Claims
- 1. A method of providing an inner surface of a weapon barrel with a chromium layer; said weapon barrel having a base material; the method comprising the following steps:(a) forming the chromium layer on said inner surface by galvanic separation; (b) after step (a), heating the chromium layer to a temperature for obtaining, upon conclusion of step (b), a uniform re-crystallization of said chromium layer in its entirety; and (c) controlling a duration of said heating step such that said base material is heated to 300° C. at the most.
- 2. A method of providing an inner surface of a weapon barrel with a chromium layer, comprising the following steps:(a) forming the chromium layer on said inner surface by galvanic separation; and (b) after step (a), heating the chromium layer with a laser beam to a temperature for obtaining, upon conclusion of step (b), a uniform re-crystallization of said chromium layer in its entirety.
- 3. The method as defined in claim 2, wherein said heating step comprises the steps of(a) positioning a mirror in said weapon barrel; (b) directing the laser beam axially into said weapon barrel for causing said laser beam to be reflected from said mirror onto said hard chromium layer; and (c) effecting a simultaneous relative rotation and axial displacement between said mirror and said weapon barrel.
- 4. The method as defined in claim 3, wherein said weapon barrel has a rifling and further wherein step (c) is controlled such that a path of impingement of the laser beam on said chromium layer is parallel to said rifling.
- 5. A method of providing an inner surface of a weapon barrel with a chromium layer, comprising the following steps:(a) forming the chromium layer on said inner surface by galvanic separation; and (b) after step (a), heating the chromium layer to a temperature for obtaining, upon conclusion of step (b), a uniform re-crystallization of said chromium layer in its entirety; said heating step comprising the step of heating the chromium layer in an oven to a re-crystallization temperature; said re-crystallization temperature being below an annealing temperature of the barrel material.
Priority Claims (1)
Number |
Date |
Country |
Kind |
198 53 293 |
Nov 1998 |
DE |
|
CROSS REFERENCE TO RELATED APPLICATION
This application claims the priority of German Application No. 198 53 293.8 filed Nov. 19, 1998, which is incorporated herein by reference.
US Referenced Citations (6)
Foreign Referenced Citations (5)
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41 07 273 |
Sep 1992 |
DE |
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Feb 1997 |
DE |
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DE |
2 460 340 |
Jan 1981 |
FR |
810494 |
Mar 1959 |
GB |