Coating method, surface layer structure, as well as applications

US9887349B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9887349-B2
Application numberUS-201314388708-A
CountryUS
Kind codeB2
Filing dateMar 12, 2013
Priority dateMar 28, 2012
Publication dateFeb 6, 2018
Grant dateFeb 6, 2018

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  1. Title

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  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

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A coating method for producing a function layer on mechanically loaded components or surfaces includes providing or applying a first material layer of a first material or substrate matrix having a mechanical flexibility higher than that of a second material on a substrate constituting the component or the surface, respectively, structuring the first material layer such that the material layer surface of the first material layer, which is opposite to the substrate, obtains a three-dimensionally molded basic structure with projections and recesses, and coating the material layer surface of the first material layer with a second material layer of the second material in such a way that the second material layer adopts substantially the basic structure of the material layer surface with the projections and recesses. Also, surface layer structures can be produced by this method.

First claim

Opening claim text (preview).

The invention claimed is: 1. A coating method for producing a function layer on a substrate formed of a substrate material including one of a metal sheet and a fiber composite component, the substrate deforming in response to a force in a longitudinal direction of the substrate, and warping or twisting about the longitudinal direction in response to a torque impose on the substrate, the method comprising: providing a first material layer made of a first material with a mechanical flexibility higher than that of a second material at or on the substrate, such that the first material exhibits a resilient load in response to the deforming, warping and twisting of the substrate; structuring the first material layer so that the material layer surface of the first material layer is given a three-dimensionally moulded basic structure with projections and recesses; and coating the material layer surface of the first material layer with a second material layer made of the second material, such that the second material layer adopts substantially the basic structure of the material layer surface with the projections and recesses. 2. The coating method according to claim 1 , wherein at least one of the following the substrate is formed of a substrate material selected from a group of materials including metal, ceramic, plastic and fibre fabric; the first material is selected from a group of materials including metal, plastic and ceramic; and the second material is selected from a group of materials including metal, plastic and ceramic. 3. The coating method according to claim 2 , wherein the providing includes selecting the first material and the second material such that the second material has at least one of the following a higher modulus of elasticity than the first material, a higher hardness than the first material, a lower breaking elongation, reduction of area at break, and fracture toughness than the first material, and a lower dynamic strength than the first material. 4. The coating according to claim 2 , further comprising providing or forming the first material layer both as first function layer for providing at least a first function or as a mold for formation of the second material layer; and forming the second material layer as second function layer for providing at least one second function. 5. The coating method according to claim 2 , wherein the structuring of the first material layer includes at least one of the following: microscopic structuring of the first material layer by an energetic beam, a laser beam, an ion beam or an electron beam; thermal microscopic structuring by a heated counter-mould; and microscopic embossing the basic structure on the material layer surface. 6. The coating method according to claim 2 , wherein the structuring of the first material layer includes at least one of the following: selecting the basic structure or the shape and the size dimensions of the basic structure in consideration of at least one of the following criteria: level of a load to be expected, type of a load to be expected, desired or predetermined deformation path, and influence from the environment on the component or the surface; and forming the basic structure with a period succession of recesses and projections. 7. The coating method according to claim 1 , wherein the providing includes selecting the first material and the second material such that the second material has at least one of the following a higher modulus of elasticity than the first material, a higher hardness than the first material, a lower breaking elongation, reduction of area at break, and fracture toughness than the first material, and a lower dynamic strength than the first material. 8. The coating according to claim 7 , further comprising providing or forming the first material layer both as first function layer for providing at least a first function or as a mold for formation of the second material layer; and forming the second material layer as second function layer for providing at least one second function. 9. The coating method according to claim 7 , wherein the structuring of the first material layer includes at least one of the following: microscopic structuring of the first material layer by an energetic beam, a laser beam, an ion beam or an electron beam; thermal microscopic structuring by a heated counter-mould; and microscopic embossing the basic structure on the material layer surface. 10. The coating method according to claim 7 , wherein the structuring of the first material layer includes at least one of the following: selecting the basic structure or the shape and the size dimensions of the basic structure in consideration of at least one of the following criteria: level of a load to be expected, type of a load to be expected, desired or predetermined deformation path, and influence from the environment on the component or the surface; and forming the basic structure with a period succession of recesses and projections. 11. The coating according to claim 1 , further comprising providing or forming the first material layer both as first function layer for providing at least a first function or as a mold for formation of the second material layer; and forming the second material layer as second function layer for providing at least one second function. 12. The coating method according to claim 1 , further comprising at least one of the following providing or forming the first material layer as at least one of the following an insulating layer for electric insulation, a protective layer for protection from moisture, and a resilient buffer layer for resilient balancing of relative displacements or relative movements between the second material layer and the substrate; and forming the second material layer as at least one of the following a protective layer for protection from chemical loads, a protective layer for protection from mechanical or physical loads, a protective layer for protection from thermal loads, an electrically conductive or electrically insulating function layer, and a field-influencing layer for influencing electromagnetic, electric or magnetic fields. 13. The coating method according to claim 1 , wherein the structuring of the first material layer includes at least one of the following: microscopic structuring of the first material layer by an energetic beam, a laser beam, an ion beam or an electron beam; thermal microscopic structuring by a heated counter-mould; and microscopic embossing the basic structure on the material layer surface. 14. The coating method according to claim 1 , wherein the structuring of the first material layer includes at least one of the following: selecting the basic structure or the shape and the size dimensions of the basic structure in consideration of at least one of the following criteria: level of a load to be expected, type of a load to be expected, desired or predetermined deformation path, and influence from the environment on the component or the surface; and forming the basic structure with a period succession of recesses and projections. 15. The coating method according to claim 1 , wherein the first material has a thickness in a range of 1 μm to 50 μm; and the second material has a thickness in a range of 1 μm to 10 μm.

Assignees

Inventors

Classifications

  • Impact or kinetic deposition of particles · CPC title

  • Deposition of sublayers, e.g. to promote adhesion of the coating (C23C14/027 takes precedence) · CPC title

  • having variation in thickness · CPC title

  • Metallic material, boron or silicon · CPC title

  • Physical treatment to alter the texture of the substrate surface, e.g. grinding, polishing · CPC title

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What does patent US9887349B2 cover?
A coating method for producing a function layer on mechanically loaded components or surfaces includes providing or applying a first material layer of a first material or substrate matrix having a mechanical flexibility higher than that of a second material on a substrate constituting the component or the surface, respectively, structuring the first material layer such that the material layer s…
Who is the assignee on this patent?
Airbus Defence & Space Gmbh
What technology area does this patent fall under?
Primary CPC classification B32B15/01. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Feb 06 2018 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).