Nonwoven laminate
US-12152326-B1 · Nov 26, 2024 · US
US10000272B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10000272-B2 |
| Application number | US-201415106904-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 23, 2014 |
| Priority date | Dec 23, 2013 |
| Publication date | Jun 19, 2018 |
| Grant date | Jun 19, 2018 |
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.
The present invention pertains to an insulation system comprising one or more insulation blankets, wherein each of said multilayer insulation blankets comprises: —a core consisting of an insulation material [material (I)], and —a shell encapsulating said core, said shell comprising at least one multilayer assembly comprising: (1) an outer layer [layer (L1)] consisting of a composition [composition (C1)] comprising, preferably consisting of, at least one thermoplastic polymer [polymer (1)] having a limiting oxygen index (LOI) of at least 20% by volume, wherein at least one surface, preferably the inner surface, of said layer (L1) comprises one or more grafted functional groups [surface (L1-f)], (2) directly adhered to said at least one surface (L1-f), a layer consisting of at least one metal compound (M1) [layer (L2)], and (3) optionally, directly adhered to the opposite side of the layer (L2), a layer consisting of at least one metal compound (M2) [layer (L3)], said metal compound (M2) being equal to or different from said metal compound (M1). The present invention also pertains to a process for the manufacture of said insulation system and to uses of said insulation system in various applications including aircraft applications.
Opening claim text (preview).
The invention claimed is: 1. A process for the manufacture of an insulation system comprising one or more insulation blankets, said process comprising: encapsulating a core consisting of an insulation material (I) with a shell comprising a multilayer assembly, said multilayer assembly being obtained by: treating at least one surface of a layer (L1) by a radio-frequency glow discharge process in the presence of an etching gas medium, wherein layer (L1) consists of a composition (C1) comprising at least one poly(aryl ether ketone) polymer having a limiting oxygen index (LOI) of at least 30% by volume, applying by electroless deposition a layer (L2) onto said at least one treated surface of layer (L1), wherein layer (L2) consists of at least one metal compound (M1), and optionally, applying by electro-deposition a layer (L3) onto the opposite side of layer (L2) wherein layer (L3) consists of at least one metal compound (M2), said metal compound (M2) being equal to or different from said metal compound (M1). 2. The process according to claim 1 , wherein layer (L1) is the outer layer of the shell. 3. The process according to claim 1 , wherein the etching gas medium is selected from the group consisting of air, N 2 , NH 3 , CH 4 , CO 2 , He, O 2 , H 2 and mixtures thereof. 4. The process according to claim 3 , wherein the etching gas medium comprises N 2 and/or NH 3 and, optionally, H 2 . 5. The process according to claim 1 , wherein metal compound (M1) is selected from the group consisting of Rh, Ir, Ru, Ti, Re, Os, Cd, Tl, Pb, Bi, In, Sb, Al, Ti, Cu, Ni, Pd, V, Fe, Cr, Mn, Co, Zn, Mo, W, Ag, Au, Pt, Ir, Ru, Pd, Sn, Ge, Ga, alloys thereof and derivatives thereof. 6. The process according to claim 1 , wherein layer (L3) is applied onto the opposite side of the layer (L2) by electro-deposition. 7. The process according to claim 6 , wherein metal compound (M2) is selected from the group consisting of Rh, Ir, Ru, Ti, Re, Os, Cd, Tl, Pb, Bi, In, Sb, Al, Ti, Cu, Ni, Pd, V, Fe, Cr, Mn, Co, Zn, Mo, W, Ag, Au, Pt, Ir, Ru, Pd, Sn, Ge, Ga, alloys thereof and derivatives thereof. 8. An insulation system comprising one or more multilayer insulation blankets, wherein each of said multilayer insulation blankets comprises: a core consisting of an insulation material (I), and a shell encapsulating said core, said shell comprising at least one multilayer assembly comprising: (1) an outer layer (L1) consisting of a composition (C1) comprising at least one poly(aryl ether ketone) polymer having a limiting oxygen index (LOI) of at least 30% by volume, wherein at least one surface (L1-f) of said layer (L1) comprises one or more grafted functional groups, (2) directly adhered to said at least one surface (L1-f), a layer (L2) consisting of at least one metal compound (M1), and (3) optionally, directly adhered to the opposite side of the layer (L2), a layer (L3) consisting of at least one metal compound (M2), said metal compound (M2) being equal to or different from said metal compound (M1). 9. The insulation system according to claim 8 , wherein the one or more grafted functional groups are selected from the group consisting of amine groups (—NH 2 ), imine groups (—CH═NH), nitrile groups (—CN) and amide groups (—CONH 2 ). 10. The insulation system according to claim 8 , wherein layer (L2) has a thickness between 0.05 μm and 5 μm. 11. The insulation system according to claim 8 , wherein layer (L3), if any, has a thickness between 0.1 μm and 30 μm. 12. An aircraft insulation system comprising the insulation system according to claim 8 . 13. The process according to claim 1 , wherein composition (C1) consists of at least one thermoplastic polymer (1) having a limiting oxygen index (LOI) of at least 20% by volume. 14. The insulation system according to claim 8 , wherein composition (C1) consists of at least one thermoplastic polymer (1) having a limiting oxygen index (LOI) of at least 20% by volume. 15. The insulation system according to claim 10 , wherein layer (L2) has a thickness between 0.8 μm and 1.5 μm. 16. The insulation system according to claim 11 , wherein layer (L3), if any, has a thickness between 1 μm and 15 μm.
Insulating · CPC title
Polyureas; Polyurethanes · CPC title
Synthetic macromolecular fibres · CPC title
specially treated, e.g. irradiated · CPC title
Inorganic fibres · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.