Polymeric Cutting Edge Structures And Method Of Manufacturing Polymeric Cutting Edge Structures
US-2017368703-A1 · Dec 28, 2017 · US
US9969094B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9969094-B2 |
| Application number | US-201514872466-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 1, 2015 |
| Priority date | Oct 6, 2014 |
| Publication date | May 15, 2018 |
| Grant date | May 15, 2018 |
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A method for shaping a coating on a razor blade is provided. The method includes the steps of: a) providing a razor blade having a tip end defined by at least one tip surface; b) applying a surface coating having a first thickness on at least one tip surface; and c) shaping the applied surface coating on the at least one tip surface to have a second thickness using a centrifuge, which second thickness is less than the first thickness.
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What is claimed is: 1. A method for shaping a coating on a razor blade, comprising the steps of: providing a razor blade having a tip end defined by at least one tip surface; applying a surface coating having a first thickness on at least one tip surface; and shaping the applied surface coating on the at least one tip surface to have a second thickness using a centrifuge, which second thickness is less than the first thickness; and sintering the applied surface coating, including heating the applied surface coating to a temperature at which the applied surface coating is in a plastic state; wherein the step of shaping the applied surface coating includes centrifuging the razor blade with the applied surface coating in a manner that causes a portion of the applied surface coating to move away from the tip end of the razor blade and thereby leaving a residual surface coating layer having the second thickness; and wherein the step of shaping the applied surface coating further includes shaping the applied surface coatings in an inert environment comprising a non-reactive gas. 2. The method of claim 1 , wherein the step of sintering the applied surface coating includes sintering the applied surface coating in an environment of gas that is non-reactive with one or both of a surface coating material or a razor blade material. 3. The method of claim 2 , wherein the gas comprises at least one of Nitrogen and Argon. 4. The method of claim 1 , wherein the gas comprises at least one of Nitrogen and Argon. 5. The method of claim 1 , wherein the residual surface coating layer extends over substantially all the tip surface. 6. The method of claim 1 wherein the centrifuge has a central rotational axis, and the razor blade is rotated around the central rotational axis, and the blade is oriented in the centrifuge with its tip end in a direction toward the central rotational axis. 7. The method of claim 1 wherein the centrifuge has a central rotational axis, and the razor blade is rotated around the central rotational axis, and the blade is oriented in the centrifuge with its tip end in a direction away from the central rotational axis. 8. The method of claim 1 , wherein the surface coating comprises a fluoropolymer. 9. The method of claim 8 , wherein the surface coating comprises polytetrafluoroethylene. 10. A method for shaping a coating on a razor blade, comprising the steps of: providing a plurality of razor blades, each razor blade having a tip end defined by at least one tip surface, and an applied surface coating having a first thickness applied on the at least one tip surface; loading the razor blades in a centrifuge with the tip ends of the razor blades disposed within the centrifuge in a common orientation; and centrifuging the blades to shape the applied surface coating on the at least one tip surface of each razor blade to have a second thickness, which second thickness is less than the first thickness; wherein the step of centrifuging the blades includes centrifuging the blades in an environment of a non-reactive gas. 11. The method of claim 10 , further comprising the step of sintering the applied surface coating on each of the razor blades, including heating the applied surface coating on each razor blade to a temperature at which the applied surface coating is in a plastic state. 12. The method of claim 11 , wherein the step of sintering the applied surface coating includes sintering the applied surface coating in an environment of gas that is non-reactive with one or both of a surface coating material or a razor blade material. 13. The method of claim 12 , wherein the gas comprises at least one of Nitrogen and Argon. 14. The method of claim 10 , wherein the step of centrifuging the blades includes centrifuging the razor blades in a manner that causes a portion of the applied surface coating on each razor blade to move away from the tip end of that razor blade and leave a residual surface coating layer having the second thickness on that blade. 15. The method of claim 10 , wherein the residual surface coating layer extends over substantially all the tip surface. 16. The method of claim 10 , wherein the gas comprises at least one of Nitrogen and Argon. 17. The method of claim 10 wherein the centrifuge has a central rotational axis, and the razor blades are rotated around the central rotational axis, and each razor blade is oriented in the centrifuge with its tip end in a direction toward the central rotational axis. 18. The method of claim 10 wherein the centrifuge has a central rotational axis, and the razor blades are rotated around the central rotational axis, and each razor blade is oriented in the centrifuge with its tip end in a direction away from the central rotational axis. 19. The method of claim 10 , wherein the surface coating comprises a fluoropolymer. 20. The method of claim 19 , wherein the surface coating comprises polytetrafluoroethylene.
the substrate being rotated · CPC title
involving the use of fluoropolymers · CPC title
Spin coating · CPC title
by the coating material · CPC title
After-treatment · CPC title
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