US2294959A - Metal casting - Google Patents
Metal casting Download PDFInfo
- Publication number
- US2294959A US2294959A US324976A US32497640A US2294959A US 2294959 A US2294959 A US 2294959A US 324976 A US324976 A US 324976A US 32497640 A US32497640 A US 32497640A US 2294959 A US2294959 A US 2294959A
- Authority
- US
- United States
- Prior art keywords
- mold
- casting
- metal
- air
- cavity
- 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 - Lifetime
Links
- 238000005058 metal casting Methods 0.000 title description 5
- 238000005266 casting Methods 0.000 description 18
- 238000000034 method Methods 0.000 description 14
- 239000002184 metal Substances 0.000 description 11
- 238000001816 cooling Methods 0.000 description 8
- 229910000831 Steel Inorganic materials 0.000 description 7
- 239000010959 steel Substances 0.000 description 7
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 208000015943 Coeliac disease Diseases 0.000 description 2
- 235000011089 carbon dioxide Nutrition 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/12—Treating moulds or cores, e.g. drying, hardening
- B22C9/126—Hardening by freezing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
Definitions
- the present invention relates to improvements in metal casting, and particularly to the casting of metal having high shrinkage characteristics such as steel,. or castings of great bulk, or unsymmetrical shape; and the objects of.
- Figure 1 is a part sectional view of the air' cooling apparatus preferably employed to cool the mold in which iscast metal inlaccordance with my method of metal casting. the view being taken on a vertical plane through the axis of the cooling tunnel and the mold in which is shown a mold cavity adapted for casting a bevel gear blank, the refrigerating apparatus beingishown diagrammatically.
- Figure 2 is a part sectional view of the cooling tunnel adapted to cool the core of'an artillery projectile which is alone supported on a cradle dryer within the cooling tunnel cooled by the refrigerating coils shown diagrammatically as also the apparatus.
- Figure 3 is a cross-sectional view of a mold in which to cast a plurality of artillery pro- :lectile bodies. the view being taken on a vertical plane through two of the mold cavities, in one of which is shown-the core whereby is formed the explosive charge cavity.
- Figure 4 is a longitudinal cross-sectional view of aprojectile body that my improved method of metal casting is particularly adapted to.
- Figure 1 illustrates one method of cooling a mold, by circulating through the mold cavities 'lownship
- apparatus comprises generally, the same refrigerating elements as that of Figure 1, such as therefrigerating coil ll gas compressor-i2, condenser coils l3, compressorconnecting tube it and liquid receiver II it difl'ering therefrom only in that the refrigerating coils are arranged within a rectangular cross-sectional housing I8, ad-
- FIG. 22 illustrating a mold 22 in which to cast artillery shell bodies, which is cooled by either the method 7 shown in Figure 1, or; by packing carbon dioxide, commonly referred to as dry ice.
- This dry ice is preferably formed to near" the shape of,the mold cavities on a hollow perforated man-' drel 23 and inserted in-the mold cavity 24.
- the mold cavity has therein the core 2i, as shown in Fig. 2, being cooled by refrigeration.
- Castings of irregular, shape,,or those having a heavy portion adjacent a lighter portion will usually have a ragged voidwithin the casting at the refrigerated dry-air cooled to a lower temperaheavier portion, or cracks extending inwardly from the junction of the light and heavy secformed, the purpose being' to bring about as near as possible, a uniform solidification of the casting and consequently, uniform shrinkage.
- Another method is to provide excessively large riser passages in which the metal is kept in a.
- a third method is to provide large riser passage and to apply pressure to the molten metal in the passage during solidification of the metal in the mold cavities.
- the first method described requires that a large quantity of specially shaped chill blocks be maintained, with frequent renewals when lost or damaged, :besides leaving objectionable marking on the casting.
- the second and third methods are objectionable on account of waste and cost, because of the heavy sprues and the labor required to prepare for casting and cutting the heavy sprues from the casting.
- the mold including cores, is cooled to a low temperature, insome cases, as when a very heavy casting is to be produced, to considerably below zero Fahrenheit, and in extreme cases as low as seventy or more below zero Fahrenheit.
- the mold can be considerably above zero, and even above thirty-two degrees Fahrenheit forthe cast; ing of very light section castings. Therefore, when the molten metal is poured into the mold cavity so cooled, it is caused to solidify-quickly and sufficiently rapidly to prevent internal shrinkage.
- shrinkage as takes place is the normal linear shrinkage of the casting and therefore in the outer dimension of the casting only.
- the method of casting steel consisting in providing a mold having amold cavity and passages extending to said cavity, refrigerating air to a temperature of approximately zero degrees Fahrenheit, blowing the refrigerated air into the mold cavity until the mold has reached a tem- ;perature below thirty-two degrees Fahrenheit and while the mold temperature is below thirtytwo degrees Fahrenheit, flowing molten steel into the mold cavity.
- the method or casting steel consisting inproviding a mold having a mold cavity and passages extending to the said cavity, refrigerating air to a temperature below thirty-two degrees Fahrenheit, passing said refrigerated air through said passages and mold cavity until the mold around the cavity is cooled to a temperature below thirty-two degrees Fahrenheit and while the mold around the cavity is below thirty-two degrees Fahrenheit, depositing in the mold cavity, molten steel.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Description
Sept. 8, 1942. N. CAMPBELL ET AL 2,294,959
METAL CASTING Filed March 20, 1940 2 Sheets-Sheet l Snvcutor 871M124 L/. M
Gttorncg Sep t 8, 1942, N. M. CAMPBELL ET AL 2,294,959
METAL CASTINQ I Filed March 20, 1940 2 Sheets-Sheet 2 [1/ [VII man mam ball Bu D na/d c7. rl/i mum Snnentor (Ittorneg Patented Sept. 8,1942
UNITED STATES PATENT OFFlCE METAL cas'rmc' Norman M. Campbell, Muskegon Heights, and
Donald J. Campbell, Spring lake Ottawa County, Mich. Application March 20,1940, sci-m No. 324,916 a 3 Claims. (Cl. 22-212) The present invention relates to improvements in metal casting, and particularly to the casting of metal having high shrinkage characteristics such as steel,. or castings of great bulk, or unsymmetrical shape; and the objects of. improvement are, first, to provide a method by which castings free from internal defects can be economically produced from metal having high shrinkage characteristics: second, to provide a method whereby bulky metal castings can be produced that are-free from shrinkage depressions on their exterior or voids within; third, to provide a method whereby metal castings produced thereby will have a' finer grain structure than castingsproduced by usual foundry practice; fourth, to provide a method whereby castin s of uniform 'grain structure will be produced; fifth, to provide a method whereby castings free from internal flaws of all kinds can be produced. The above named objects and other objects that appear from a perusal of the method herein describe assistedby the devices diagram-' matically illustrated, are attained by such devim shown in the accompanying drawings, in w h:
Figure 1 is a part sectional view of the air' cooling apparatus preferably employed to cool the mold in which iscast metal inlaccordance with my method of metal casting. the view being taken on a vertical plane through the axis of the cooling tunnel and the mold in which is shown a mold cavity adapted for casting a bevel gear blank, the refrigerating apparatus beingishown diagrammatically.
Figure 2 is a part sectional view of the cooling tunnel adapted to cool the core of'an artillery projectile which is alone supported on a cradle dryer within the cooling tunnel cooled by the refrigerating coils shown diagrammatically as also the apparatus.
Figure 3 is a cross-sectional view of a mold in which to cast a plurality of artillery pro- :lectile bodies. the view being taken on a vertical plane through two of the mold cavities, in one of which is shown-the core whereby is formed the explosive charge cavity. a
Figure 4 is a longitudinal cross-sectional view of aprojectile body that my improved method of metal casting is particularly adapted to. and
as would befprpduced in the mold shown in Fi ure 3.
Referring further to Figures 1, 2, and 3. Figure 1 illustrates one method of cooling a mold, by circulating through the mold cavities 'lownship,
tur'e, by the device shown diagrammatically as comprising a centrifugal air drier and fan i,
having its discharge 2 connected to the air cooling tunnel 3, surrounded by suitable tempera- 1 ture insulation 4, and having a flexible tubular air conductor 5 provided with a canvas-like funnel-shaped hood 6, held against the mold I over the gate riser 8 connected with the mold cavity .9, and held securely thereover byweight lot Within the air cooling'tunnel 3 is refrigerating coil ll connected 'to the gas compressor l2 through condenser coils i3 at one of its ends, and its other end connected .to the compressor l2 by tube and liquid receiver II. From the abovedescription it will readily be understood that the air delivered to the mold will first be, to a great extent, dehydrated 'by the air drier and forced thereby through the tunnel 3, around the refrigerating coils ll therein by which the air will be cooled to a low temperature, and by passing to and through the mold, will cool or refrigerate the'mold to the required low temperature degree. Figure 2 represents the cooling of a core as employed in casting artillery shell bodies. The.
apparatus comprises generally, the same refrigerating elements as that of Figure 1, such as therefrigerating coil ll gas compressor-i2, condenser coils l3, compressorconnecting tube it and liquid receiver II it difl'ering therefrom only in that the refrigerating coils are arranged within a rectangular cross-sectional housing I8, ad-
jacent-the walls thereof and in which is core supporting carriage 19 for supporting the core drier 20 on which rests core 2|, which core is the same as the core illustrated in Figure 3,
illustrating a mold 22 in which to cast artillery shell bodies, which is cooled by either the method 7 shown in Figure 1, or; by packing carbon dioxide, commonly referred to as dry ice. This dry ice is preferably formed to near" the shape of,the mold cavities on a hollow perforated man-' drel 23 and inserted in-the mold cavity 24. The mold cavity has therein the core 2i, as shown in Fig. 2, being cooled by refrigeration.
Bulky castings produced by the usual foundry methods invariably have depressionsin their top,
which are caused by shrinkage of the metal during solidification of the metal within the castin after the outer shell portion has solidified. Castings of irregular, shape,,or those having a heavy portion adjacent a lighter portion, will usually have a ragged voidwithin the casting at the refrigerated dry-air cooled to a lower temperaheavier portion, or cracks extending inwardly from the junction of the light and heavy secformed, the purpose being' to bring about as near as possible, a uniform solidification of the casting and consequently, uniform shrinkage. Another method is to provide excessively large riser passages in which the metal is kept in a.
molten state by churning with a steel rod, thus feeding molten metal to the heavy portion of the casting to overcome shrinkage voids during solidification of the molten metal therein. A third method is to provide large riser passage and to apply pressure to the molten metal in the passage during solidification of the metal in the mold cavities.
The first method described requires that a large quantity of specially shaped chill blocks be maintained, with frequent renewals when lost or damaged, :besides leaving objectionable marking on the casting. The second and third methods are objectionable on account of waste and cost, because of the heavy sprues and the labor required to prepare for casting and cutting the heavy sprues from the casting.
In the present improved method of metal casting, the mold, including cores, is cooled to a low temperature, insome cases, as when a very heavy casting is to be produced, to considerably below zero Fahrenheit, and in extreme cases as low as seventy or more below zero Fahrenheit. In the production of lighter castings, the mold can be considerably above zero, and even above thirty-two degrees Fahrenheit forthe cast; ing of very light section castings. Therefore, when the molten metal is poured into the mold cavity so cooled, it is caused to solidify-quickly and sufficiently rapidly to prevent internal shrinkage. Such shrinkage as takes place is the normal linear shrinkage of the casting and therefore in the outer dimension of the casting only.
Having described the present invention, the rights it is desired to secure are disclosed in the claims hereinafter set forth. Therefore, we claim:
1. The method of casting steel consisting in providing a mold having amold cavity and passages extending to said cavity, refrigerating air to a temperature of approximately zero degrees Fahrenheit, blowing the refrigerated air into the mold cavity until the mold has reached a tem- ;perature below thirty-two degrees Fahrenheit and while the mold temperature is below thirtytwo degrees Fahrenheit, flowing molten steel into the mold cavity.
2. The method or casting steel consisting inproviding a mold having a mold cavity and passages extending to the said cavity, refrigerating air to a temperature below thirty-two degrees Fahrenheit, passing said refrigerated air through said passages and mold cavity until the mold around the cavity is cooled to a temperature below thirty-two degrees Fahrenheit and while the mold around the cavity is below thirty-two degrees Fahrenheit, depositing in the mold cavity, molten steel.
3. The method of casting steel consisting in refrigerating air, forcing said refrigerated air into a mold cavity until the mold has reached a temperature below thirty-two degrees Fahrenheit and immediately thereafter depositing molten steel in the mold.
NORMAN M. CAlVIPBELL. DONALD J. CAMPBELL.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US324976A US2294959A (en) | 1940-03-20 | 1940-03-20 | Metal casting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US324976A US2294959A (en) | 1940-03-20 | 1940-03-20 | Metal casting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2294959A true US2294959A (en) | 1942-09-08 |
Family
ID=23265918
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US324976A Expired - Lifetime US2294959A (en) | 1940-03-20 | 1940-03-20 | Metal casting |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2294959A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2766498A (en) * | 1951-09-21 | 1956-10-16 | James C Heintz Company | Use of plaster of paris forms in making metal castings |
| US2844855A (en) * | 1953-11-05 | 1958-07-29 | Bristol Aero Engines Ltd | Method of producing castings with one or more internal passages |
| EP1916493A3 (en) * | 2006-10-26 | 2008-09-17 | Maschinen- und Stahlbau Julius Lippert GmbH & Co. | Plant for drying at least one multi-part casting mould |
-
1940
- 1940-03-20 US US324976A patent/US2294959A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2766498A (en) * | 1951-09-21 | 1956-10-16 | James C Heintz Company | Use of plaster of paris forms in making metal castings |
| US2844855A (en) * | 1953-11-05 | 1958-07-29 | Bristol Aero Engines Ltd | Method of producing castings with one or more internal passages |
| EP1916493A3 (en) * | 2006-10-26 | 2008-09-17 | Maschinen- und Stahlbau Julius Lippert GmbH & Co. | Plant for drying at least one multi-part casting mould |
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