GB553265A - Improvements relating to the manufacture of sheet metal articles - Google Patents
Improvements relating to the manufacture of sheet metal articlesInfo
- Publication number
- GB553265A GB553265A GB3107739A GB3107739A GB553265A GB 553265 A GB553265 A GB 553265A GB 3107739 A GB3107739 A GB 3107739A GB 3107739 A GB3107739 A GB 3107739A GB 553265 A GB553265 A GB 553265A
- Authority
- GB
- United Kingdom
- Prior art keywords
- dies
- zinc
- copper
- heating
- manufacture
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D37/00—Tools as parts of machines covered by this subclass
- B21D37/16—Heating or cooling
Abstract
553,265. Annealing; zinc alloy. BOULTON PAUL AIRCRAFT, Ltd., and NORTH, J. D. Nov. 29, 1939, Nos. 31077/39 and 1197/40. [Classes 72 and 82 (i)] [Also in Group XXII] Sheet steel articles such as corrugated parts of aircraft, are simultaneously formed and hardened, by heating the parts to a temperature above the upper critical limit and pressing them between cold, massive, highly heat-conducting dies. The dies may be of zinc or zinc lead alloy coated as by electrodeposition with a thin layer of metal such as copper. The dies may be made from an alloy containing 94 per cent. zinc and 6 copper or steel dies may be employed. The shaping may be effected in two or more stages with intermediate re-heating and the work is lubricated as by oil containing graphite or ground micaceous iron.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3107739A GB553265A (en) | 1939-11-29 | 1939-11-29 | Improvements relating to the manufacture of sheet metal articles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3107739A GB553265A (en) | 1939-11-29 | 1939-11-29 | Improvements relating to the manufacture of sheet metal articles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB553265A true GB553265A (en) | 1943-05-14 |
Family
ID=10317606
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3107739A Expired GB553265A (en) | 1939-11-29 | 1939-11-29 | Improvements relating to the manufacture of sheet metal articles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB553265A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2478171A (en) * | 1945-08-20 | 1949-08-09 | Ductile Chrome Process Co | Method of making metal drawing dies |
US2726972A (en) * | 1953-06-01 | 1955-12-13 | North American Aviation Inc | Method and apparatus for forming metal workpieces |
US2762734A (en) * | 1952-09-29 | 1956-09-11 | North American Aviation Inc | Process and apparatus for forming and stress relieving metal |
-
1939
- 1939-11-29 GB GB3107739A patent/GB553265A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2478171A (en) * | 1945-08-20 | 1949-08-09 | Ductile Chrome Process Co | Method of making metal drawing dies |
US2762734A (en) * | 1952-09-29 | 1956-09-11 | North American Aviation Inc | Process and apparatus for forming and stress relieving metal |
US2726972A (en) * | 1953-06-01 | 1955-12-13 | North American Aviation Inc | Method and apparatus for forming metal workpieces |
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