GB738757A - Improvements in or relating to methods of casting metals - Google Patents
Improvements in or relating to methods of casting metalsInfo
- Publication number
- GB738757A GB738757A GB2095252A GB2095252A GB738757A GB 738757 A GB738757 A GB 738757A GB 2095252 A GB2095252 A GB 2095252A GB 2095252 A GB2095252 A GB 2095252A GB 738757 A GB738757 A GB 738757A
- Authority
- GB
- United Kingdom
- Prior art keywords
- mould
- inert gas
- casting
- space
- pores
- 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
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
738,757. Casting processes. BRISTOL AEROPLANE CO., Ltd. July 21, 1953 [Aug. 20, 1952], No. 20952/52. Class 83 (1). In a method of casting metals in a porous mould, such as a sand or wax - investment mould, an inert gas is caused to pass through the pores of the mould and into the mould space to expel air entrapped in the pores and also in the mould space, and the casting metal is poured into the mould while it is impregnated and filled with the inert gas. An investment mould 10, Fig. 1, for turbine blades, is covered by a member 16 clamped against an asbestos mat 21 supported over a furnace, the mould space communicating with the atmosphere through the pouring gate 13, 14. Inert gas, e.g. argon, is supplied under pressure through a pipe 19 and after a period of time sufficient to ensure the expulsion of the air from the pores of the mould and the mould space, the metal is poured by inverting the mould and furnace assembly, the flow of inert gas being maintained meanwhile and after casting while the metal is allowed to cool sufficiently to solidify. After solidification the mould on a base 23, Fig. 2, is covered by a vessel 26 with a valve 30, and propane under pressure supplied to the chamber 27. The gas jet is lit before the vessel 26 is placed in position, to prevent an explosion. Ducts 31, which may be formed by passing a wire through the mould, ensure that argon penetrates to the mould space remote from the pouring gate. Nitrogen may be used instead of argon.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2095252A GB738757A (en) | 1952-08-20 | 1952-08-20 | Improvements in or relating to methods of casting metals |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2095252A GB738757A (en) | 1952-08-20 | 1952-08-20 | Improvements in or relating to methods of casting metals |
Publications (1)
Publication Number | Publication Date |
---|---|
GB738757A true GB738757A (en) | 1955-10-19 |
Family
ID=10154606
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2095252A Expired GB738757A (en) | 1952-08-20 | 1952-08-20 | Improvements in or relating to methods of casting metals |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB738757A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174200A (en) * | 1961-06-15 | 1965-03-23 | Union Carbide Corp | Method of purging mold and pouring metal therein |
US3420291A (en) * | 1965-12-29 | 1969-01-07 | Trw Inc | Method for reducing metal casting porosity |
US4021910A (en) * | 1974-07-03 | 1977-05-10 | Howmet Turbine Components Corporation | Method for treating superalloy castings |
CN105170948A (en) * | 2015-10-09 | 2015-12-23 | 西安航空动力股份有限公司 | Method for protecting ZG1Cr112Ni3Mo2Co2VN stainless steel casting against oxide spots |
WO2019222138A1 (en) * | 2018-05-14 | 2019-11-21 | Magna International Inc. | Direct chill permanent mold casting system and method of same |
CN117102436A (en) * | 2023-10-20 | 2023-11-24 | 江苏二马液压元件有限公司 | Die for producing hydraulic valve body and processing method thereof |
-
1952
- 1952-08-20 GB GB2095252A patent/GB738757A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174200A (en) * | 1961-06-15 | 1965-03-23 | Union Carbide Corp | Method of purging mold and pouring metal therein |
US3420291A (en) * | 1965-12-29 | 1969-01-07 | Trw Inc | Method for reducing metal casting porosity |
US4021910A (en) * | 1974-07-03 | 1977-05-10 | Howmet Turbine Components Corporation | Method for treating superalloy castings |
CN105170948A (en) * | 2015-10-09 | 2015-12-23 | 西安航空动力股份有限公司 | Method for protecting ZG1Cr112Ni3Mo2Co2VN stainless steel casting against oxide spots |
WO2019222138A1 (en) * | 2018-05-14 | 2019-11-21 | Magna International Inc. | Direct chill permanent mold casting system and method of same |
CN117102436A (en) * | 2023-10-20 | 2023-11-24 | 江苏二马液压元件有限公司 | Die for producing hydraulic valve body and processing method thereof |
CN117102436B (en) * | 2023-10-20 | 2023-12-19 | 江苏二马液压元件有限公司 | Die for producing hydraulic valve body and processing method thereof |
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