US3433282A - Method for eliminating hot tear cracks in castings - Google Patents

Method for eliminating hot tear cracks in castings Download PDF

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US3433282A
US3433282A US513874A US3433282DA US3433282A US 3433282 A US3433282 A US 3433282A US 513874 A US513874 A US 513874A US 3433282D A US3433282D A US 3433282DA US 3433282 A US3433282 A US 3433282A
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casting
castings
core
hot
hot tear
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US513874A
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Bryant W Crocker
Frederick Schmid
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US Department of Army
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US Department of Army
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D7/00Casting ingots, e.g. from ferrous metals
    • B22D7/06Ingot moulds or their manufacture
    • B22D7/10Hot tops therefor
    • B22D7/104Hot tops therefor from exothermic material only

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  • FIG. 1 A first figure.
  • This invention relates to the production of higher quality castings by eliminating a casting defect known as hot tear cracking a condition in which the surface of the casting splits or cracks leaving open grooves or furrows in the casting surface.
  • hot tear cracking occurs in the hotter, weaker areas of the casting and at a critical temperature depending on the chemistry and the stress imposed on the hotter, weaker areas by the other sections of the casting which are contracting during cooling; depending upon existing conditions of individual castings, this critical temperature usually occurs at the time of development of liquid film during the process of solidification.
  • This object is generally accomplished by control of metal temperature in the areas of the casting which are prone to hot tears, by keeping these areas well above the solidus temperature while the balance of the castings which imposes the stress is undergoing a high percentage of contraction.
  • the desired result is obtained by using an exothermic material or a refractory insulating material both designed to keep the socalled weaker area at a higher temperature during contraction and solidification of the balance of the casting and with no harmful effect to any part of the casting.
  • FIGURE 1 is an illustration in cross section of the use of an exothermic material in the areas prone to hot tearing
  • FIGURE 2 is an illustration in cross section of the use of an insulating material as the inner core of the mold.
  • FIGURE 1 there is shown a steel casting 10, an internal sand core 11 vented in the usual manner (not shown) with exothermic material 12 padding the corners 13 and 14 of the mold.
  • the exothermic material is placed in the areas where hot tear cracking is most likely to occur and supplies the ad- 3,433,282 Patented Mar. 18, 1969 ditional heat necessary to maintain these weaker areas above the solidus temperature while the balance of the casting is exerting a stress thereon during the solidification period.
  • This exothermic padding material on contacting the molten metal is ignited and heats to a temperature greater than 3000 F. and this heat input to the adjacent metal keeps the temperature in the area or at the interface of the padding material above the critical temperature at which the hot tear occurs.
  • FIGURE 2 shows a tubular tool steel casting 15 having dry refractory insulating material 16 for an inner core with a thin layer sand core 17 therebetwen.
  • the core would not be vented to carry off accumulated heat and the retention of heat by the insulating material is the means of supplying the heat necessary to keep the area prone to hot tear cracking, namely the inner periphery 18 of the tubular casting 15, above the solidus temperature during the solidification and contraction of the balance of the casting in the cooling period.
  • the molds employed were of green sand, AFS fineness No. 60-70 and were well vented to assist in exhausting gases generated by the padding material which were not removed through the core vents;
  • the basic core was a cold setting resin core mix which was hollowed out and filled with a weak bedding sand and properly vented; a one-eighth inch thickness of exothermic padding was placed in the radii area during the making of the basic core which was then baked at 400 F. (204.4 C.) for eight hours and after cooling was covered with two coats of a proprietary zircon wash; utilizing a 5500 lb.
  • a method of eliminating hot tear cracks in castings having recessed portions comprising, casting a metal around a core padded with an exothermic material in areas prone to hot tear cracks and cooling said casting while said padded areas are maintained longer at a higher temperature than the balance of said casting by additional heat supplied by the ignited exothermic material whereby the solidified casting is entirely free of hot tear cracks.
  • a method of eliminating hot tear cracks in high quality castings having recessed portions comprising, casting a metal around a core padded on its exterior surface with an exothermic material in areas adjacent to portions of the castings which are prone to hot tear cracks and cooling said casting while said padded areas are maintained by the ignited exothermic material above the solidus temperature during the stress imposed by the contraction of the balance of the casting whereby the solidified casting is entirely free of hot tear cracks.
  • a method of eliminating hot tear cracks in high quality metal castings having recessed portions comprising, utilizing a sand core for a casting, padding the core on its exterior surface adjacent recessed areas of the casting prone to hot tear cracking with a thin layer of an exothermic material, casting the metal around the padded core and maintaining during cooling said prone areas above solidus temperature by additional heat supplied by contact of exothermic material with the cast metal during the contraction of the remainder of the casting whereby all areas of cast metal are entirely free of hot tear cracks.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Description

M51481 18, 1969 CROCKER ET AL 3,433,282
METHOD FOR ELIMINATING HOT TBAR CRACKS 1N CASTINGS Filed D80. 14, 1965 I0 STEEL CASTING J2 I2 EXOTHERMIC MATERIAL.
FIG. 1
TOOL STEEL CASTING l5 THIN LAYER OF SAND CORE /7 F! G. 2
DRY REFRACT RY INNER CORE /6 (msuLAT/ms MATERIAL) INVENTORS BRYANT W. CROCKER J W ATTORNEYS Unitcd States Patent 3,433,282 METHOD FOR ELIMINATING HOT TEAR CRACKS IN CASTINGS Bryant W. Crocker, Reading, and Frederick Schmid, Cambridge, Mass., assignors to the United States of America as represented by the Secretary of the Army Filed Dec. 14, 1965, Ser. No. 513,874
US. Cl. 164--53 Int. Cl. B22d 19/00 3 Claims ABSTRACT OF THE DISCLOSURE The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment to us of any royalty thereon.
This invention relates to the production of higher quality castings by eliminating a casting defect known as hot tear cracking a condition in which the surface of the casting splits or cracks leaving open grooves or furrows in the casting surface.
It is generally agreed that hot tear cracking occurs in the hotter, weaker areas of the casting and at a critical temperature depending on the chemistry and the stress imposed on the hotter, weaker areas by the other sections of the casting which are contracting during cooling; depending upon existing conditions of individual castings, this critical temperature usually occurs at the time of development of liquid film during the process of solidification.
The occurrence of hot tearing in castings has been a constant problem of foundries required to produce and deliver high quality crack-free castings. When hot tearing cannot be eliminated, it is generally removed by grinding and welding at a highr cost of foundry time.
It is therefore, the object of this invention to eliminate hot tear cracking in high quality castings with a substantial savings in cost and time.
This object is generally accomplished by control of metal temperature in the areas of the casting which are prone to hot tears, by keeping these areas well above the solidus temperature while the balance of the castings which imposes the stress is undergoing a high percentage of contraction. Specifically, the desired result is obtained by using an exothermic material or a refractory insulating material both designed to keep the socalled weaker area at a higher temperature during contraction and solidification of the balance of the casting and with no harmful effect to any part of the casting.
The application of this treatment is shown diagrammatically in the drawing in which:
FIGURE 1 is an illustration in cross section of the use of an exothermic material in the areas prone to hot tearing; and
FIGURE 2 is an illustration in cross section of the use of an insulating material as the inner core of the mold.
In the drawing, with particular reference to FIGURE 1, there is shown a steel casting 10, an internal sand core 11 vented in the usual manner (not shown) with exothermic material 12 padding the corners 13 and 14 of the mold. The exothermic material is placed in the areas where hot tear cracking is most likely to occur and supplies the ad- 3,433,282 Patented Mar. 18, 1969 ditional heat necessary to maintain these weaker areas above the solidus temperature while the balance of the casting is exerting a stress thereon during the solidification period. This exothermic padding material on contacting the molten metal is ignited and heats to a temperature greater than 3000 F. and this heat input to the adjacent metal keeps the temperature in the area or at the interface of the padding material above the critical temperature at which the hot tear occurs.
FIGURE 2 shows a tubular tool steel casting 15 having dry refractory insulating material 16 for an inner core with a thin layer sand core 17 therebetwen. In this casting the core would not be vented to carry off accumulated heat and the retention of heat by the insulating material is the means of supplying the heat necessary to keep the area prone to hot tear cracking, namely the inner periphery 18 of the tubular casting 15, above the solidus temperature during the solidification and contraction of the balance of the casting in the cooling period.
There are castings of diflicult shapes which are particularly conducive to hot tearing, such for example, as alloy steel cradles. Such a casting has internal angles which create natural hot spots the heat from which is normally rapidly dissipated through the adjacent core material. The thin walls required and the necessary large core provide casting configurations contributing to hot tearing due to core restraint. The reason for this is that the internal radii during cooling does no have suflicient ductility at higher temperatures to resist the strain imposed on it by the contracting metal of the balance of the casting and the large core hinders the required total contratcion of the cooling metal.
The treatment of this invention was applied to castings of a 350 lb. alloy steel cradle as follows:
The molds employed were of green sand, AFS fineness No. 60-70 and were well vented to assist in exhausting gases generated by the padding material which were not removed through the core vents; the basic core was a cold setting resin core mix which was hollowed out and filled with a weak bedding sand and properly vented; a one-eighth inch thickness of exothermic padding was placed in the radii area during the making of the basic core which was then baked at 400 F. (204.4 C.) for eight hours and after cooling was covered with two coats of a proprietary zircon wash; utilizing a 5500 lb. electric induction furnace charged with cold scrap, when the contents were molten, a chemical analysis from a vacuum spectrometer determined the required amounts of pig, ferrochrome and ferromolybdenum to be added, to ensure a time boil; before tapping the furnace, ferromanganese and ferrosilicon were added; the contents of the furnace were tapped into a preheated ladle at 3075 F. (1691 C.) and deoxidized with .10% aluminum in the ladle; the molten material at a temperature of 2975 F. (1635 C.) was poured into six molds with the pouring time of one mold being 45 seconds; these cradle castings were heat treated by normalizing at 1650 F. (989.9 C.) for four hours, austenized at 1600 F. (871.1 C.) for three hours, quenched in oil and tempered to obtain the desired physical properties.
No evidence of hot tearing of these castings utilizing the exothermic padding material in the radii area could be detected by the magnafiux inspection.
Chemical analysis of the casting surface, to detect possible casting contamination from the exothermic material, revealed that there was no evidence of chemical pickup from the padding material which would decrease the quality of the casting.
Physical properties were also tested from the radius area of a heat treated casting which employed a core with exothermic material and from other areas of the same casting which were not in contact with the padding material, and there was no evidence of the physical properties of the casting being lowered by the use of the padding material.
The results from over 100 castings show that controlled use of exothermic material will definitely eliminate hot tearing and reduce excessive casting repair which averages six hours of foundry time per casting.
This procedure, which has been utilized to eliminate all external hot tearing in the radii of 350 lb. steel alloy cradle castings, has also been employed successfully on 1200 lb. alloy steel breech ring castings.
What is claimed is:
1. A method of eliminating hot tear cracks in castings having recessed portions comprising, casting a metal around a core padded with an exothermic material in areas prone to hot tear cracks and cooling said casting while said padded areas are maintained longer at a higher temperature than the balance of said casting by additional heat supplied by the ignited exothermic material whereby the solidified casting is entirely free of hot tear cracks.
2. A method of eliminating hot tear cracks in high quality castings having recessed portions comprising, casting a metal around a core padded on its exterior surface with an exothermic material in areas adjacent to portions of the castings which are prone to hot tear cracks and cooling said casting while said padded areas are maintained by the ignited exothermic material above the solidus temperature during the stress imposed by the contraction of the balance of the casting whereby the solidified casting is entirely free of hot tear cracks.
3. A method of eliminating hot tear cracks in high quality metal castings having recessed portions comprising, utilizing a sand core for a casting, padding the core on its exterior surface adjacent recessed areas of the casting prone to hot tear cracking with a thin layer of an exothermic material, casting the metal around the padded core and maintaining during cooling said prone areas above solidus temperature by additional heat supplied by contact of exothermic material with the cast metal during the contraction of the remainder of the casting whereby all areas of cast metal are entirely free of hot tear cracks.
References Cited UNITED STATES PATENTS 2,335,008 11/1943 Hites 164-53 X 2,568,428 9/1951 Billiar 16453 X 2,925,637 2/1960 Edmonds et a1. 164'--53 3,204,301 9/ 1965 Flemings et a1 16453 3,212,749 10/1965 LaBate 164-53 X J. SPENCER OVERHOLSER, Primary Examiner.
E. MAR, Assistant Examiner.
U.S. Cl. X.R. 164-369; 249200
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3662809A (en) * 1968-10-03 1972-05-16 John Ernest Gotheridge Method of producing metal castings by using insulating pads in the mold
US5135690A (en) * 1986-01-22 1992-08-04 Honda Giken Kogyo Kabushiki Kaisha Process for producing cylindrical reinforcing fibrous molding
US5394932A (en) * 1992-01-17 1995-03-07 Howmet Corporation Multiple part cores for investment casting
EP2823916A1 (en) * 2013-07-10 2015-01-14 Georg Fischer GmbH Composite casting
US10105755B2 (en) 2014-07-14 2018-10-23 Gf Casting Solutions Mettmann Gmbh Composite casting part

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2335008A (en) * 1943-01-28 1943-11-23 Ohio Steel Foundry Co Means for casting metals
US2568428A (en) * 1949-09-09 1951-09-18 Irvin A Billiar Mold with riser and exothermic insert
US2925637A (en) * 1956-04-05 1960-02-23 Foundry Services Ltd Manufacture of metal ingots and castings
US3204301A (en) * 1960-10-24 1965-09-07 M C Flemings Jr Casting process and apparatus for obtaining unidirectional solidification
US3212749A (en) * 1964-03-24 1965-10-19 Bate Micheal Donald La Consumable hot top with inserts of exothermic material

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2335008A (en) * 1943-01-28 1943-11-23 Ohio Steel Foundry Co Means for casting metals
US2568428A (en) * 1949-09-09 1951-09-18 Irvin A Billiar Mold with riser and exothermic insert
US2925637A (en) * 1956-04-05 1960-02-23 Foundry Services Ltd Manufacture of metal ingots and castings
US3204301A (en) * 1960-10-24 1965-09-07 M C Flemings Jr Casting process and apparatus for obtaining unidirectional solidification
US3212749A (en) * 1964-03-24 1965-10-19 Bate Micheal Donald La Consumable hot top with inserts of exothermic material

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3662809A (en) * 1968-10-03 1972-05-16 John Ernest Gotheridge Method of producing metal castings by using insulating pads in the mold
US5135690A (en) * 1986-01-22 1992-08-04 Honda Giken Kogyo Kabushiki Kaisha Process for producing cylindrical reinforcing fibrous molding
US5394932A (en) * 1992-01-17 1995-03-07 Howmet Corporation Multiple part cores for investment casting
US5498132A (en) * 1992-01-17 1996-03-12 Howmet Corporation Improved hollow cast products such as gas-cooled gas turbine engine blades
EP2823916A1 (en) * 2013-07-10 2015-01-14 Georg Fischer GmbH Composite casting
US10105755B2 (en) 2014-07-14 2018-10-23 Gf Casting Solutions Mettmann Gmbh Composite casting part

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