GB738757A - Improvements in or relating to methods of casting metals - Google Patents

Improvements in or relating to methods of casting metals

Info

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
Application number
GB2095252A
Inventor
Joseph Hinde
Arthur Taylor
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB2095252A priority Critical patent/GB738757A/en
Publication of GB738757A publication Critical patent/GB738757A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use 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.
GB2095252A 1952-08-20 1952-08-20 Improvements in or relating to methods of casting metals Expired GB738757A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (7)

* Cited by examiner, † Cited by third party
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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