USRE32622E - Method for the manufacture of molds using casting sand or another mixture of raw material particles - Google Patents

Method for the manufacture of molds using casting sand or another mixture of raw material particles Download PDF

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Publication number
USRE32622E
USRE32622E US06/880,721 US88072186A USRE32622E US RE32622 E USRE32622 E US RE32622E US 88072186 A US88072186 A US 88072186A US RE32622 E USRE32622 E US RE32622E
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pressure
process according
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atmospheres
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US06/880,721
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Christoph Landolt
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George Fischer Foundry Systems Inc
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George Fischer Foundry Systems Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C15/00Moulding machines characterised by the compacting mechanism; Accessories therefor

Definitions

  • the present invention relates to a method of manufacturing molds from casting sand or from an otherwise moldable mixture by the use of a pressure surge wave in a closed chamber.
  • the other moldable mixture comprises particles of raw material, binder, water, and, if need be, additives.
  • a number of processes are known whereby the manufacturing of molds is effected by means of a pressure surge wave.
  • a gas pressure is built up over a moldable mixture such as, for example, a casting sand, and then subsequently decreased.
  • the object of the invention is to select a range in pressure variation within which an optimal compaction of the moldable mixture is assured.
  • castings are made from casting sand or other moldable mixture by means of a pressure surge wave.
  • the pressure surge wave is characterized by four parameters: these are the increasing pressure gradient, the maximum pressure, the duration of the maximum pressure, and the decreasing pressure gradient.
  • the rise in pressure takes place with an increasing pressure gradient, dp/dt, of at least about 50 atmospheres (absolute)/second.
  • a .[.maximum.]. pressure of at least about 2 atmospheres (absolute) is maintained for at least 0.01 seconds.
  • the pressure drop takes place with a decreasing pressure gradient, -dp/dt, of up to 2.0 atmospheres (absolute)/sec.
  • the FIGURE shows four pressure surge waves as a function of time, in accordance with an illustrative embodiment of the invention.
  • the pressure range is characterized bythe fact that the moldable mixture is exposed to a gas pressure of at least 2 atmospheres (absolute) using an increasing pressure gradient, dp/dt, of at least 50 atmospheres (absolute)/second, maintaining at least this pressure for at least 0.01 seconds and then allowing the pressure to drop back to normal pressure within at least 0.2 seconds from the onset of the pressure increase.
  • the pressure surge wave should be applied to the surface of the sand as a mass flow through change of the amount of air per unit time.
  • the pressure surge may be produced by compressing a gas or by an exothermic reaction of an explosive gas mixture.
  • the pressure surge wave should be reduced to a low final pressure, that is, finally reduced to normal pressure.
  • a pressure maximum of 4 to 5.5 atmospheres (absolute) in a combustion chamber represents an optimization between the desired strength properties of the sand molds and the cost of sealing the combustion chamber. .[.The maximum.]. .Iadd.An elevated .Iaddend.pressure .Iadd.of at least 2 atmospheres (absolute) .Iaddend.should be maintained for at least 0.01 second and may be .[.mainted.]. .Iadd.maintained .Iaddend.for about 0.03-0.05 seconds.
  • the FIGURE shows four pressure surges, all of which are characterized by increasing pressure gradients, maximum pressures, duration of maximum pressure, and decreasing pressure gradients in the aforementioned ranges in accordance with the present invention.
  • Each of the surges starts at normal, i.e. atmospheric pressure and ends at normal, i.e. atmospheric pressure.
  • Compactibility relates to the decrease in volume of the casting mixture after the pressure surge is applied thereto.
  • the process described finds an application in the precise molding of a casting mold by using a pattern wherein the derived optimum values are so adjusted and combined that a pressure of 80 to 180 Newtons/centimeter 2 is produced on the surface of the pattern.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Casting Devices For Molds (AREA)
  • Mold Materials And Core Materials (AREA)

Abstract

In order to make casting sand or another moldable mixture, a pressure surge wave is used which has upper and lower limit values which values have been established by an optimal selection of a pattern of pressures. The other moldable mixture comprises particles of raw material, binder, water, and, if need be, additives. The rise in pressure takes place with an increasing pressure gradient, dp/dt, of at least 50 atmospheres (absolute)/second. A minimum pressure of at least 2 atmospheres (absolute) is maintained for at least 0.01 second. The pressure drop takes place at a decreasing pressure gradient,--dp/dt, of up to about 2.0 atmospheres (absolute)/second. The disclosed values represent an optimalization, in view of a simple design and economy of operation, with a surprisingly good compacting.

Description

FIELD OF THE INVENTION
The present invention relates to a method of manufacturing molds from casting sand or from an otherwise moldable mixture by the use of a pressure surge wave in a closed chamber. The other moldable mixture comprises particles of raw material, binder, water, and, if need be, additives.
BACKGROUND OF THE INVENTION
A number of processes are known whereby the manufacturing of molds is effected by means of a pressure surge wave. In such processes, a gas pressure is built up over a moldable mixture such as, for example, a casting sand, and then subsequently decreased.
The object of the invention is to select a range in pressure variation within which an optimal compaction of the moldable mixture is assured.
SUMMARY OF THE INVENTION
In accordance with the present invention, castings are made from casting sand or other moldable mixture by means of a pressure surge wave. The pressure surge wave is characterized by four parameters: these are the increasing pressure gradient, the maximum pressure, the duration of the maximum pressure, and the decreasing pressure gradient. The rise in pressure takes place with an increasing pressure gradient, dp/dt, of at least about 50 atmospheres (absolute)/second. A .[.maximum.]. pressure of at least about 2 atmospheres (absolute) is maintained for at least 0.01 seconds. The pressure drop takes place with a decreasing pressure gradient, -dp/dt, of up to 2.0 atmospheres (absolute)/sec. These values yield surprisingly good compacting of the casting sand and or other moldable mixture from which the castings are made.
BRIEF DESCRIPTION OF THE DRAWINGS
The FIGURE shows four pressure surge waves as a function of time, in accordance with an illustrative embodiment of the invention.
DETAILED DESCRIPTION OF THE INVENTION
The pressure range is characterized bythe fact that the moldable mixture is exposed to a gas pressure of at least 2 atmospheres (absolute) using an increasing pressure gradient, dp/dt, of at least 50 atmospheres (absolute)/second, maintaining at least this pressure for at least 0.01 seconds and then allowing the pressure to drop back to normal pressure within at least 0.2 seconds from the onset of the pressure increase.
Theoretically, no upper limit is set for the pressure-rise gradient.
Several tests have shown that an increasing pressure gradient of about 600 atmospheres (absolute)/second is a value which represents a suitable limit regarding both the hardness of the sand mold and the choice of the pressure medium.
The pressure surge wave should be applied to the surface of the sand as a mass flow through change of the amount of air per unit time. The pressure surge may be produced by compressing a gas or by an exothermic reaction of an explosive gas mixture. The pressure surge wave should be reduced to a low final pressure, that is, finally reduced to normal pressure.
A pressure maximum of 4 to 5.5 atmospheres (absolute) in a combustion chamber represents an optimization between the desired strength properties of the sand molds and the cost of sealing the combustion chamber. .[.The maximum.]. .Iadd.An elevated .Iaddend.pressure .Iadd.of at least 2 atmospheres (absolute) .Iaddend.should be maintained for at least 0.01 second and may be .[.mainted.]. .Iadd.maintained .Iaddend.for about 0.03-0.05 seconds.
With regard to the reduction of pressure, two oppositely directed phenomena must be weighed one against the other. On one hand, the pressure drop should not be too rapid, because cracks could form in the molds; whereas, on the other hand, too much time should not be taken for the pressure to drop, otherwise the cycle times for producing the molds would become too long. An upper limit would be in the range of about 2 atmospheres (absolute)/second, up to which limit, crack-free molds with a clean surface can be produced. The maximum pressure is reduced in a time ranging from 0.2 sec. to about 1.5 sec.
In the afore-described process use is made of four parameters to define a pressure surge. These parameters are the increasing pressure gradient, the maximum pressure, the duration of maximum pressure, and the decreasing pressure gradient. These parameters may be varied independently.
The FIGURE shows four pressure surges, all of which are characterized by increasing pressure gradients, maximum pressures, duration of maximum pressure, and decreasing pressure gradients in the aforementioned ranges in accordance with the present invention. Each of the surges starts at normal, i.e. atmospheric pressure and ends at normal, i.e. atmospheric pressure.
Additional influencing factors were investigated to determine the above-mentioned optimum values. Thus, a boundary surface concentration of the raw material particles of 10-9 to 5·10-9 mole/centimeter2, and especially, moreover, a concentration of 1.9 to 2.5·10-9 mole/centimeter2, has been found to be advantageous.
In addition, with regard to making a choice of raw material particles, a determination was made relating to the velocity of propagation of elastic longitudinal waves in such particles, wherein a value of 4 to 7 kilometers/second, and preferably, a velocity of 5.8 to 6.0 kilometers/second, was found to be especially favorable.
For the tests, use was made of raw material particles which had a major constituent which was silicon dioxide. These particles had a compactability which lay between 27 and 60%, and preferably, 32 to 45%.
Compactibility relates to the decrease in volume of the casting mixture after the pressure surge is applied thereto.
Advantageously, the process described finds an application in the precise molding of a casting mold by using a pattern wherein the derived optimum values are so adjusted and combined that a pressure of 80 to 180 Newtons/centimeter2 is produced on the surface of the pattern.
The limiting values thus determined for the pressure rise, for the maximum value and for the pressure reduction, yield data for the optimal operation of equipment for compacting sand.

Claims (14)

I claim:
1. A method for manufacturing molds from casting sand or other mixture comprising raw material particles, binder and water, by applying a pressure surge wave to said casting sand or other mixture in a closed chamber, said pressure surge wave being formed by a process comprising the steps of:
(a) starting from atmospheric pressure in said chamber, increasing said pressure with a pressure gradient of at least about 50 atmospheres/sec to a .[.maximum.]. pressure of at least about 2 atmospheres;
(b) maintaining said .[.maximum.]. pressure .[.of at least.]. .Iadd.in said chamber equal to or above .Iaddend.about 2 atmospheres for at least about 0.01 seconds;
(c) reducing said pressure .[.from said maximum pressure.]. to atmospheric pressure within .[.at least.]. about 0.2 seconds .Iadd.or more .Iaddend.from the initiation of the pressure increase.
2. A process according to claim 1, characterized in that the increasing pressure gradient has a maximum value of about 600 atmospheres (absolute)/sec.
3. A process according to claim 1, characterized in that the maximum value of the pressure p lies between about 4 and about 5.5 atmospheres (absolute).
4. A process according to claim 1, characterized in that the maximum gas pressure is maintained for 0.03 to 0.05 seconds.
5. A process according to claim 1, characterized in that the gas pressure is reduced within about 1.5 seconds.
6. A process according to claim 1, characterized in that the reduction in pressure is carried out using a decreasing pressure gradient up to about 2.0 atmospheres (absolute)/second.
7. A process according to claim 1, characterized in that use is made of raw material particles having a propagation velocity for elastic longitudinal waves of 4 to 7 kilometers/second, and preferably of 5.8 to 6.0 kilometers/second.
8. A process according to claim 1, characterized in that use is made of raw material particles whose boundary surface concentration is 10-9 to 5·10-9 mole/centimeter2, and preferably 1.9·10-9 to 2.5·10-9 mole/centimeter2.
9. A process according to claim 1, characterized in that the raw material particles comprise mainly silicon dioxide.
10. A process according to claim 1, characterized in that the pressure rise is effected by compressing a gas.
11. A process according to claim 1, characterized in that the pressure rise is produced by the exothermic reaction of an explosive gas mixture.
12. A process according to claim 1, characterized in that use is made of a mixture with a volume capable of being compacted by 27 to 60% upon application of said pressure surge wave, and preferably by 32 to 45%.
13. The use of the process according to claim 1, characterized in that a maximum pressure of 80 to 180 Newtons/centimeter2, is produced on the surface of a pattern. .Iadd.
14. A method for manufacturing molds from casting sand or other mixture comprising raw material particles, binder and water, by applying a pressure surge wave to said casting sand or other mixture in a closed chamber, said pressure surge wave being formed by a process comprising the steps of:
(a) starting from atmospheric pressure in said chamber, increasing said pressure with a pressure gradient of at least about 50 atmospheres/sec to a maximum pressure of at least about 2 atmospheres;
(b) maintaining said maximum pressure of at least about 2 atmospheres for at least about 0.01 seconds;
(c) reducing said pressure from said maximum pressure to atmospheric pressure within about 0.2 seconds or more from the initiation of the pressure increase. .Iaddend. .Iadd.15. A process according to claim 14, characterized in that the increasing pressure gradient has a maximum value of about 600 atmospheres (absolute)/sec. .Iaddend. .Iadd.16. A process according to claim 14, characterized in that the maximum value of the pressure lies between about 4 and about 5.5 atmospheres (absolute). .Iaddend. .Iadd.17. A process according to claim 14, characterized in that the maximum gas pressure is maintained for 0.03 to 0.05 seconds. .Iaddend. .Iadd.18. A process according to claim 14, characterized in that the gas pressure is reduced within about 1.5 seconds. .Iaddend. .Iadd.19. A process according to claim 14, characterized in that the reduction in pressure is carried out using a decreasing pressure gradient up to about 2.0 atmospheres (absolute)/second. .Iaddend. .Iadd.20. A process according to claim 14, characterized in that use is made of raw material particles having a propagation velocity for elastic longitudinal waves of 4 to 7 kilometers/second, and preferably of 5.8 to 6.0 kilometers/second. .Iaddend. .Iadd.21. A process according to claim 14, characterized in that use is made of raw material particles whose boundary surface concentration is 10-9 to 5×10-9 mole/centimeter2, and preferably 1.9×10-9 to 2.5×10-9 mole/centimeter2. .Iaddend. .Iadd.22. A process according to claim 14, characterized in that the raw material particles comprise mainly silicon dioxide. .Iaddend. .Iadd.23. A process according to claim 14, characterized in that the pressure rise is effected by compressing a gas. .Iaddend. .Iadd.24. A process according to claim 14, characterized in that the pressure rise is produced by the exothermic reaction of an explosive gas mixture. .Iaddend. .Iadd.25. A process according to claim 14, characterized in that use is made of a mixture with a volume capable of being compacted by 27 to 60% upon application of said pressure surge wave, and preferably by 32 to 45%. .Iaddend. .Iadd.26. The use of the process according to claim 14, characterized in that a maximum pressure of 80 to 180 Newtons/centimeter2, is produced on the surface of a pattern. .Iaddend.
US06/880,721 1981-12-11 1982-12-09 Method for the manufacture of molds using casting sand or another mixture of raw material particles Expired - Fee Related USRE32622E (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813149172 DE3149172A1 (en) 1981-12-11 1981-12-11 "METHOD FOR PRODUCING MOLDED BODIES USING GAS PRESSURE"
DE3149172 1981-12-11

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US06/531,827 Ceased US4546810A (en) 1981-12-11 1982-12-09 Method for the manufacture of molds using casting sand or another mixture of raw material particles

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US (2) USRE32622E (en)
EP (1) EP0096045A1 (en)
JP (1) JPS58502090A (en)
AU (1) AU1013183A (en)
CA (1) CA1217620A (en)
DD (1) DD208311B5 (en)
DE (1) DE3149172A1 (en)
DK (1) DK364983D0 (en)
IT (1) IT1191115B (en)
WO (1) WO1983002078A1 (en)
ZA (1) ZA829066B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5020582A (en) * 1988-10-29 1991-06-04 Bmd Badische Maschinenfabrik Durlach Gmbh Method and apparatus for compacting foundry molding material in a foundry mold

Families Citing this family (7)

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Publication number Priority date Publication date Assignee Title
DE3344520A1 (en) * 1983-12-09 1985-06-20 BMD Badische Maschinenfabrik Durlach GmbH, 7500 Karlsruhe DEVICE FOR COMPRESSING FOUNDRY MOLD BY PRESSURE GAS
CH666636A5 (en) * 1984-01-09 1988-08-15 Fischer Ag Georg PROCESS FOR COMPRESSING GRAINY MOLDING MATERIALS.
CH672270A5 (en) * 1986-12-17 1989-11-15 Fischer Ag Georg
US5136497A (en) * 1990-07-12 1992-08-04 Bdm International, Inc. Material consolidation modeling and control system
US5202837A (en) * 1990-07-12 1993-04-13 Coe Carlos J Material consolidation modeling and control system
CH686412A5 (en) * 1992-03-10 1996-03-29 Fischer Georg Giessereianlagen A method of compacting molding sand for molds.
BRPI0114571B1 (en) 2000-10-11 2016-11-08 Rovi Guides Inc systems and methods for providing on-demand or on-demand media storage on server servers

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US2847736A (en) * 1954-12-31 1958-08-19 Pulvermacher Dietrich Device for making sand molds for metal casting
US3170202A (en) * 1962-08-22 1965-02-23 Sr William J Huston Foundry process
US3659642A (en) * 1969-12-05 1972-05-02 Lev Fedorovich Vasilkovsky Apparatus for compacting a moulding mixture
FR2141235A5 (en) * 1971-06-08 1973-01-19 Dynamit Nobel Ag
DE2249244A1 (en) * 1972-10-07 1974-04-11 Buderus Eisenwerk Explosive compaction and hardening of moulding sand - contg. plastics binder, by controlled detonation of gas mixts esp. hydrogen- oxygen
DE2844464B1 (en) * 1978-10-12 1980-04-24 Eugen Dipl-Ing Buehler Method and device for compacting casting molds
JPS55133847A (en) * 1979-04-05 1980-10-18 Sintokogio Ltd Molding method of mold and device thereof
JPS55141355A (en) * 1979-04-19 1980-11-05 Sintokogio Ltd Mold molding method and its device
JPS55147462A (en) * 1979-05-08 1980-11-17 Sintokogio Ltd Molding method of lower mold and squeeze plate device
US4289194A (en) * 1979-04-11 1981-09-15 Sintokogio Ltd. Molding machine
US4306609A (en) * 1978-12-15 1981-12-22 Georg Fischer Aktiengesellschaft Method and apparatus for packing granular materials
US4415015A (en) * 1979-02-02 1983-11-15 George Fischer, Ltd. Process of compacting moulding sand
US4483383A (en) * 1980-11-06 1984-11-20 George Fischer Ltd. Process for compacting granular materials

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CH640757A5 (en) * 1979-04-04 1984-01-31 Fischer Ag Georg METHOD AND DEVICE FOR COMPRESSING MOLDING MATERIALS.
WO1982003348A1 (en) * 1981-04-02 1982-10-14 Koebel Alfons Method and device for pneumatically compacting molding sand

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US2847736A (en) * 1954-12-31 1958-08-19 Pulvermacher Dietrich Device for making sand molds for metal casting
US3170202A (en) * 1962-08-22 1965-02-23 Sr William J Huston Foundry process
US3659642A (en) * 1969-12-05 1972-05-02 Lev Fedorovich Vasilkovsky Apparatus for compacting a moulding mixture
FR2141235A5 (en) * 1971-06-08 1973-01-19 Dynamit Nobel Ag
DE2249244A1 (en) * 1972-10-07 1974-04-11 Buderus Eisenwerk Explosive compaction and hardening of moulding sand - contg. plastics binder, by controlled detonation of gas mixts esp. hydrogen- oxygen
DE2844464B1 (en) * 1978-10-12 1980-04-24 Eugen Dipl-Ing Buehler Method and device for compacting casting molds
US4306609A (en) * 1978-12-15 1981-12-22 Georg Fischer Aktiengesellschaft Method and apparatus for packing granular materials
US4415015A (en) * 1979-02-02 1983-11-15 George Fischer, Ltd. Process of compacting moulding sand
JPS55133847A (en) * 1979-04-05 1980-10-18 Sintokogio Ltd Molding method of mold and device thereof
US4289194A (en) * 1979-04-11 1981-09-15 Sintokogio Ltd. Molding machine
JPS55141355A (en) * 1979-04-19 1980-11-05 Sintokogio Ltd Mold molding method and its device
JPS55147462A (en) * 1979-05-08 1980-11-17 Sintokogio Ltd Molding method of lower mold and squeeze plate device
US4483383A (en) * 1980-11-06 1984-11-20 George Fischer Ltd. Process for compacting granular materials

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5020582A (en) * 1988-10-29 1991-06-04 Bmd Badische Maschinenfabrik Durlach Gmbh Method and apparatus for compacting foundry molding material in a foundry mold

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IT8224627A0 (en) 1982-12-06
JPS58502090A (en) 1983-12-08
EP0096045A1 (en) 1983-12-21
CA1217620A (en) 1987-02-10
DD208311B5 (en) 1994-08-25
DD208311A5 (en) 1984-05-02
DK364983A (en) 1983-08-10
IT1191115B (en) 1988-02-24
WO1983002078A1 (en) 1983-06-23
IT8224627A1 (en) 1984-06-06
AU1013183A (en) 1983-06-30
DK364983D0 (en) 1983-08-10
US4546810A (en) 1985-10-15
DE3149172A1 (en) 1983-06-30
ZA829066B (en) 1983-09-28

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