ZA813064B - Surface hardening of hardmetal articles - Google Patents
Surface hardening of hardmetal articlesInfo
- Publication number
- ZA813064B ZA813064B ZA00813064A ZA813064A ZA813064B ZA 813064 B ZA813064 B ZA 813064B ZA 00813064 A ZA00813064 A ZA 00813064A ZA 813064 A ZA813064 A ZA 813064A ZA 813064 B ZA813064 B ZA 813064B
- Authority
- ZA
- South Africa
- Prior art keywords
- hardmetal
- articles
- surface hardening
- hardening
- hardmetal articles
- Prior art date
Links
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ZA00813064A ZA813064B (en) | 1980-04-18 | 1981-05-08 | Surface hardening of hardmetal articles |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ZA802316 | 1980-04-18 | ||
ZA00813064A ZA813064B (en) | 1980-04-18 | 1981-05-08 | Surface hardening of hardmetal articles |
Publications (1)
Publication Number | Publication Date |
---|---|
ZA813064B true ZA813064B (en) | 1982-05-26 |
Family
ID=27132144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ZA00813064A ZA813064B (en) | 1980-04-18 | 1981-05-08 | Surface hardening of hardmetal articles |
Country Status (1)
Country | Link |
---|---|
ZA (1) | ZA813064B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6415486B1 (en) * | 2000-03-01 | 2002-07-09 | Surface Technology Holdings, Ltd. | Method and apparatus for providing a residual stress distribution in the surface of a part |
US6926970B2 (en) | 2001-11-02 | 2005-08-09 | The Boeing Company | Apparatus and method for forming weld joints having compressive residual stress patterns |
-
1981
- 1981-05-08 ZA ZA00813064A patent/ZA813064B/en unknown
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6415486B1 (en) * | 2000-03-01 | 2002-07-09 | Surface Technology Holdings, Ltd. | Method and apparatus for providing a residual stress distribution in the surface of a part |
US6926970B2 (en) | 2001-11-02 | 2005-08-09 | The Boeing Company | Apparatus and method for forming weld joints having compressive residual stress patterns |
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