US2995479A - Degassing aluminum articles - Google Patents
Degassing aluminum articles Download PDFInfo
- Publication number
- US2995479A US2995479A US2995479DA US2995479A US 2995479 A US2995479 A US 2995479A US 2995479D A US2995479D A US 2995479DA US 2995479 A US2995479 A US 2995479A
- Authority
- US
- United States
- Prior art keywords
- gas
- article
- aluminum
- metal
- coating
- 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
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 41
- 229910052782 aluminium Inorganic materials 0.000 title claims description 40
- 238000007872 degassing Methods 0.000 title description 11
- 238000000576 coating method Methods 0.000 claims description 30
- 239000011248 coating agent Substances 0.000 claims description 26
- 238000010438 heat treatment Methods 0.000 claims description 19
- 238000000034 method Methods 0.000 claims description 18
- 229910017052 cobalt Inorganic materials 0.000 claims description 10
- 239000010941 cobalt Substances 0.000 claims description 10
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 10
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 9
- 229910052750 molybdenum Inorganic materials 0.000 claims description 9
- 239000011733 molybdenum Substances 0.000 claims description 9
- 230000004927 fusion Effects 0.000 claims description 6
- 229910052741 iridium Inorganic materials 0.000 claims description 6
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 claims description 6
- 229910052703 rhodium Inorganic materials 0.000 claims description 6
- 239000010948 rhodium Substances 0.000 claims description 6
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 claims description 6
- -1 PALADIUM Chemical compound 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 description 44
- 239000002184 metal Substances 0.000 description 44
- 239000007789 gas Substances 0.000 description 43
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 18
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 11
- 239000001257 hydrogen Substances 0.000 description 9
- 229910052739 hydrogen Inorganic materials 0.000 description 9
- 229910052763 palladium Inorganic materials 0.000 description 9
- 238000005242 forging Methods 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000000605 extraction Methods 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 230000035876 healing Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 239000011800 void material Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- XFBXDGLHUSUNMG-UHFFFAOYSA-N alumane;hydrate Chemical compound O.[AlH3] XFBXDGLHUSUNMG-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000007772 electroless plating Methods 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000009497 press forging Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
Definitions
- This invention relates to a method for the extraction of gas and the elimination of voids and flakes in wrought aluminum and aluminum base alloy articles.
- aluminum will be used herein to encompass aluminum and aluminum base alloys which contain at least 50 percent by weight of aluminum.
- Finished and semi-finished aluminum articles occasionally contain occluded gas, principally hydrogen, WhlCll may give rise to objectionable discontinurtres 1n the metal structure.
- Some of the hydrogen is usually considered to be in solution in the solid metal, i.e. it is in the monatomic state, although pockets or voids filled with molecular hydrogen have also been observed.
- some thermal treatments are generally employed to aid in working the metal or to develop the desired strength, and it is considered that such heating also produces diflusion of the monatomic hydrogen to any voids or discontinuities within the metal whereat association into molecular form takes place.
- the problem of so-called flakes within the internal metal structure has been'treated to these hydrogen-filled voids.
- an aluminum article having a low gas content, or substantially none can be produced by a method in which the aluminum body containing gas and voids is coated with at least one metal selected from the group consisting of cobalt, molybdenum, palladium, rhodium and iridium, and is heated in a gaseous atmosphere at a temperature above 750 F. but below that at which any substantial amount of fusion occurs for a length of time sufiicient to difiuse occluded gas' into the atmosphere surrounding the article.
- the metal article may be thereafter worked to plastically deform the metal article.
- the metal coating is also highly beneficial in preventing o -'dation and blistering of the aluminum during subsequent heating operations.
- the heating step must be conducted under conditions which facilitate gas removal. It has been found that this can be accomplished by initially coating the article with cobalt, moylbdenum, palladium, rhodium or iridium or a combination of these metals, to form a film on the metal surface which reduces greatly, if it does not altogether eliminate the existence of monatomic hydrogen at the metal surface, as well as tending to inhibit oxidation of the aluminum.
- the nature of the mechanism by which the gas is driven out of the aluminum article is not fully understood; however, it seems to involve an irreversible conversion of monatomic hydrogen into molecular hydrogen.
- the degassing or prolonged heating step may be carried out in a normal atmosphere without danger of reabsorbing gas, thus removing one of the great economic handicaps to the use of long-time heating procedures to extract gas from aluminum articles.
- the surface of an aluminum article Prior to coating the surface of an aluminum article with one or more of the metals named above, the surface of the article should be treated to remove any oxide film.
- the metallic coatings may be deposited on the surface in any convenient manner. Electra-plating and electro-less plating techniques have been highly successful, as have been metallic spray coatings. The thickness of the coating is not critical, and apparently it need not be continuous but it should be relatively thin, such as normally produced by plating or spraying procedures. For example, coatings of less than 0.1 mil have been satisfactory. Furthermore, a coating initially applied to plate has been found to protect it through the ensuingreduction steps to sheet.
- the electrolytic coatings may be applied directly or they may be applied over a base coating or strike of another metal, such as copper in accordance with conventional practice.
- the copper strike has no etfect on the treatment of the present invention.
- a multilayer coating of one or more metals may be employed or the layer may consist of an alloy of two or more of the metals as might be applied in spraying.
- the coating and degassing steps may be conducted at I any step of the working operation.
- Coatings applied to plate slabs have been found to provide protection throughout the rolling sequence and its various preheating operations. For this reason, it is often desirable to leave the protective metal coating on the aluminum article until after the final heat treatment.
- the coating may be removed by any convenient method. Generally, it is most convenient to strip the metal electrolytically in a sulfuric acid electrolyte.
- the article may be degassed in a conventional air atmosphere furnace. No drying of the air need be undertaken as moisture can be tolerated inthe gas extraction step, thus permitting employment of conventional industrial furnace atmospheres which generally contain 1.5 to 30 grains of water per cubic foot.
- Gases which are inert or nondeleterious to aluminum may be employed in place of air such as nitrogen, argon, helium and fuel gas, or such gases may be used in admixture with air.
- atmosphere includes air
- the duration of the heating step will be dependent upon the thickness of the article being treated (the shortest diflusing path), the desired final gas content of the metal and the temperature employed.
- the rate of diffusion increases almost exponentially with increase in temperature. Since commercial degassing of large quantities of aluminum articles required space-consuming heating equipment, it is desirable that the heating step be of as short duration as possible. Therefore, a temperature at least above 750 F., and generally above 900 F., should be used.
- the temperature is preferably below the temperature of incipient fusion, but temperatures above the melting point of one or more of the phases have been successfully employed where the amount is very small and eutectic melting has not been a concern.
- the articles should not be heated at temperatures which adversely aifect the properties of the metal.
- an article will be considered substantially degassed or gas-free if the gas has been substantially diffused out of the internal discontinuities to permit subsequent healing, although some may remain in solution in the metal. Generally, this will require removal of at least 75 percent or more of the occluded gas, although it may often be desirable to extract as much as 90 percent, or more.
- the length of time for degassing increases as the square of the half-thickness of the metal body. Therefore, in some cases, it may be desirable only to seek extraction of the gas from relatively thin crosssections of the articles where the strength characteristics are of primary concern rather than to degas the entire article which might require a much longer time.
- Tables I and H are a guide to the time theoretically necessary at several temperatures for removing various percentages of gas, as based on Fick's law and the diffusion constant for hydrogen in aluminum. These tables give a time factor per centimeter half-thickness (or radius) which may be converted to the ideal length of time necessary to degas a given thickness of metal by multiplying the factor by the square of the half-thickness of the metal body in centimeters.
- T time necessary for degassing article (in hours)
- t time factor for unit thickness (from table)
- d thickness (or diameter) of the article (in centimeters)
- TABLE I Time factor for sheet, plate, or rectangular cross-section, hrs/unit centimeter half-thickness
- Time factor for rod or bar hrs/unit centimeter radius Tam '0.
- Percent Removal p sso too am cm 1.0 .84 .005 .or 7.6 1.1 .47 .14 121 as .15 .24 is a1 .05 .st as as 1.5 .41
- the above time values can be converted to inches and in terms of the full thickness of the metal body by multiplying them by a factor of 1.613.
- 850 to 1000 F. (450 to 540' C.) is a temperature range conveniently employed.
- a rule of thumb figure has been to maintain aluminum forgings at temperature at least 16 and preferably 24 hours or more per inch of thickness for adequate gas removal.
- articles having a thickness of over several inches require shorter times but often require more than 24 hours per inch of thickness.
- at least about 4 hours and preferably six hours are used for a half-inch thickness.
- thinner sheet products degas very quickly, .091 inch thick sheet was degassed at 940 F. in only 1 minute.
- the rate may vary with the mode of fabrication or grain orientation or with the surface condition. For this reason and also for obtaining a more definite determination of the time necessary to degas a particular articles, the testing of samples is desirable for the establishment of conditions for the heating step. Similarly, the time necessary for degassing compressed aluminum powder products will vary with the conditions under which the compact was prepared.
- the article is subjected to a working operation for elfecting plastic deformation of the metal and to heal voids left by the difiused hydrogen.
- the various working methods may be employed singly or in combination to effect the welding of the voids.
- the term forging includes both hammer-forging and press-forging methods. The amount of working or percentage of reduction necessary will be dependent upon the nature of the article and the original content of voids. In some cases, especially in larger articles such as die forgings, a relatively small reduction may be sufiicient to heal or weld the discontinuities in the structure.
- the degassed and healed aluminum articles may then be subjected to further heat treatments. Because the voids or discontinuities within the metal structure no longer exist, the problem of gassing (or negassing) is minimized unless new discontinuities are subsequently created within the metal structure.
- gaseous occlusions is most pronounced of metals referred to above may be in the form of a casting, compressed powder product or wrought article. Conditions necessary to eflect degassing will, of course, be influenced by the structure of the article.
- Illustrating the efficacy of the present invention are the following examples in which aluminum articles were coated with some of the metals of the present invention and heated to extract occluded gas.
- EXAMPLE 3 The effect of a molybdenum coating upon the degassing of aluminum was determined by spraying panels of the same kind as referred to in the two preceding examples with metallic molybdenum in a conventional manner.
- the coating so produced had a thickness of about 5 mils.
- the coated panels along with bare ones were heated at 940 F. for 15 minutes in a normal air atmosphere, cooled to room temperature, and the molybdenum coating electrolytically stripped from the panels upon cooling to room temperature. Both groups of panels were subjected to the blister anneal test mentioned above.
- the coating so produced had a thickness of about 5 mils.
- the coated panels along with bare ones were heated at 940 F. for 15 minutes in a normal air atmosphere, cooled to room temperature, and the molybdenum coating electrolytically stripped from the panels upon cooling to room temperature. Both groups of panels were subjected to the blister anneal test mentioned above.
- the method of substantially reducing the gas content of aluminum articles comprising: coating the surface of an aluminum article containing gas with at least one metal selected from the group consisting of cobalt, molybdenum, paladium, rhodium and' iridium and thereafter heating said coated article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a length of time sufiicient to dilfuse occluded gas into the atmosphere around said article.
- the method of substantially reducing the gas content of aluminum articles comprising: coating the surface of an aluminum article containing gas with at least one metal selected from the group consisting of cobalt, m0- lybdenum, palladium; rhodium and iridium; heating said coated article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a'length of time sufficient to difiuse occluded gas into the atmosphere around said article and thereafter stripping said coating from said article.
- the method substantially reducing the gas content and voids in aluminum articles comprising: coating an aluminum article containing gas and voids with at least one metal selected from the group consisting of cobalt, molybdenum, palladium, rhodium and iridium; heating said article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a length of time sufiicient to diffuse occluded gas into the atmosphere around said article; and thereafter working said article to heal any voids therein.
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Description
United States Patent e ce Patented Aug. 8, 1961 This invention relates to a method for the extraction of gas and the elimination of voids and flakes in wrought aluminum and aluminum base alloy articles.
The term aluminum will be used herein to encompass aluminum and aluminum base alloys which contain at least 50 percent by weight of aluminum.
Finished and semi-finished aluminum articles occasionally contain occluded gas, principally hydrogen, WhlCll may give rise to objectionable discontinurtres 1n the metal structure. Some of the hydrogen is usually considered to be in solution in the solid metal, i.e. it is in the monatomic state, although pockets or voids filled with molecular hydrogen have also been observed. In the fabrication of wrought articles from the ingot, some thermal treatments are generally employed to aid in working the metal or to develop the desired strength, and it is considered that such heating also produces diflusion of the monatomic hydrogen to any voids or discontinuities within the metal whereat association into molecular form takes place. The problem of so-called flakes within the internal metal structure has been'treated to these hydrogen-filled voids.
Because of the gas pressures developed by the molecular gas, subsequent working of the metal does not effect a healing of the void or discontinuity, and heating of the article at elevated temperatures may increase such pressures to the point where the metal suffers local plastic deformation.
The problem of occluded gas has become increasingly important with the growing requirements for high strength aluminum articles. Any gas-filled void may not only constitute an area of weakness in the final article, but may give rise to flakes, blisters, slivers and other defects which result in rejection. These problems have prompted investigations to find a method for the elimination of occluded gas and voids associated therewith.
It has heretofore been proposed that hydrogen gas contained in aluminum articles may be driven out of the metal by heating under a vacuum at temperatures on the order of 500-1000 -F. Commercial utilization of this procedure has not proven feasible and attempts to remove gas in an undried air atmosphere have been unsuccessful. Also, it has been suspected that the degassed articles are prone to again absorb gas.
Recent investigations have indicated that one of the prime factors in the failure to degas aluminum articles heated in an air atmosphere furnace has been the existence of relatively high monatomic hydrogen partial pressures at the surface of the aluminum article, which may be the result of oxidation of the aluminum by small amounts of moisture in the furnace atmosphere at the temperature of treatment. The aluminum-water vapor reaction becomes pronounced at temperatures above 650 F, and especially above about 750 F.
It has now been discovered that an aluminum article having a low gas content, or substantially none, can be produced by a method in which the aluminum body containing gas and voids is coated with at least one metal selected from the group consisting of cobalt, molybdenum, palladium, rhodium and iridium, and is heated in a gaseous atmosphere at a temperature above 750 F. but below that at which any substantial amount of fusion occurs for a length of time sufiicient to difiuse occluded gas' into the atmosphere surrounding the article. The metal article may be thereafter worked to plastically deform the metal article. The metal coating is also highly beneficial in preventing o -'dation and blistering of the aluminum during subsequent heating operations.
To bring about the extraction of gas from the aluminum article, the heating step must be conducted under conditions which facilitate gas removal. It has been found that this can be accomplished by initially coating the article with cobalt, moylbdenum, palladium, rhodium or iridium or a combination of these metals, to form a film on the metal surface which reduces greatly, if it does not altogether eliminate the existence of monatomic hydrogen at the metal surface, as well as tending to inhibit oxidation of the aluminum. The nature of the mechanism by which the gas is driven out of the aluminum article is not fully understood; however, it seems to involve an irreversible conversion of monatomic hydrogen into molecular hydrogen. By employing the metal film on the article, the degassing or prolonged heating step may be carried out in a normal atmosphere without danger of reabsorbing gas, thus removing one of the great economic handicaps to the use of long-time heating procedures to extract gas from aluminum articles.
Prior to coating the surface of an aluminum article with one or more of the metals named above, the surface of the article should be treated to remove any oxide film.
- This may be conveniently accomplished by dipping or otherwise applying a l aqueous solution of hydrofluoric acid to the article. Other suitable solutions can be used, of course. The metallic coatings may be deposited on the surface in any convenient manner. Electra-plating and electro-less plating techniques have been highly successful, as have been metallic spray coatings. The thickness of the coating is not critical, and apparently it need not be continuous but it should be relatively thin, such as normally produced by plating or spraying procedures. For example, coatings of less than 0.1 mil have been satisfactory. Furthermore, a coating initially applied to plate has been found to protect it through the ensuingreduction steps to sheet.
The electrolytic coatings may be applied directly or they may be applied over a base coating or strike of another metal, such as copper in accordance with conventional practice. The copper strike has no etfect on the treatment of the present invention. If desired, a multilayer coating of one or more metals may be employed or the layer may consist of an alloy of two or more of the metals as might be applied in spraying.
The coating and degassing steps may be conducted at I any step of the working operation. Coatings applied to plate slabs have been found to provide protection throughout the rolling sequence and its various preheating operations. For this reason, it is often desirable to leave the protective metal coating on the aluminum article until after the final heat treatment.
The coating may be removed by any convenient method. Generally, it is most convenient to strip the metal electrolytically in a sulfuric acid electrolyte.
After the metal coating has been applied, the article may be degassed in a conventional air atmosphere furnace. No drying of the air need be undertaken as moisture can be tolerated inthe gas extraction step, thus permitting employment of conventional industrial furnace atmospheres which generally contain 1.5 to 30 grains of water per cubic foot. Gases which are inert or nondeleterious to aluminum may be employed in place of air such as nitrogen, argon, helium and fuel gas, or such gases may be used in admixture with air.
The term atmosphere, as used herein, includes air,
v moisture associated with air and other gases.
The duration of the heating step will be dependent upon the thickness of the article being treated (the shortest diflusing path), the desired final gas content of the metal and the temperature employed. The rate of diffusion increases almost exponentially with increase in temperature. Since commercial degassing of large quantities of aluminum articles required space-consuming heating equipment, it is desirable that the heating step be of as short duration as possible. Therefore, a temperature at least above 750 F., and generally above 900 F., should be used. The temperature is preferably below the temperature of incipient fusion, but temperatures above the melting point of one or more of the phases have been successfully employed where the amount is very small and eutectic melting has not been a concern. However, the articles should not be heated at temperatures which adversely aifect the properties of the metal. When the gas-containing metal is heated in this manner, the major portion of the gas is driven ofi within a reasonably short time, a proportionately longer time being required to remove the last few percent of gas. For purposes of this application, an article will be considered substantially degassed or gas-free if the gas has been substantially diffused out of the internal discontinuities to permit subsequent healing, although some may remain in solution in the metal. Generally, this will require removal of at least 75 percent or more of the occluded gas, although it may often be desirable to extract as much as 90 percent, or more.
Theoretically, the length of time for degassing increases as the square of the half-thickness of the metal body. Therefore, in some cases, it may be desirable only to seek extraction of the gas from relatively thin crosssections of the articles where the strength characteristics are of primary concern rather than to degas the entire article which might require a much longer time.
Indicative of the variables governing the difiusion step, Tables I and H are a guide to the time theoretically necessary at several temperatures for removing various percentages of gas, as based on Fick's law and the diffusion constant for hydrogen in aluminum. These tables give a time factor per centimeter half-thickness (or radius) which may be converted to the ideal length of time necessary to degas a given thickness of metal by multiplying the factor by the square of the half-thickness of the metal body in centimeters.
where:
T=time necessary for degassing article (in hours) t=time factor for unit thickness (from table) d=thickness (or diameter) of the article (in centimeters) TABLE I Time factor for sheet, plate, or rectangular cross-section, hrs/unit centimeter half-thickness TABLE II Time factor for rod or bar, hrs/unit centimeter radius Tam '0. Percent Removal p sso too am cm 1.0 .84 .005 .or 7.6 1.1 .47 .14 121 as .15 .24 is a1 .05 .st as as 1.5 .41
The above time values can be converted to inches and in terms of the full thickness of the metal body by multiplying them by a factor of 1.613.
For most aluminum articles, 850 to 1000 F. (450 to 540' C.) is a temperature range conveniently employed. In practicing the invention at a temperature of 940 F. (505 0.), since commercial conditions are far from ideal, a rule of thumb figure has been to maintain aluminum forgings at temperature at least 16 and preferably 24 hours or more per inch of thickness for adequate gas removal. However, occasionally articles having a thickness of over several inches require shorter times but often require more than 24 hours per inch of thickness. In the treatment of rolled articles at the same temperature, at least about 4 hours and preferably six hours are used for a half-inch thickness. However, thinner sheet products degas very quickly, .091 inch thick sheet was degassed at 940 F. in only 1 minute. Because of the difiicultly in removing gas from some articles, it is conceivable that the rate may vary with the mode of fabrication or grain orientation or with the surface condition. For this reason and also for obtaining a more definite determination of the time necessary to degas a particular articles, the testing of samples is desirable for the establishment of conditions for the heating step. Similarly, the time necessary for degassing compressed aluminum powder products will vary with the conditions under which the compact was prepared.
Subsequent to the heating step, the article is subjected to a working operation for elfecting plastic deformation of the metal and to heal voids left by the difiused hydrogen. The various working methods may be employed singly or in combination to effect the welding of the voids. The term forging" includes both hammer-forging and press-forging methods. The amount of working or percentage of reduction necessary will be dependent upon the nature of the article and the original content of voids. In some cases, especially in larger articles such as die forgings, a relatively small reduction may be sufiicient to heal or weld the discontinuities in the structure. Generally, in die forgings a reduction of from A to 50 percent by a blocking or finishing operation has been found to be satisfactory, although even greater reductions may occasionally be necessary; hand .forgings may necessitate reductions of 2 to 50 percent. Although extrusion operations will generally heal discontinuities, it is frequently desirable to first forge the metal billets to a reduction in thickness of 2 to 50 percent. Similarly, a preliminary forging is sometimes desirable before a rolling operation.
The degassed and healed aluminum articles may then be subjected to further heat treatments. Because the voids or discontinuities within the metal structure no longer exist, the problem of gassing (or negassing) is minimized unless new discontinuities are subsequently created within the metal structure.
The problem of gaseous occlusions is most pronounced of metals referred to above may be in the form of a casting, compressed powder product or wrought article. Conditions necessary to eflect degassing will, of course, be influenced by the structure of the article.
Illustrating the efficacy of the present invention are the following examples in which aluminum articles were coated with some of the metals of the present invention and heated to extract occluded gas.
EXAMPLE 1 To determine the effect of a cobalt coating upon the degassing of aluminum some 0.091" thick panels of the metal of 99% minimum purity were tested. The panels were given a copper strike followed by electroplating with cobalt thus producing a coating of 0.1 to 0.2 mil in thickness. These panels as well as bare ones were heated in a normal air atmosphere at 940 F. for 15 minutes. The cobalt coating was electrolytically stripped from the panels in a sulfuric acid bath after they had cooled to room temperature. Both groups of panels were then subjected to a blister anneal test in which they were heated to 1100" F. under a vacuum of 1 micron mercury pressure. Upon cooling to room temperature the panels were examined for surface blisters to determine EXAMPLE 2 The effect of a palladium coating upon the degassing of aluminum was determined in the same manner as described in the preceding example. Panels of the same purity of metal and of the same thickness as stated above were first given a copper strike and then electroplated with palladium to provide a coating 0.1 to 0.2 mil in thickness. After heating these and bare panels at 940 F. for 15 minutes in a normal air atmosphere the palladium coating was electrolytically stripped and both groups subjected to the blister annealing. test described above. The panels which had been coated with palladium were free from blisters while those that had received no coating were severely blistered thus indicating the removal of substantially all of the gas from the palladium-coated material.
EXAMPLE 3 The effect of a molybdenum coating upon the degassing of aluminum was determined by spraying panels of the same kind as referred to in the two preceding examples with metallic molybdenum in a conventional manner. The coating so produced had a thickness of about 5 mils. The coated panels along with bare ones were heated at 940 F. for 15 minutes in a normal air atmosphere, cooled to room temperature, and the molybdenum coating electrolytically stripped from the panels upon cooling to room temperature. Both groups of panels were subjected to the blister anneal test mentioned above. The
panels which had been coated with molybdenum revealed no blisters whereas the bare panels were badly blistered. This was considered to show that gas had been removed from the coated panels to the point wheresubstantially none remained.
Having thus described our invention, we claim:
1. The method of substantially reducing the gas content of aluminum articles comprising: coating the surface of an aluminum article containing gas with at least one metal selected from the group consisting of cobalt, molybdenum, paladium, rhodium and' iridium and thereafter heating said coated article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a length of time sufiicient to dilfuse occluded gas into the atmosphere around said article.
2. The method in accordance with claim 1 wherein said atmosphere is air.
3. The method in accordance with claim 1 wherein said atmosphere contains from 1.5 to 30 grains of water per cubic foot.
4. The method in accordance with claim 1 wherein the metal selected is cobalt.
5. The method in accordance with claim 1 wherein the metal selected is molybdenum.
6. The method of substantially reducing the gas content of aluminum articles comprising: coating the surface of an aluminum article containing gas with at least one metal selected from the group consisting of cobalt, m0- lybdenum, palladium; rhodium and iridium; heating said coated article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a'length of time sufficient to difiuse occluded gas into the atmosphere around said article and thereafter stripping said coating from said article.
7. The method substantially reducing the gas content and voids in aluminum articles comprising: coating an aluminum article containing gas and voids with at least one metal selected from the group consisting of cobalt, molybdenum, palladium, rhodium and iridium; heating said article in a gaseous atmosphere at a temperature above 750 F., but below the temperature at which any substantial amount of fusion occurs, for a length of time sufiicient to diffuse occluded gas into the atmosphere around said article; and thereafter working said article to heal any voids therein.
8. The method in accordance with claim 7 wherein said atmosphere is an air containing 1.5 to 30 grains of moisture per cubic foot.
References Cited in the file of this patent UNITED STATES PATENTS UNITED STATESDPATENT OFFICE Q CERTIFICATE OF CORRECTION Patent No. 2,99s 479 August 8, 1961 Charles N, Cochran et a1.
It is hereby certified that error appears in the above numbered petent requiring correction and that the. said Letters Patent should read as corrected below.
Column 1 line 3O for "treated" read traced Signed and sealed this 12th day of December 1961.
(SEAL) Attest:
ERNEST W. SWIDER DAVID L. LADD Attesting Officer Commissioner of Patents USCOMM-DC
Claims (1)
1. THE METHOD OF SUBSTANTIALLY REDUCING THE GAS CONTENT OF ALUMINUM ARTICLES COMPRISING: COATING THE SURFACE OF AN ALUMINUM ARTICLE CONTAINING GAS WITH AT LEAST ONE METAL SELECTED FROM THE GROUP CONSISTING OF COBALT, MOLYBDENUM, PALADIUM, RHODIUM AND IRIDIUM AND THEREAFTER HEATING SAID COATED ARTICLE IN A GASEOUS ATMOSPHERE AT A TEMPERATURE ABOVE 750*F., BUT BELOW THE TEMPERATURE AT WHICH ANY SUBSTANTIAL AMOUNT OF FUSION OCCURS, FOR A LENGTH OF TIME SUFFICIENT TO DIFFUSE OCCLUDED GAS INTO THE ATMOSPHERE AROUND SAID ARTICLE.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2995479A true US2995479A (en) | 1961-08-08 |
Family
ID=3450117
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US2995479D Expired - Lifetime US2995479A (en) | Degassing aluminum articles |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2995479A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3084080A (en) * | 1958-07-17 | 1963-04-02 | Aluminum Co Of America | Production of void-free aluminum and aluminum base alloy articles |
| US5753056A (en) * | 1996-11-25 | 1998-05-19 | Aluminum Company Of America | Transition metal salt compositions that eliminate hydrogen absorption and enhance hydrogen degassing of aluminum |
| US6120618A (en) * | 1997-07-18 | 2000-09-19 | Alcoa Inc. | Hydrocarbon phosphonic acid surface treatment that eliminates hydrogen absorption and enhances hydrogen degassing of aluminum at elevated temperatures |
| US6355121B1 (en) * | 1996-11-25 | 2002-03-12 | Alcoa Inc. | Modified etching bath for the deposition of a protective surface chemistry that eliminates hydrogen absorption at elevated temperatures |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1497417A (en) * | 1919-03-31 | 1924-06-10 | Henry C P Weber | Process of coating metals |
| US1975818A (en) * | 1932-08-24 | 1934-10-09 | Aluminum Co Of America | Coating for pistons |
| US2028312A (en) * | 1932-07-29 | 1936-01-21 | Electrochimie Electrometallurg | Electroplating of aluminium |
| US2499808A (en) * | 1942-08-31 | 1950-03-07 | Univ St Louis | Process for electroplating molybdenum and molybdenum alloys |
| US2733168A (en) * | 1956-01-31 | Tin-zinc base alloys | ||
| US2761792A (en) * | 1952-06-13 | 1956-09-04 | Eutectic Welding Alloys | Process for preparing aluminum cables for soldering |
| US2885316A (en) * | 1958-07-21 | 1959-05-05 | Aluminum Co Of America | Method for degassing aluminum articles by means of a vaporous fluoride |
-
0
- US US2995479D patent/US2995479A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2733168A (en) * | 1956-01-31 | Tin-zinc base alloys | ||
| US1497417A (en) * | 1919-03-31 | 1924-06-10 | Henry C P Weber | Process of coating metals |
| US2028312A (en) * | 1932-07-29 | 1936-01-21 | Electrochimie Electrometallurg | Electroplating of aluminium |
| US1975818A (en) * | 1932-08-24 | 1934-10-09 | Aluminum Co Of America | Coating for pistons |
| US2499808A (en) * | 1942-08-31 | 1950-03-07 | Univ St Louis | Process for electroplating molybdenum and molybdenum alloys |
| US2761792A (en) * | 1952-06-13 | 1956-09-04 | Eutectic Welding Alloys | Process for preparing aluminum cables for soldering |
| US2885316A (en) * | 1958-07-21 | 1959-05-05 | Aluminum Co Of America | Method for degassing aluminum articles by means of a vaporous fluoride |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3084080A (en) * | 1958-07-17 | 1963-04-02 | Aluminum Co Of America | Production of void-free aluminum and aluminum base alloy articles |
| US5753056A (en) * | 1996-11-25 | 1998-05-19 | Aluminum Company Of America | Transition metal salt compositions that eliminate hydrogen absorption and enhance hydrogen degassing of aluminum |
| US6355121B1 (en) * | 1996-11-25 | 2002-03-12 | Alcoa Inc. | Modified etching bath for the deposition of a protective surface chemistry that eliminates hydrogen absorption at elevated temperatures |
| US6120618A (en) * | 1997-07-18 | 2000-09-19 | Alcoa Inc. | Hydrocarbon phosphonic acid surface treatment that eliminates hydrogen absorption and enhances hydrogen degassing of aluminum at elevated temperatures |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4505764A (en) | Microstructural refinement of cast titanium | |
| US4820360A (en) | Method for developing ultrafine microstructures in titanium alloy castings | |
| US2885316A (en) | Method for degassing aluminum articles by means of a vaporous fluoride | |
| US3645800A (en) | Method for producing wrought zirconium alloys | |
| US2995479A (en) | Degassing aluminum articles | |
| JPS59145766A (en) | Aluminum alloy heat treatment | |
| JPS62149859A (en) | Manufacturing method of β-type titanium alloy wire | |
| US4150178A (en) | Aluminum diffusion layer forming method | |
| US2965963A (en) | Aluminum cladding of steel | |
| EP0117671B1 (en) | Bonding metals | |
| US4624714A (en) | Microstructural refinement of cast metal | |
| CA1045009A (en) | Process for producing copper base alloys | |
| US2885315A (en) | Process of treating magnesium-bearing aluminum base alloys with boron trifluoride | |
| US2995478A (en) | Degassing aluminum articles | |
| US3034934A (en) | Method for processing of refractory metals | |
| US2365208A (en) | Manufacture of copper base alloy products | |
| US2885313A (en) | Process of treating magnesium-bearing aluminum base alloys with fluoroborate | |
| US3183588A (en) | Production of alloy-clad articles | |
| US3378916A (en) | Manufacture of superconducting wire | |
| Dobson et al. | Oxidation-vacancy production in aluminium alloys | |
| US3084080A (en) | Production of void-free aluminum and aluminum base alloy articles | |
| US3653250A (en) | Process for forming titanium | |
| Nieh et al. | Unloading yield effects in aluminum alloys | |
| JPH0517857A (en) | Metal matrix composite processing method | |
| US3496036A (en) | Process of making titanium alloy articles |