US2299860A - Method and apparatus for centrifugally casting corrosion resistant alloys - Google Patents
Method and apparatus for centrifugally casting corrosion resistant alloys Download PDFInfo
- Publication number
- US2299860A US2299860A US435005A US43500542A US2299860A US 2299860 A US2299860 A US 2299860A US 435005 A US435005 A US 435005A US 43500542 A US43500542 A US 43500542A US 2299860 A US2299860 A US 2299860A
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- 238000005266 casting Methods 0.000 title description 39
- 238000000034 method Methods 0.000 title description 11
- 238000005260 corrosion Methods 0.000 title description 9
- 230000007797 corrosion Effects 0.000 title description 9
- 229910045601 alloy Inorganic materials 0.000 title description 7
- 239000000956 alloy Substances 0.000 title description 7
- 229910052751 metal Inorganic materials 0.000 description 50
- 239000002184 metal Substances 0.000 description 50
- 239000000203 mixture Substances 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 7
- 238000000465 moulding Methods 0.000 description 7
- 229910052799 carbon Inorganic materials 0.000 description 6
- 238000010276 construction Methods 0.000 description 6
- 239000007789 gas Substances 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 6
- 238000005520 cutting process Methods 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- WQZGKKKJIJFFOK-GASJEMHNSA-N Glucose Natural products OC[C@H]1OC(O)[C@H](O)[C@@H](O)[C@@H]1O WQZGKKKJIJFFOK-GASJEMHNSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 239000004927 clay Substances 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000008103 glucose Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 101100188552 Arabidopsis thaliana OCT3 gene Proteins 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910001347 Stellite Inorganic materials 0.000 description 1
- 238000009750 centrifugal casting Methods 0.000 description 1
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/06—Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould
- B22D13/066—Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould several moulds being disposed in a circle
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S76/00—Metal tools and implements, making
- Y10S76/03—Casting
Definitions
- This invention relates to a method and apparatus for making precision castings centrifugally of high melting point corrosion resistant alloys.
- an object of the invention is to provide anew method and mold for making a multiplicity of castings centrifugally of relatively high melting point corrosion resistant alloys so that the castings will be so accurately formed that they will be identical requiring a minimum amount of machining or finishing operations.
- Another object of the invention is to provide a method and apparatus for centrifugally casting metals and like substances wherein adequate provision is made to insure that only firm, clean, dense metal will be introduced into the mold cavity during the centrifugal casting operation, vents and reservoirs for the mold cavity so that pipes that may form as the metal cools will not continue or extendinto the metal of the casting.
- the invention may be employed wherever a multiplicity of identical and'accurately formed castings is desired, it has been primarily designed for the production of the turbine blades of a molten metal adjacent supercharger used on aircraft. In such a construction the supercharger is driven by a turbine,
- exhaust gases which are not infrequently still flaming, are heated to a temperature of approxi- F. They consequently, must be resistant to the burning action of the exhaust gases and should be capable of sustaining a tensile stress of approximate1y70,000 pounds per square inch.
- Figure 1 is a perspective view of a diecast pattern that is employed to make and shape the mold cavity in the mold that forms a part of the apparatus embodying the present invention
- Fig. 2 is a sectional view of a flask illustrating the pattern shown in Fig. l as positioned therein 1 and illustrating the mold as having been reamed R.P. M.
- the blades being subjected to the direct tions of the mold that up or tamped up in the flask about the pattern;
- g. 3 is a top plan view of the mold illustrated as having been formed in Fig. 2 and illustrating in phantom lines the portions of the mold that are removed to produce one segment of the complete centrifugal mold;
- Fig. 4 is a view in side elevation of thesegment produced illustrating in phantom lines the porhave been removed to produce the finished segment;
- Fig. 5 is a view in side elevation of the segment illustrating in phantom that have been removed;
- Fig. 6 is a perspective view of the finished segment that forms a part of the complete centrif ugal mold
- Fig. 7 is atop plan View of the completed centrifugal mold, parts being broken away and shown in horizontal section, the mold being made up of a plurality of segments of the character illustrated in Fig. 6;
- Fig.8 is a vertical section through the mold taken substantially upon the line 8-8 upon Fig. 7;
- v Fig. 9 is a diametrical section through the completed mold;
- FIG. 10 is a partial view in plan illustrating a portion of the casting produced prior to its being divided into the individual turbine blades;
- Fig. 11 is a secti nal view through the portion of the casting illustrated in Fig. 10:
- Figs. 12, 13, and 14 are views of the casting produced, Fig. 12 being a view in side elevation of one side of the turbine blade; Fig. 13 an end elevation of the same; and Fig. 14 a view in side .elevation of the reverse side of the blade;
- Fig. 15 is a sectional view similar to Fig. 8, but illustrating a slightly modified form of construction whereby a much greater multiplicity of castings may be produced from a single pour;
- Fig. 16 is a view similar to Fig. 15, the section however having been taken through the mold on a plane between adjacent segments whereas Fig.
- ' 15 is a section taken through the mold cavities in superposed segments
- Fig. 17 is a view similar to Fig. 11 illustrating a portion of the casting produced from the mold illustrated in Figs. 15 and 16.
- This enlargement is designed to mold or shape the riser or outlet from the mold cavity in the mold that is produced.
- the pattern is preferably diecast so that in making a multiplicity of patterns it is relatively easy to make the patterns identical.
- the metal used for making the pattern is preferably tin as this metal has the required melting point to enable the mold to be properly baked and on baking to be ultimately melted out.
- the pattern illustrated in Fig. 1 is positioned in a suitable flask l which is normally cylindrical in form and which is formed of carbon.
- a suitable flask l which is normally cylindrical in form and which is formed of carbon.
- an aperture I! that snugly receives the stud l4.
- Grooves l8 are formed at diametrically opposite sides of the flask adjacent the top thereof to receive portions of the enlargements I0 and II at the sides of the pattern.
- This molding composition has certain definite requirements in order to produce the desired results.
- the metal that is to be poured has a relatively high melting point and is normally poured at a temperature of approximately 3000 F. it is manifest that the mold-must resist burning or melting. Also, it cannot be so extremely hard that as the casting cools and As a result of a great deal of experimentation we have ascertained that a molding composition composed of the following ingredients in approximately the following proportions gives very satisfactory results.
- Such a mixture is prepared by mulling together the graphitic carbon and fire clay while dry for approximately five minutes. The glucose and Water are warmed to about F. and added thereto and the ingredients thoroughly mixed. The resulting mixture is damp and will hold together on squeezing.
- the molding composition is tamped up rather firmly about the pattern and when the flask is thus filled it is placed in an oven and baked. It is usually advisable to bake the flask and mold therein contained for a considerable length of time at approximately 150 F. to drive out the moisture without creating voids in the mold. The temperature can then be raised to approximately 300 to 400 F. to thoroughly bake the mold and finally its temperature is raised to .approximately 585 F. During this latter treatment the tin pattern melts out of the mold leaving themold cavity 20 formed in the mold equipped with lateral entrances 2
- the beveled surfaces 23 at the upper outer corners of the segment are portions of the original cylindrical surface on the exterior of the mold that are not removed in extends inwardly a short distance over'the top ments. It will be noted that the cylindrical porwill of course be understood that the metal in site the inner end ofthe riser 22 and above this cut away portion there is a shoulder ZLha-ving a beveled under surface 25. Grooves "are then' routed down the outward 1y divergent sides of the 1 5 mold segment to a point indicated at :1 beyond the'entrances 2
- a suitable carrier 28 see Figs. 7 and 8.
- This carrier has a central aperture 29 formed therethrough andradial grooves 30 on its under suri'ace.
- a carbon ring 3! is positioned on the bottom of the carrier and preferably of the aperture 29.
- the segments fit together within an outer upstanding flange 32 around a hollow carbon cone 33 having a vertical or cylindrlcal lower portion 34.
- The-bottom of the cone immediately above the cylindrical portion 34 fits against the beveled surface beneath the shoulder 24 so that the top surface of the cone 33 together with the inner wall of the gate cooperate to direct the metal that is poured through the radial passages 31 that are formed by opposed grooves26 on adjacent segtion at the bottom of the cone 33 has apertures or passages '38 formed therein which register with the inner ends of the risers 22 on the mold segments so that egress from the mold cavity of gases and air is readily permitted through the risers 22 and the passages '38, the aperture 29 and the radial grooves 30.
- the carrier 28- and the mold parts that are thus assembled are then positioned on a suitable rotary table or other rotating device, the axis of rotation of which is coincident with the vertical axis through the cone 33 and through the gate 36.
- the metal that is to be poured may be one of the specific metals above mentioned and is. normally poured at. a temperature of approximately 3000 while the mold is being rotated at a fair rotational speed, such as 1500 R. P. M.
- the metal that is poured into the central gate encounters the cone 33 and is distributed and thrown outwardly through the radial passages 31 formed by the grooves 36.
- the initial metal that enters these passages is apt to become somewhat'chilled and it may beoxidized and if there is any dirt present in the passages it is apt to pick up this dirt.
- This initial metal is consequently carried outwardly to the extreme outer end 21 of the passage and being received in this recess or pocket, remains there.
- succeeding metal flows laterally into the entrances 2
- Those segments 40 that form the lower layer do not have their inner ends. in Figs. 5 and 6 but exte distance so as to shaped as illustrated nd inwardly the full provide a support for the bot tom of the cone 33. These lower segments also do not havethe grooves ZB routed in their sides. When these segments are arranged'to form a lower layer on the carrier 28 an upper row of segments '42 is positioned thereon 'in vertical alignment. These segments 42, however, are of the same size and shape as that previously described and illustrated in Fig. 6. It will be noted from an inspection of Fig. 6 that there is a small web 43 at the bottom of each entrance 2
- the webs 43 of the upper and lower segments are broken out so that metal may flow from the passages 31 produced by the grooves 36 not only into the entrances 2
- the advantages are substantially the same as above described in that the initial metal is first thrown out to the extreme ends of the radial passages 31 and this metal. which may have been chilled, oxidized, or may have picked up dirt, is
- the succeeding metal enters the mold cavities of the upper and lower segments filling the mold cavities and expelling-the air andgases therefrom,
- the method of centrifugally casting metal which includes throwing metal outwardly from a central gate towards the pocket by centrifugal action so that the initial metal poured remains in the pocket, causing succeeding metal to flow laterally into one or more mold cavities and while under centrifugal pressure to fill the mold cavities towards risers arranged inwardly with respect to the mold cavity.
- a mold for centrifugally casting having a mold cavity, the entrance to the cavity being adjacent its outer end and the riser for the mold being adjacent its inner end, there being a passage for molten metal leading from adjacent the center of rotation of the mold to a point beyond the entrance to the mold cavity to form a pocket into which the initial metal poured may flow and be trapped.
- a mold for centrifugally casting having a mold cavity arranged off center with respect to the axis of rotation of the mold, said cavity having entrances at each side adjacent its outer end, and a riser adjacent its inner end, there being passages at each side of the mold cavity leading from adjacent the axis of rotationof the mold toward the entrances.
- a mold for centrifugally casting having a mold cavity arranged ofl center with respect to the axis of rotation of the mold, said cavity having entrances at each side adjacent its outer end, and a riser adjacent its inner end, there being passages at each side of the mold cavity leading from adjacent the axis of rotation of the mold to points beyond the entrances to the cavity so as to provide pockets for receiving and retaining the initial metal poured.
- a mold for centrifugally casting made up of segments arranged around a central gate, each segment having a mold cavity formed therein having an entrance adjacent its outer end and a riser adjacent its inner end, there being passages formed between the segments leading from the gate toward the entrances.
- a mold for centrifugally casting made up of segments arranged around a central gate, each segment having a mold cavity formed therein having an entrance adjacent its outer end and a riser adjacent its inner end, there being passages formed between the segments leading from thegate to points beyond the entrancesto provide pockets that receive and retain the initial metal poured.v
- A'mold for centrifugally casting comprising a plurality of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end, each segment having passages leading outwardly toward the entrances from the gate, a cone providing the bottom of the gate for directing metal poured into the gate into said passages, said cone being passaged to provide outlets from the risers.
- a mold for centrifugally casting comprising a plurality of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end, each segment having passages formed on its sides leading outwardly to points beyond the entrances from the gate, a cone providing a bottom for the gate for directing metal poured into the gate into the passages, said cone being passaged to provide outlets from the risers.
- a mold for centrifugally casting comprising upper and lower layers of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end, each mold cavity having a riser adjacent its inner end, the segments of the upper layer having passages leading outwardly toward the entrances from the gate, and a cone providing the bottom for the gate for directing metal poured into the I gate into said passages.
- a mold for centrifugally casting comprising upper and lower layers of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent .its outer end, each mold cavity having a riser adjacent its inner end, the segments of the upper layer having passages leading outwardly toward the entrances from the gate, and a cone providing the bottom for the gate for directing metal poured into the gate into said pasages, said cone being passaged to provide outlets from at least some of the risers.
- a mold for centrifugally casting comprising a carrier having a central aperture therethrough, grooves on the underside of the carrier, a plurality of segments arranged about the aperture in the carrier, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end communicating with the aperture through the carrier, each segment having passages leading outwardly toward the entrances from the center of the carrier, and means for directing metal poured in the center of the carrier into the passages for permitting air and gases in the mold cavities to escape through the risers.
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Description
Oct. 27, 1942.
. M. STOODY EI'AL 2,299,860
METHOD AND APPARATUS FOR CENTRIFUGALLY k CASTING CORROSION RESISTANT ALLOYS Filed March 17, 1942 4 Sheets-Sheet l.
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,sx/azzwfiamj iap/ulAaos, INVENTORS ATTOR/VEXZ Oct. 27, 1942.
s. M. s'rooDY ETAL 2,299,860 METHOD AND APPARATUS FOR CENTRIFUGALLY CASTING CORROSION RESISTANT ALLOYS I F'iled March I7, 1942 4 Sheets-Sheet 2 5,44PHLA50 2 6 2! 30 8 3 .40 2 INVENTORS ATTORNEYS s. M. STOODY ETAL ,299,860 METHOD AND APPARATUS FOR CENTRIFUGALLY CASTING CORROSION RESISTANT ALLOYS Filed March 1'7, 1942 4 Sheets-Sheet 3 Oct. 27, 1942.
I l 27 Z1 26 Q5 [a g5 5 Z1 Z7 {yam/M57000 7 Ram/12,4505, v .7 INVENTORS 4 in llllll m BYJ l WM Oct. 27, 1942. s, M. STOODY ETAL 2,299,350
METHOD AND APPARATUS FOR GENTRIFUGALLY CASTING CORROSION RESISTANT ALLOYS Filed March l'h 1942 4 Sheets-Sheet 4 Sana M 5/7001;
14LP//L.A505, I a i INVENTORS Arroz/m'rs.
. and to provide adequate mately 1200 "Patented Oct; 27, 1942 UNITED STATES PATENT OFFICE 2,299,860
METHOD AND APPARATUS FOR CENTRIFU- GALLY CASTING CORROSION RESISTANT ALLOYS Shelley M. Stootly CaliL, assignors as Ralph 1,. Abos, Whittier, to Stoody Company, Whittier,
Calif., a corporation of California Application March 17, 1942', Serial No. 435,005 (or. v2245) 11 Claims.
This invention relates to a method and apparatus for making precision castings centrifugally of high melting point corrosion resistant alloys.
-An object of the invention is to provide anew method and mold for making a multiplicity of castings centrifugally of relatively high melting point corrosion resistant alloys so that the castings will be so accurately formed that they will be identical requiring a minimum amount of machining or finishing operations.
Another object of the invention is to provide a method and apparatus for centrifugally casting metals and like substances wherein adequate provision is made to insure that only firm, clean, dense metal will be introduced into the mold cavity during the centrifugal casting operation, vents and reservoirs for the mold cavity so that pipes that may form as the metal cools will not continue or extendinto the metal of the casting.
While the invention may be employed wherever a multiplicity of identical and'accurately formed castings is desired, it has been primarily designed for the production of the turbine blades of a molten metal adjacent supercharger used on aircraft. In such a construction the supercharger is driven by a turbine,
the blades of which are of the aircraft engine. operation are driven by gine at a rotary speed subjected to the exhaust These turbines when in the exhaust of the enof approximately 20,000
exhaust gases which are not infrequently still flaming, are heated to a temperature of approxi- F. They consequently, must be resistant to the burning action of the exhaust gases and should be capable of sustaining a tensile stress of approximate1y70,000 pounds per square inch.
Metals that are resistant to corrosion or the burning action of the exhaust gases from the engine and which possess this high tensile streng h under high temperatureare inherently hard and'of a relatively high melting point, being poured usually at a temperature of approximately 3000 F. Because of their inherent hardness they are extremely difficult to machine. Consequently, it is of great importance to be able to accurately cast the turbine blades with such precision thatwthe finish machine operations are reduced to a minimum. In other words, "it is desired to reduce the machining operations to a mere cutting of-the casting from its riser and the gates or entrances to the mold cavity, As
speed and are subjected to high centrifugal forces it is manifest that the blades must be as nearly identical as possible for if the blades are not uniform the turbine will be unbalanced and the lack of balance becomes a materially destructive force.llnder the high rotary speed. Inasmuch as the blades are formed of a metal that is inherently hard in order to secure corrosion resistance, it is difiicult to machine the blades in accompanying drawings for an illustrative embodiment of the invention, wherein:
Figure 1 is a perspective view of a diecast pattern that is employed to make and shape the mold cavity in the mold that forms a part of the apparatus embodying the present invention;
Fig. 2 is a sectional view of a flask illustrating the pattern shown in Fig. l as positioned therein 1 and illustrating the mold as having been reamed R.P. M. The blades being subjected to the direct tions of the mold that up or tamped up in the flask about the pattern;
g. 3 is a top plan view of the mold illustrated as having been formed in Fig. 2 and illustrating in phantom lines the portions of the mold that are removed to produce one segment of the complete centrifugal mold;
Fig. 4 is a view in side elevation of thesegment produced illustrating in phantom lines the porhave been removed to produce the finished segment;
Fig. 5 is a view in side elevation of the segment illustrating in phantom that have been removed;
Fig. 6 is a perspective view of the finished segment that forms a part of the complete centrif ugal mold;
Fig. 7 is atop plan View of the completed centrifugal mold, parts being broken away and shown in horizontal section, the mold being made up of a plurality of segments of the character illustrated in Fig. 6;
Fig.8 is a vertical section through the mold taken substantially upon the line 8-8 upon Fig. 7; v Fig. 9 is a diametrical section through the completed mold;
the blades of the turbine are rotated at high 55 Fig. 10 is a partial view in plan illustrating a portion of the casting produced prior to its being divided into the individual turbine blades;
lines portions of the mold Fig. 11 is a secti nal view through the portion of the casting illustrated in Fig. 10:
Figs. 12, 13, and 14 are views of the casting produced, Fig. 12 being a view in side elevation of one side of the turbine blade; Fig. 13 an end elevation of the same; and Fig. 14 a view in side .elevation of the reverse side of the blade;
Fig. 15 is a sectional view similar to Fig. 8, but illustrating a slightly modified form of construction whereby a much greater multiplicity of castings may be produced from a single pour;
Fig. 16 is a view similar to Fig. 15, the section however having been taken through the mold on a plane between adjacent segments whereas Fig.
' 15 is a section taken through the mold cavities in superposed segments;
Fig. 17 is a view similar to Fig. 11 illustrating a portion of the casting produced from the mold illustrated in Figs. 15 and 16.
Referring to the accompanying drawings wherein similar reference characters designate similar parts throughout, and referring particularly to Figs. 12, 13, and 14, there is illustrated in these figures the nature of the finished casting that it is desired to produce for the blades of the turbine of the supercharger. With this construction in mind, although it will be appreciated that the invention is in no way restricted thereto but is applicable to all shapes of castings, a die- At the bottom of the pattern there is an enlargement I 3 terminating in a cylindrical stud M. This enlargement is designed to mold or shape the riser or outlet from the mold cavity in the mold that is produced. The pattern is preferably diecast so that in making a multiplicity of patterns it is relatively easy to make the patterns identical. The metal used for making the pattern is preferably tin as this metal has the required melting point to enable the mold to be properly baked and on baking to be ultimately melted out.
The pattern illustrated in Fig. 1 is positioned in a suitable flask l which is normally cylindrical in form and which is formed of carbon. In the bottom I 6 of the flash there is formed an aperture I! that snugly receives the stud l4. Grooves l8 are formed at diametrically opposite sides of the flask adjacent the top thereof to receive portions of the enlargements I0 and II at the sides of the pattern. Thus, with the stud l4 fitting in the aperture l1 and the enlargements l l and l2fitting in the grooves l8 in the flask the pattern is properly and accurately positioned within the flask. A molding composition I9 is then rammed or tamped up about the pattern within the flask. This molding composition has certain definite requirements in order to produce the desired results. As the metal that is to be poured has a relatively high melting point and is normally poured at a temperature of approximately 3000 F. it is manifest that the mold-must resist burning or melting. Also, it cannot be so extremely hard that as the casting cools and As a result of a great deal of experimentation we have ascertained that a molding composition composed of the following ingredients in approximately the following proportions gives very satisfactory results.
Graphitic carbon, 200 mesh and finer "pounds" 9 Fire clay do Glucose do 1 /2 Water ounces 4 Such a mixture is prepared by mulling together the graphitic carbon and fire clay while dry for approximately five minutes. The glucose and Water are warmed to about F. and added thereto and the ingredients thoroughly mixed. The resulting mixture is damp and will hold together on squeezing. We find that it is very suitable for making a mold for casting such metals as that sold under the trade-name of Silfram consisting of chromium approximately 33%, nickel approximately 10%, silicon approximately 2%, and the balance iron; Vitalium, an alloycomposed of approximately 65% cobalt, 30% chromium, and 5% molybdenum, or that Stellite' that is composed of approximately 65% cobalt, 26% chromium, 5%% tungsten, 1% iron,
1% silicon, and 1% carbon.
The molding composition is tamped up rather firmly about the pattern and when the flask is thus filled it is placed in an oven and baked. It is usually advisable to bake the flask and mold therein contained for a considerable length of time at approximately 150 F. to drive out the moisture without creating voids in the mold. The temperature can then be raised to approximately 300 to 400 F. to thoroughly bake the mold and finally its temperature is raised to .approximately 585 F. During this latter treatment the tin pattern melts out of the mold leaving themold cavity 20 formed in the mold equipped with lateral entrances 2| adjacent its outer end and a riser 22 extending inwardly from its inner end.
A very satisfactory procedure in baking the molds has been to heat the molds for the following periods at the following temperatures in consecutive order:
7 hours at 150 F.;
hour at F.;
A hour at 225 F.;
hour at 275 F.;
3 hours at 300 F.;
1 hour at 400 F.;
2 hours at 470 F.; and 1 hour at 585 F.
While it is not necessary to precisely follow this procedure it is important to have the mold thoroughly cured and entirely shrunk about the pattern before the tin pattern melts out. When the mold is thus produced the flask may be broken away leaving the cylindrical mold illustrated in phantom lines in Figs. 4 and 5, and in full lines in Fig. 3. Those portions between the full lines and the phantom lines on Figs.3, 4, and 5 are then removed, such as by mounting the mold on a suitable jig and grinding away the excess mold material, forming a segmental shaped mold as illustrated in Fig. 4 having a fiat top and bottom as shown in Fig. 5. The beveled surfaces 23 at the upper outer corners of the segment are portions of the original cylindrical surface on the exterior of the mold that are not removed in extends inwardly a short distance over'the top ments. It will be noted that the cylindrical porwill of course be understood that the metal in site the inner end ofthe riser 22 and above this cut away portion there is a shoulder ZLha-ving a beveled under surface 25. Grooves "are then' routed down the outward 1y divergent sides of the 1 5 mold segment to a point indicated at :1 beyond the'entrances 2| to the moldcavity.
' When a plurality. of thesemold segments are made they are posltioned'in side-by-side relationship on a suitable carrier 28, see Figs. 7 and 8. This carrier has a central aperture 29 formed therethrough andradial grooves 30 on its under suri'ace.' A carbon ring 3! is positioned on the bottom of the carrier and preferably of the aperture 29. The segments fit together within an outer upstanding flange 32 around a hollow carbon cone 33 having a vertical or cylindrlcal lower portion 34. On top of the segments there is positioned a carbon plate 35 having a conical gate 36 formed therein. The-bottom of the cone immediately above the cylindrical portion 34 fits against the beveled surface beneath the shoulder 24 so that the top surface of the cone 33 together with the inner wall of the gate cooperate to direct the metal that is poured through the radial passages 31 that are formed by opposed grooves26 on adjacent segtion at the bottom of the cone 33 has apertures or passages '38 formed therein which register with the inner ends of the risers 22 on the mold segments so that egress from the mold cavity of gases and air is readily permitted through the risers 22 and the passages '38, the aperture 29 and the radial grooves 30. The carrier 28- and the mold parts that are thus assembled are then positioned on a suitable rotary table or other rotating device, the axis of rotation of which is coincident with the vertical axis through the cone 33 and through the gate 36.
' The metal that is to be poured may be one of the specific metals above mentioned and is. normally poured at. a temperature of approximately 3000 while the mold is being rotated at a fair rotational speed, such as 1500 R. P. M.
The metal that is poured into the central gate encounters the cone 33 and is distributed and thrown outwardly through the radial passages 31 formed by the grooves 36. The initial metal that enters these passages is apt to become somewhat'chilled and it may beoxidized and if there is any dirt present in the passages it is apt to pick up this dirt. This initial metal is consequently carried outwardly to the extreme outer end 21 of the passage and being received in this recess or pocket, remains there. When the pocket is filled succeeding metal flows laterally into the entrances 2| at the sides of the adjacent segments filling the mold cavity and entering the riser 22. -Usually:asufllcientamount of metal is poured to, completely fill the riser which should have a volume nearly equal to the volume of the casting under ordinary circumstances. It
the passages 31 andin the risers 22 is constantly being subjected to centrifugal action, the metal in the riser being urged outwardly toward the.
mold cavity and the metal in the passages 37 being urged outwardly toward the entrances 2|. Consequently, the metal in the mold cavity is subjected to pressure from the metal in the passages 31 and the metal in the risers, both being urged outwardly with the result that the casting produced is normally clean, free of oxideaand however, to double the number 0 very dense. Any gases or air that is in the mold cavity and in the riser prior to the filling or the mold cavity is readily expelled by the metal through the riser, the passages 38, aperture 28, and gr0oves 3ll so.l5hat,,thel:e will norm y be an entire absence of any blow holes'.Metals ofthe above described characteristics are apt to pipe somewhat badly. However, with sufllclent length of risers .22 and the long passages 31 those pipes that do form are formed inwaste metal that is ultimately cut off to form the finished casting and this metal can of course be reheated and repoured.
When the metal cools a duced, aportion of which 10 and 11 consisting of th ing in the passages 31, therisers, and the castings themselves. The castings may then be out free by cutting on the phantom lines indicated in Fig. 10, thus obtaining the; finished article illustrated in Figs. 12, 13, and 14. The cutting single casting is pro is illustrated in Figs. e metal left remainmay be accomplished with any high speed cutting mechanism used for cutting hard metals of this character. It will be found that if the molding composition .is properly prepared and is 1 also be identical in weight, shape, and size, havingno voids or blow holes andbeing substantially free of oxides and dirt. .There will also be an absence of any shrinkage cracks due to the mold resisting the shrinkage of the metal as it cools. v
In Figs. 1 to 9, inclusive, the moldis illustrated as being made up of segments arranged in a,
single layer-on the carrier 28. It is possible,
f castings produced per pouring operation, as illustrated in Figs. 15 to '17, inclusive. In this form of construction of the mold the mold is produced in the flask in the same manner as above described.
Those segments 40 that form the lower layer do not have their inner ends. in Figs. 5 and 6 but exte distance so as to shaped as illustrated nd inwardly the full provide a support for the bot tom of the cone 33. These lower segments also do not havethe grooves ZB routed in their sides. When these segments are arranged'to form a lower layer on the carrier 28 an upper row of segments '42 is positioned thereon 'in vertical alignment. These segments 42, however, are of the same size and shape as that previously described and illustrated in Fig. 6. It will be noted from an inspection of Fig. 6 that there is a small web 43 at the bottom of each entrance 2| These webs of course will be present in the top of each of the lower mold segments 40. The webs 43 of the upper and lower segments are broken out so that metal may flow from the passages 31 produced by the grooves 36 not only into the entrances 2| of the upper mold segments but may also flow downwardly to the entrances to the lower mold segments. In using this .form o f. construction the advantages are substantially the same as above described in that the initial metal is first thrown out to the extreme ends of the radial passages 31 and this metal. which may have been chilled, oxidized, or may have picked up dirt, is
pocketedat the outer ends of the passages. The succeeding metal enters the mold cavities of the upper and lower segments filling the mold cavities and expelling-the air andgases therefrom,
finally filling or substantially filling the risers.
entrapped or Thus, by employing upper and lower rows of a continuation-in-part of our copending application Serial No. 424,370, filed December 24, 1941. The molding composition herein disclosed is not herein claimed but is claimed in our copending application filed collaterally herewith entitled Molding composition.
Various changes may be made in the details of construction without departing from the spirit or scope of the invention as defined by the appended claims.
We claim:
1. The method of centrifugally casting metal which includes throwing metal outwardly from a central gate towards the pocket by centrifugal action so that the initial metal poured remains in the pocket, causing succeeding metal to flow laterally into one or more mold cavities and while under centrifugal pressure to fill the mold cavities towards risers arranged inwardly with respect to the mold cavity.
2. A mold for centrifugally casting having a mold cavity, the entrance to the cavity being adjacent its outer end and the riser for the mold being adjacent its inner end, there being a passage for molten metal leading from adjacent the center of rotation of the mold to a point beyond the entrance to the mold cavity to form a pocket into which the initial metal poured may flow and be trapped.
3. A mold for centrifugally casting having a mold cavity arranged off center with respect to the axis of rotation of the mold, said cavity having entrances at each side adjacent its outer end, and a riser adjacent its inner end, there being passages at each side of the mold cavity leading from adjacent the axis of rotationof the mold toward the entrances.
4. A mold for centrifugally casting having a mold cavity arranged ofl center with respect to the axis of rotation of the mold, said cavity having entrances at each side adjacent its outer end, and a riser adjacent its inner end, there being passages at each side of the mold cavity leading from adjacent the axis of rotation of the mold to points beyond the entrances to the cavity so as to provide pockets for receiving and retaining the initial metal poured.
5. A mold for centrifugally casting made up of segments arranged around a central gate, each segment having a mold cavity formed therein having an entrance adjacent its outer end and a riser adjacent its inner end, there being passages formed between the segments leading from the gate toward the entrances.
6. A mold for centrifugally casting made up of segments arranged around a central gate, each segment having a mold cavity formed therein having an entrance adjacent its outer end and a riser adjacent its inner end, there being passages formed between the segments leading from thegate to points beyond the entrancesto provide pockets that receive and retain the initial metal poured.v
7. A'mold for centrifugally casting comprising a plurality of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end, each segment having passages leading outwardly toward the entrances from the gate, a cone providing the bottom of the gate for directing metal poured into the gate into said passages, said cone being passaged to provide outlets from the risers.
8. A mold for centrifugally casting comprising a plurality of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end, each segment having passages formed on its sides leading outwardly to points beyond the entrances from the gate, a cone providing a bottom for the gate for directing metal poured into the gate into the passages, said cone being passaged to provide outlets from the risers.
9. A mold for centrifugally casting comprising upper and lower layers of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end, each mold cavity having a riser adjacent its inner end, the segments of the upper layer having passages leading outwardly toward the entrances from the gate, and a cone providing the bottom for the gate for directing metal poured into the I gate into said passages.
10. A mold for centrifugally casting comprising upper and lower layers of segments arranged about a central gate, each segment having a mold cavity formed therein having one or more entrances adjacent .its outer end, each mold cavity having a riser adjacent its inner end, the segments of the upper layer having passages leading outwardly toward the entrances from the gate, and a cone providing the bottom for the gate for directing metal poured into the gate into said pasages, said cone being passaged to provide outlets from at least some of the risers.
11. A mold for centrifugally casting comprising a carrier having a central aperture therethrough, grooves on the underside of the carrier, a plurality of segments arranged about the aperture in the carrier, each segment having a mold cavity formed therein having one or more entrances adjacent its outer end and a riser adjacent its inner end communicating with the aperture through the carrier, each segment having passages leading outwardly toward the entrances from the center of the carrier, and means for directing metal poured in the center of the carrier into the passages for permitting air and gases in the mold cavities to escape through the risers.
SHELLEY M. STOODY. RALPH L. ABOS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US435005A US2299860A (en) | 1942-03-17 | 1942-03-17 | Method and apparatus for centrifugally casting corrosion resistant alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US435005A US2299860A (en) | 1942-03-17 | 1942-03-17 | Method and apparatus for centrifugally casting corrosion resistant alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2299860A true US2299860A (en) | 1942-10-27 |
Family
ID=23726604
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US435005A Expired - Lifetime US2299860A (en) | 1942-03-17 | 1942-03-17 | Method and apparatus for centrifugally casting corrosion resistant alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2299860A (en) |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2419716A (en) * | 1945-09-13 | 1947-04-29 | Indiana Steel Products Co | Mold assembly for centrifugal casting |
| US2469907A (en) * | 1946-08-22 | 1949-05-10 | Whitehead Bros Co | Mold composition |
| US2479039A (en) * | 1944-11-06 | 1949-08-16 | United Aircraft Corp | Cast disk for turbine rotors |
| US2506216A (en) * | 1946-12-24 | 1950-05-02 | Albert B Hemstreet | Self-locking centrifugal mold |
| US2530853A (en) * | 1945-06-07 | 1950-11-21 | Joseph B Brennan | Method of casting |
| US2586814A (en) * | 1949-05-18 | 1952-02-26 | Jr Herbert Greenewald | Mold composition for precision casting and method of forming mold |
| US2766498A (en) * | 1951-09-21 | 1956-10-16 | James C Heintz Company | Use of plaster of paris forms in making metal castings |
| US2819501A (en) * | 1950-10-13 | 1958-01-14 | Griffin Wheel Co | Wheel mold |
| US2855295A (en) * | 1956-12-26 | 1958-10-07 | Gen Electric | Cobalt base hard surfacing alloy |
| US2870497A (en) * | 1956-08-13 | 1959-01-27 | Strauss | Casting metals and alloys |
| US4087996A (en) * | 1976-12-13 | 1978-05-09 | General Electric Company | Method and apparatus for correcting distortion in gas turbine engine blades |
| WO2002040727A3 (en) * | 2000-11-14 | 2003-11-27 | California Inst Of Techn | Centrifugal apparatus for processing molten metal alloys |
| US9481029B2 (en) | 2013-03-14 | 2016-11-01 | Hitchiner Manufacturing Co., Inc. | Method of making a radial pattern assembly |
| US9486852B2 (en) | 2013-03-14 | 2016-11-08 | Hitchiner Manufacturing Co., Inc. | Radial pattern assembly |
| US9498819B2 (en) | 2013-03-14 | 2016-11-22 | Hitchiner Manufacturing Co., Inc. | Refractory mold and method of making |
| FR3145299A1 (en) * | 2023-01-27 | 2024-08-02 | Safran Aircraft Engines | Foundry mold |
-
1942
- 1942-03-17 US US435005A patent/US2299860A/en not_active Expired - Lifetime
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2479039A (en) * | 1944-11-06 | 1949-08-16 | United Aircraft Corp | Cast disk for turbine rotors |
| US2530853A (en) * | 1945-06-07 | 1950-11-21 | Joseph B Brennan | Method of casting |
| US2419716A (en) * | 1945-09-13 | 1947-04-29 | Indiana Steel Products Co | Mold assembly for centrifugal casting |
| US2469907A (en) * | 1946-08-22 | 1949-05-10 | Whitehead Bros Co | Mold composition |
| US2506216A (en) * | 1946-12-24 | 1950-05-02 | Albert B Hemstreet | Self-locking centrifugal mold |
| US2586814A (en) * | 1949-05-18 | 1952-02-26 | Jr Herbert Greenewald | Mold composition for precision casting and method of forming mold |
| US2819501A (en) * | 1950-10-13 | 1958-01-14 | Griffin Wheel Co | Wheel mold |
| US2766498A (en) * | 1951-09-21 | 1956-10-16 | James C Heintz Company | Use of plaster of paris forms in making metal castings |
| US2870497A (en) * | 1956-08-13 | 1959-01-27 | Strauss | Casting metals and alloys |
| US2855295A (en) * | 1956-12-26 | 1958-10-07 | Gen Electric | Cobalt base hard surfacing alloy |
| US4087996A (en) * | 1976-12-13 | 1978-05-09 | General Electric Company | Method and apparatus for correcting distortion in gas turbine engine blades |
| FR2373359A1 (en) * | 1976-12-13 | 1978-07-07 | Gen Electric | PROCESS AND MACHINE FOR THE SHAPING BY CENTRIFUGAL EFFECT OF METAL PARTS SUCH AS TURBINE FINS |
| WO2002040727A3 (en) * | 2000-11-14 | 2003-11-27 | California Inst Of Techn | Centrifugal apparatus for processing molten metal alloys |
| US9481029B2 (en) | 2013-03-14 | 2016-11-01 | Hitchiner Manufacturing Co., Inc. | Method of making a radial pattern assembly |
| US9486852B2 (en) | 2013-03-14 | 2016-11-08 | Hitchiner Manufacturing Co., Inc. | Radial pattern assembly |
| US9498819B2 (en) | 2013-03-14 | 2016-11-22 | Hitchiner Manufacturing Co., Inc. | Refractory mold and method of making |
| USRE48971E1 (en) | 2013-03-14 | 2022-03-15 | Hitchiner Manufacturing Co., Inc. | Refractory mold and method of making |
| USRE49063E1 (en) | 2013-03-14 | 2022-05-10 | Hitchiner Manufacturing Co., Inc. | Radial pattern assembly |
| FR3145299A1 (en) * | 2023-01-27 | 2024-08-02 | Safran Aircraft Engines | Foundry mold |
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