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The present invention is directed to a method for applying to a substrate having a faying surface, a polysiloxane-containing coating, preferably a polysiloxane(amide-ureide) coating capable of inhibiting corrosion as well as the accumulation of ice. One embodiment of the present invention is directe

The present invention is directed to a method for applying to a substrate having a faying surface, a polysiloxane-containing coating, preferably a polysiloxane(amide-ureide) coating capable of inhibiting corrosion as well as the accumulation of ice. One embodiment of the present invention is directed to a polysiloxane(amide-ureide) that forms a durable, long lasting, anti-corrosive and anti-ice coating when directed to a substrate faying surface.

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1. A coating for use on a component surface, said coating comprising a polymer comprising Component A and Component B, wherein Component A is a compound comprising the formula:and wherein Component B is a compound comprising the formula:or a compound comprising the formula: wherein X is a pre

1. A coating for use on a component surface, said coating comprising a polymer comprising Component A and Component B, wherein Component A is a compound comprising the formula:and wherein Component B is a compound comprising the formula:or a compound comprising the formula: wherein X is a prepolymer comprising the formula: wherein R 1 , R 3 , and R 4 are independently selected from the group consisting of hydrogen; C 1 to C 6 alkyls and aryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;A 1 and A 2 are independently selected from the group consisting of C 1 to C 6 alkyls and aryls; C 7 to C 12 alkylaryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;R 2 , R 5 , and R 6 are independently selected from the group consisting of C 1 to C 10 alkyls; aryls, and heterocycles;m and x are each a number from 1 to about 10,000;CYAN is a diisocyanate residue; andZ is a halide-substituted dicarboxylic acid residue. 2. The coating of claim 1, wherein the diisocyanate is selected from the group consisting of alkyl diisocyanate, wherein the alkyl portion is from C 1 to C 10 ; non-linear aryl diisocyanate; and non-linear heterocyclic diisocyanate. 3. The coating of claim 1, wherein at least a portion if the substituted dicarboxylic acid is selected from the group consisting of fumaryl halides, succinyl halides, phthalyl halides, terephthalyl halides, and maleiyl halides. 4. The coating of claim 1, wherein the component comprises an aircraft component. 5. The coating of claim 1, wherein the component surface comprises a faying surface. 6. A substrate comprising a surface coated with a coating, said coating comprising a polymer, said polymer comprising a Component A and a Component B, wherein Component A is a compound comprising the formula:and wherein Component B is a compound comprising the formula:or a compound comprising the formula: wherein X is a prepolymer comprising the formula wherein R 1 , R 3 , and R 4 are independently selected from the group consisting of hydrogen; C 1 to C 6 alkyls and aryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;A 1 and A 2 are independently selected from the group consisting of C 1 to C 6 alkyls and aryls; C 7 to C 12 alkylaryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;R 2 , R 5 , and R 6 are independently selected from the group consisting of C 1 to C 10 alkyls; aryls, and heterocycles;m and x are each a number from 1 to about 10.000;CYAN diisocyanate residue; andZ is a halide-substituted dicarboxylic acid residue. 7. The substrate of claim 6, wherein the diisocyanate is selected from the group consisting of alkyl diisocyanate, wherein the alkyl portion is from C 1 in C 10 ; non-linear aryl diisocyanate; and non-linear heterocyclic diisocyanate. 8. The substrate of claim 6, wherein at least a portion of the substituted dicarboxylic acid is selected from the group consisting of fumaryl halides, succinyl halides, phthalyl halides, terephthalyl halides, and maleiyl halides. 9. The substrate of claim 6 wherein the dicarboxylic component is selected from fumaryl moieties, maleiyl moieties, saturated C 4 to C 8 dicarboxylic moieties, and partially-saturated C 4 to C 8 dicarboxylic moieties. 10. The substrate of claim 6, wherein greater than approximately 50 mol % of the dicarboxylic component of the polymer comprises fumaryl moieties. 11. The substrate of claim 6, wherein greater than approximately 80 mol % of the dicarboxylic component of the polymer comprises fumaryl moieties. 12. The substrate of claim 6, wherein R 1 and R 2 are independently selected from the group consisting of methyl, ethyl, propyl, butyl, and phenyl, moieties. 13. The substrate of claim 6, wherein at least one of R 1 and R 2 are selected from the group consisting of halogenated alkyls and halogenated aryls. 14. The substrate of claim 6, wherein A 1 and A 2 are independently selected from the group co nsisting of methyl, ethyl, propyl, butyl, and phenyl moieties. 15. The substrate of claim 6, wherein at least one of A 1 and A 2 are selected from the group consisting of halogenated alkyls, halogenated aryls, halogenated alkylaryls, halogentated cycloaliphatics, and halogenated heterocycles. 16. The substrate of claim 6, wherein the diisocyanate component comprises an aromatic diisocyante. 17. The substrate of claim 6, wherein the diisocyanate component comprises toluene-2,4-diisocyanate. 18. The substrate of claim 6, wherein the diisocyanate component comprises a saturated aliphatic diisocyanate. 19. The substrate of claim 6, wherein x is a number from 1 to about 1000. 20. The substrate of claim 6, wherein x is a number from about 20 to about 200. 21. The substrate of claim 6, wherein the substrate comprises an aircraft component. 22. The substrate of claim 6, wherein the surface comprises a faying surface. 23. The substrate of claim 6, wherein the coating inhibits the ability of ice to adhere to a surface of the aircraft component surface. 24. The substrate of claim 6, wherein the coating inhibits the ability of moisture to adhere to a surface of the aircraft component surface. 25. The substrate of claim 6, wherein the substrate further comprises a subsequent coating applied to the polymer coating. 26. The substrate of claim 6, wherein the substrate further comprises a pre-treatment applied to the substrate surface. 27. The substrate of claim 26, wherein the pre-treatment is selected from the group consisting of ZnNi pre-treatment, Cd flash pre-treatment, and an anodizing pre-treatment process. 28. The substrate of claim 6, wherein the substrate further comprises a first coating applied to the substrate, with the polymer coating applied to the first coating as a secondary coating. 29. The substrate of claim 28, wherein the first coating comprises a curable organic coating material selected from the group consisting of phenolics, urethanes, epoxies, and melamines. 30. The substrate of claim 28, wherein the first coating comprises a curable organic coating material selected from the group consisting of polyurethanes, polyvinyl chlorides, silicones, epoxides, acrylates, polyimides, and phenolics. 31. The substrate of claim 6, wherein the substrate is made from a material selected from the group consisting of: aluminum alloys, ferrous alloys, and non-metallic materials. 32. The substrate of claim 31, wherein the non-metallic material is selected from the group consisting of ceramic-, epoxy-, glass-, wood-, and carbon-containing materials. 33. The substrate of claim 6, wherein the substrate comprises an aluminum-alloy aircraft component. 34. The substrate of claim 28, wherein the substrate comprises an aluminum-alloy aircraft component. 35. An aircraft comprising the substrate of claim 6. 36. An aircraft comprising the substrate of claim 28. 37. A method for coating the surface of a component with a corrosion-inhibiting coating comprising the steps of:providing a component having a surface;providing a coating material, said coating material comprising a polymer comprising Component A and Component B, wherein Component A is a compound comprising the formula: and wherein Component B comprises a compound comprising the formula: or a compound comprises the formula: wherein X is a prepolymer comprising the formula: wherein R 1 , R 3 , and R 4 are independently selected from the group consisting of hydrogen; C 1 to C 6 alkyls and aryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;A 1 and A 2 are independently selected from the group consisting of C 1 to C 6 alkyls and aryls; C 1 to C 12 alkylaryls; C 3 to C 6 cycloaliphatics; and C 3 to C 6 heterocycles;R 2 , R 5 , and R 6 are independently selected from the group consisting of C 1 to C 10 alkyls; aryls, and heterocycles;m and x are each a number from 1 to about 10,000;CYAN is a diisocyanate residue;Z is a halide-substi tuted dicarboxylic acid residue; andapplying the polymer coating to the surface. 38. The method of the claim 37, wherein the dicarboxylic component is selected from fumaryl moieties, maleiyl moieties, saturated C 4 to C 8 dicarboxylic moieties, and partially-saturated C 4 to C 8 dicarboxylic moieties. 39. The method of claim 37, wherein greater than approximately 50 mol % of the dicarboxylic component of the polymer comprises fumaryl moieties. 40. The method of claim 37 wherein greater than approximately 80 mol % of the dicarboxylic component of the polymer comprises fumaryl moieties. 41. The method of claim 37, wherein R 1 and R 2 are independently selected from the group consisting of methyl, ethyl, propyl, butyl, and phenyl moieties. 42. The method of claim 37, wherein at least one of R 1 and R 2 are selected from the group consisting of halogenated alkyls and halogenated aryls. 43. The method of claim 37, wherein A 1 and A 2 are independently selected from the group consisting of methyl, ethyl, propyl, butyl, and phenyl moieties. 44. The method of claim 37, wherein at least one of A 1 and A 2 are selected from the group consisting of halogenated alkyls, halogenated aryls, halogenated alkylaryls, halogentated cycloaliphatics, and halogenated heterocycles. 45. The method of claim 37, wherein the diisocyanate component comprises an aromatic diisocyante. 46. The method of claim 37, wherein the diisocyanate component comprises toluene-2,4-diisocyanate. 47. The method of claim 37, wherein the diisocyanate component comprises a saturated aliphatic diisocyanate. 48. The method of claim 37, wherein x is a number from 1 to about 1000. 49. The method according to claim 37, wherein x is a number from about 20 to about 200. 50. The method of claim 37, further comprising the steps of providing a first coating between the component surface and the polymer coating. 51. The method of claim 50, wherein the first coating comprises a curable organic coating material selected from the group consisting of phenolics, urethanes, epoxies, and melamines. 52. The method of claim 50, wherein the first coating comprises a curable organic coating material selected from the group consisting of polyurethanes, polyvinyl chlorides, silicones, epoxides, acrylates, polyimides, and phenolics. 53. The method according to claim 37, wherein the component comprises an aircraft component. 54. The method of claim 37, wherein the component is made from a material selected from the group consisting of: aluminum alloys, ferrous alloys, and non-metallic materials. 55. The method of claim 37, further comprising the step of applying a second coating to the polymer coating. 56. The method of claim 37, further comprising the step of applying a pre-treatment to the component surface. 57. The substrate of claim 37, wherein the pre-treatment is selected from the group consisting of a ZnNi pre-treatment and an anodizing pre-treatment. 58. The method of claim 37, wherein the surface comprises a faying surface. 59. An aircraft comprising components comprising surfaces coated according to the method of claim 37. 60. An aircraft comprising components comprising surfaces coated according to the method of claim 50. 61. The method of claim 37, wherein the coating inhibits the ability of ice to adhere to a component surface. 62. The method of claim 37, wherein the coating inhibits the ability of moisture to adhere to a component surface. 63. The method of claim 50, wherein the coating inhibits the ability of ice to adhere to a surface of the aircraft component surface. 64. The method claim 50, wherein the coating inhibits the ability of moisture to adhere to a surface of the aircraft component surface.