Method to produce high corrosion and wear resistant cast iron components by water jet surface activation, nitrocarburization and thermal spray coating
US-2024084430-A1 · Mar 14, 2024 · US
US10570495B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10570495-B2 |
| Application number | US-201515563716-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 8, 2015 |
| Priority date | Apr 8, 2015 |
| Publication date | Feb 25, 2020 |
| Grant date | Feb 25, 2020 |
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A number of variations may include a method that may include laser shock peening a friction work surface of a working part and applying a ferritic nitrocarburizing process to the friction work surface such that diffusion of carbon and nitrogen atoms into the friction work surface is accelerated.
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What is claimed is: 1. A method comprising: laser shock peening a friction work surface of a working part; and applying a ferritic nitrocarburizing process to the friction work surface of the working part in order to facilitate diffusion of carbon and nitrogen atoms into the friction work surface of the working part. 2. The method according to claim 1 wherein the laser shock peening process refines the microstructure of the friction work surface of the working part such that a nanocrystalline layer of about 5 to about 500 μm in depth is formed. 3. The method according to claim 1 wherein the laser shock peening process refines the microstructure of the friction work surface of the working part such that an amorphous layer of less than or equal to about 500 μm in depth is formed. 4. The method according to claim 1 wherein the laser shock peening process utilizes a high power density laser having a power ranging from about 0.5 GW/cm 2 to about 5 GW/cm 2 . 5. The method according to claim 1 wherein the ferritic nitrocarburizing process comprises a furnace treatment for about 2-6 hours at about 555° C. to about 585° C. 6. The method according to claim 1 wherein the ferritic nitrocarburizing process comprises a furnace treatment for about 2-4 hours at about 570° C.-580° C. 7. The method according to claim 1 wherein the laser shock peening process includes a pulse energy of about 3 Joules, pulse duration of about 20 nanoseconds, and a laser beam diameter of about 3 mm. 8. The method according to claim 1 , further comprising, prior to laser shock peening the friction work surface, applying a stress relief treatment to the working part at about 610° C. for about 2-4 hours. 9. The method according to claim 1 , further comprising, prior to laser shock peening the friction work surface of the working part, machining the friction work surface. 10. The method according to claim 1 wherein the laser shock peening process refines the microstructure of the friction work surface of the working part such that an amorphous layer is formed. 11. The method according to claim 1 , further comprising, prior to laser shock peening the friction work surface of the working part, applying a stress relief treatment to the working part at about 610° C. for greater than or equal to about 3 hours. 12. A method comprising: machining a friction work surface of a working part; laser shock peening the friction work surface of the working part; and applying a ferritic nitrocarburizing process to the friction work surface of the working part in order to facilitate diffusion of carbon and nitrogen atoms into the friction work surface of the working part. 13. The method according to claim 12 , wherein the ferritic nitrocarburizing process comprises a furnace treatment for about 8 to about 12 hours at about 455° C. to about 495° C. 14. A method comprising: applying a stress relief treatment to a working part at about 610° C. for 3 hours; machining a friction work surface of the working part; laser shock peening the friction work surface of the working part utilizing a high power density laser having a power of about 1 GW/cm 2 including a pulse energy of about 3 Joules pulse duration of about 20 nanoseconds, and a laser beam diameter of about 3 mm; and applying a ferritic nitrocarburizing process to the friction work surface of the working part in order to facilitate such that diffusion of carbon and nitrogen atoms into the friction work surface of the working part. 15. The method according to claim 14 wherein the ferritic nitrocarburizing process comprises a furnace treatment ranging from about 1 to about 3 hours at about 555° C. to about 585° C. 16. The method according to claim 14 wherein the ferritic nitrocarburizing process comprises a furnace treatment ranging from about 8 to about 12 hours at about 465° C. to about 495° C. 17. A method comprising: machining a friction work surface of a working part; laser shock peening the friction work surface of the working part utilizing a high power density laser having a power greater than or equal to 1 GW/cm 2 including a pulse energy of about 3 Joules, pulse duration of about 20 nanoseconds, and a laser beam diameter of about 3 mm; and applying a ferritic nitrocarburizing process for about 8 to about 12 hours at about 465° C. to about 495° C. to the friction work surface of the working part in order to facilitate such that diffusion of carbon and nitrogen atoms into the friction work surface of the working part. 18. A product comprising: a part comprising a friction working surface that has been cast, undergone a stress relief process at about 610° C. for about 3 hours, machined, and laser shock peened and an amorphous layer disposed on the friction working surface wherein the amorphous layer ranges from about 5 microns to about 500 microns in depth. 19. The product according to claim 18 , wherein the part is a cast iron brake rotor. 20. A product comprising: a part comprising a friction working surface that has been cast, machined, laser shock peened, and treated with a ferritic nitrocarburizing process at about 450° C. for about 2 to about 4 hours and an amorphous layer disposed on the friction working surface wherein the amorphous layer ranges from about 5 microns to about 500 microns in depth. 21. The product according to claim 20 , wherein the part is a cast iron brake rotor.
Pretreatment of the material to be coated (C23C8/04 takes precedence) · CPC title
of ferrous surfaces · CPC title
by laser shock processing · CPC title
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