing agent comprises a polyepoxide. 7. A cured sealant, comprising the composition of claim 1 . 8. The cured sealant of claim 7 , having a tensile strength of 1900 mega-Pascals or greater measured according to AS 5127/1a7.7. 9. The cured sealant of claim 7 , wherein the cured sealant exhibits: a percent volume swell of not greater than 40% after immersion for one week at 140° F. (60° C.) and ambient pressure in Jet Reference Fluid Type 1; an elongation of at least 80% measured as described in AMS 3269a; and a tensile strength of at least 2000 mega-Pascals when measured according to AS 5127/1a7.7. 10. An aerospace vehicle, having an aperture at least partially sealed with a sealant deposited from the composition of claim 1 . 11. An aerospace vehicle, having an aperture at least partially sealed with a sealant deposited from the composition of claim 6 . 12. A composition comprising: c) a sulfur-containing polymer binder; d) a curing agent comprising a polyepoxide; and e) particles dispersed in the binder, wherein, the particles comprise expanded thermoplastic microcapsules comprising an exterior surface having a coating thereon wherein the coating comprises an aminoplast resin; the aminoplast resin-coated expanded thermoplastic microcapsules are characterized by a specific gravity of no more than 0.1, and a particle size from 5 μm to 300 μm; the composition comprises less than 5 wt % of the aminoplast resin-coated expanded thermoplastic microcapsules, wherein wt % is based on the total weight of the composition; and the composition is formulated as an aerospace sealant having a specific gravity of less than 1.0. 13. The composition of claim 12 , wherein the sulfur-containing polymer binder comprises a thiol-functional polythioether. 14. The composition of claim 13 , further comprising a reinforcing filler and/or an adhesion promoter. 15. The composition of claim 14 , wherein the reinforcing filler comprises calcium carbonate. 16. The composition of claim 14 , wherein the adhesion promoter comprises a silane. 17. A composition comprising: a) a thiol-functional polythioether binder; b) a curing agent comprising a polyepoxide; c) a reinforcing filler; d) an adhesion promoter; and particles dispersed in the composition, wherein the particles dispersed in the binder, wherein, the particles comprise expanded thermoplastic microcapsules comprising an exterior surface having a coating thereon wherein the coating comprises an aminoplast resin; the aminoplast resin-coated expanded thermoplastic microcapsules are characterized by a specific gravity of no more than 0.1, and a particle size from 5 μm to 300 μm; the composition comprises less than 5 wt % of the aminoplast resin-coated expanded thermoplastic microcapsules, wherein wt % is based on the total weight of the composition; and the composition is formulated as an aerospace sealant having a specific gravity of less than 1.0. 18. An aerospace vehicle having an aperture at least partially sealed with a sealant deposited from the composition of claim 17 . 19. The composition of claim 1 , wherein the composition comprises from 1 wt % to less than 5 wt % of the aminoplast resin-coated expanded thermoplastic microcapsules, wherein wt % is based on the total weight of the composition. 20. The cured sealant of claim 7 , which when cured exhibits: a percent volume swell of not greater than 40% after immersion for one week at 140° F. (60° C.) and ambient pressure in Jet Reference Fluid Type 1; an elongation of at least 80% measured as described in AMS 3269a; and a tensile strength of at least 2000 mega-Pascals when measured according to AS 5127/1a7.7. 21. The composition of claim 1 , wherein the specific gravity of the composition is less than 0.9. 22. The composition of claim 1 , wherein the specific gravity of the composition is less than 0.8. 23. The composition of claim 1 , wherein the composition comprises a reinforcing filler.
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