GB824768A - Method of producing a direct and firm bond between structural components of ferrous metal and aluminium or aluminium base alloys by casting molten aluminium or aluminiumbase alloys around or on to the surface of the ferrous metal components - Google Patents
Method of producing a direct and firm bond between structural components of ferrous metal and aluminium or aluminium base alloys by casting molten aluminium or aluminiumbase alloys around or on to the surface of the ferrous metal componentsInfo
- Publication number
- GB824768A GB824768A GB1651355A GB1651355A GB824768A GB 824768 A GB824768 A GB 824768A GB 1651355 A GB1651355 A GB 1651355A GB 1651355 A GB1651355 A GB 1651355A GB 824768 A GB824768 A GB 824768A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aluminium
- ferrous metal
- alloys
- components
- aluminiumbase
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Coating With Molten Metal (AREA)
Abstract
Ferrous metal structural components are tinned by immersion in a tin salt melt before aluminium or aluminium-base alloys are cast around or on to the surface thereof. An electrodeposit of iron is preferably applied to components made of cast iron having pronounced coarse veins of graphite or steels alloyed with nickel before tinning them. The example relates to the tinning of a stainless steel peg in a melt consisting of 50-62% SNCl2 and 50-38% KCl before being cast around with aluminium-silicon alloy. According to the Provisional Specification, the tin coating may be applied galvanically or by immersion and may be thermally after-treated.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1651355A GB824768A (en) | 1955-06-08 | 1955-06-08 | Method of producing a direct and firm bond between structural components of ferrous metal and aluminium or aluminium base alloys by casting molten aluminium or aluminiumbase alloys around or on to the surface of the ferrous metal components |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1651355A GB824768A (en) | 1955-06-08 | 1955-06-08 | Method of producing a direct and firm bond between structural components of ferrous metal and aluminium or aluminium base alloys by casting molten aluminium or aluminiumbase alloys around or on to the surface of the ferrous metal components |
Publications (1)
Publication Number | Publication Date |
---|---|
GB824768A true GB824768A (en) | 1959-12-02 |
Family
ID=10078687
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1651355A Expired GB824768A (en) | 1955-06-08 | 1955-06-08 | Method of producing a direct and firm bond between structural components of ferrous metal and aluminium or aluminium base alloys by casting molten aluminium or aluminiumbase alloys around or on to the surface of the ferrous metal components |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB824768A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110640114A (en) * | 2019-10-31 | 2020-01-03 | 陕西航空电气有限责任公司 | Method for overcoming defect of casting looseness of motor shell |
-
1955
- 1955-06-08 GB GB1651355A patent/GB824768A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110640114A (en) * | 2019-10-31 | 2020-01-03 | 陕西航空电气有限责任公司 | Method for overcoming defect of casting looseness of motor shell |
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