An air cured composite coating and method for applying same

Abstract

 An air cured composite coating for providing an abrasion resistant release surface to a substrate which comprises a metal matrix thermally sprayed onto a substrate and a film forming polymerized silicon impregnate applied to the metal matrix to seal its porosity. The composite coating is air cured in situ and exhibits a hardness of up to 72 Rc. The coating maintains thermal stability at continuous operating temperature of up to 400 degrees fahrenheit.

Description

BACKGROUND OF THE INVENTION

[0001] The present invention relates to a composite coating which imparts an abrasion resistant release surface to a substrate and a method for applying the coating to the substrate. More particularly, the present invention relates to an air cured composite coating comprising a porous metal matrix and a silicon impregnant which seals the porosity of the matrix.

[0002] Composite coatings applied to substrates to a enhance their abrasion resistence and release properties are old in the art. Prior art composite coatings usually include either a ceramic or a metal matrix applied to substrate, with the matrix being impregnated with a silicon polymer or fluorocarbon polymer release agent. The major drawback to all the prior art composite coatings is that they must be heat cured at temperatures near or above 500 degrees fahrenheit. Heat curing of the composite coating presents significant problems where the substrate is of substantial size or weight or where the substrate is a component of a larger machine. Where the substrate is large and/or heavy, it may be expensive to ship the substrate to a distant coating facility. Further, when the substrate is a component of a larger machine, productivity of the machine is lost while the component is removed from the machine and sent away to be coated.

SUMMARY OF THE INVENTION

[0003] It is the general object of the described embodiments to provide a composite coating which imparts an abrasion resistant release surface to a substrate where, because the composite coating is air cured, it can be applied on site. That is, because the composite coating of the present invention does not require oven-heating for proper curing, the substrate does not have to be shipped to a distant coating facility. The air cured composite coating of the present invention comprises a porous metal matrix impregnated with a silicone to seal the porosity of the matrix. The coating is continuously operable to temperatures of up to 400 degrees fahrenheit and exhibits a hardness of up to 72 Rc.

BRIEF DESCRIPTION OF THE DRAWINGS

[0004] 

Fig. 1 is a semi-schematic, enlarged, cross-sectional view of a substrate having a composite layer produced in accordance with the present invention.

Fig. 2 is an enlarged cross-section of Fig. 1 on the line 2-2.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0005] In accordance with the present invention, a porous metal matrix is initially formed on a substrate and then impregnated with a film forming, polymerizable, silicon impregnate which is polymerized in situ to serve as a release agent. The resulting composite coating thus formed has the abrasion resistance of the metal matrix and the release properties of the impregnating silicon.

[0006] Referring to Fig. 1, a substrate coated with the air cured conposite coating of the present invention is shown generally at 10. The substrate 12, such as an idler roller or drum, carries the composite coating, represented at 14. As shown in Fig. 2, the composite coating comprises a porous metal matrix which in cross section exhibits a multitude of depressions 16 and plateaus 18 formed therein. A film forming, polymerized, silicon impregnate 20 fills the depressions 16 in the matrix 14 and penetrates into the matrix to seal its porosity. It is also preferred that an excess of the impregnate 20 extends above the plateaus 18 to completely cover the matrix 14.

[0007] In accordance with the present invention, the metallic matrix is applied to the substrate 12 in a flame spraying process. The material of the metal matrix 14 may vary widely within the scope of the invention, and can be of any metal which is of powder form. Metals from the group consisting of stainless steel, nickel, nickel chromium, molybdenum or the carbides are some of the materials used. The metal matrix 14 is deposited onto the substrate 10 to a depth of from 0.002 to 0.010 of an inch, depending upon the purpose for which the coated substrate is employed.

[0008] Further, and in accordance with the present invention, the silicon may be applied to the metal matrix 14 such that the silicon fills the depressions 16, extends above the plateaus 18 and penetrates into the matrix 14. It is permitted to polymerize in situ at ambient temperatures for a period of from 16 to 24 hours. As noted above, this is the major advantage of the present invention over prior art composite release coatings; the coating can be applied and cured on site, eliminating the need for heat-curing in an oven.

[0009] The composite coating which results has a hardness of up to 72 Rc and a surface finish of from 250 to 700 microinches. The composite exhibits thermal stability at continuous operating temperatures of up to 400 degrees fahrenheit and intermittent operating temperatures of up to 500 degrees fahrenheit. The composite coating also provides 2 1/2 - 3 times longes release life than composite coatings utilizing fluorocarbon release agents. In the case of certain adhesives, absolute release is offered with no adhesive transfer onto the release surface, whereas resistance as well as adhesive transfer is apparent when used with the above mentioned fluorocarbon release coatings. It also has a high coefficient of friction which is desireable for web tracking.

Claims

1. An air cured, composite coating for imparting an abrasion resistant release surface to a substrate, said air cured composite coating comprising:
      a porous metal matrix thermally sprayed onto said substrate to a depth of 0.002 to 0.010 of an inch, said matrix comprising a metal of powdered form and
      a film of silicon impregnated into said metal matrix to seal the porosity of said matrix.

2. The air cured, composite coating of Claim 1 wherein the metal of powdered form is selected from the group consisting of stainless steel, nickel, nickel chromium, molybdenum or a carbide.

3. The air cured composite coating of claim 1 wherein said coating maintains thermal stability at a continuous operating temperature of up to 400 degrees fahrenheit and an intermittent operating temperature of up to 500 degrees fahrenheit.

4. The air cured composite coating of claim 1 wherein said coating has a hardness of up to 72 Rc.

5. The air cured composite coating of claim 1 wherein said coating has a surface finish in the range of 250 to 700 micro-inches.

6. The air cured composite coating of claim 1 wherein said coating is completely air cured within 16 - ­24 hours.

7. A method of applying an air cured composite coating to a substrate comprising the steps of:
      providing a substrate;
      applying a porous metal matrix to said substrate to a depth of 0.002 to 0.0010 of an inch in a flame spraying process, said metal matrix comprising a metal of powdered form;
      impregnating a silicon into said metal matrix to seal the porosity of said matrix; and
      air curing said composite coating on said substrate for a period of 16 - 24 hours.

8. A method of applying an air cured composite coating to a substrate as set forth in claim 6 wherein said process is of the metal spraying type.

9. A method of applying an air cured composite coating to a substrate substantially as described herein with reference to the accompanying drawings.

10. An air cured composite coating made by a method according to any one of claims 7,8, or 9.

Drawing