US3304208A - Production of fine grain aluminum alloy sheet - Google Patents

Production of fine grain aluminum alloy sheet Download PDF

Info

Publication number
US3304208A
US3304208A US387169A US38716964A US3304208A US 3304208 A US3304208 A US 3304208A US 387169 A US387169 A US 387169A US 38716964 A US38716964 A US 38716964A US 3304208 A US3304208 A US 3304208A
Authority
US
United States
Prior art keywords
temperature
ingot
hot rolling
annealing
alloy
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
Application number
US387169A
Inventor
Jager Albert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Revere Copper and Brass Inc
Original Assignee
Revere Copper and Brass Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Revere Copper and Brass Inc filed Critical Revere Copper and Brass Inc
Priority to US387169A priority Critical patent/US3304208A/en
Application granted granted Critical
Publication of US3304208A publication Critical patent/US3304208A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing 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

  • homogenization of the aluminum alloy ingot is carried out at a soaking temperature close to but below the solidus temperature of the alloy for a period not in excess of about 10 hours, the soaked ingot is then controllably cooled at a maximum rate of less than about 50 F. per hour to a temperature not in excess of 100 F. above the initial hot rolling temperature.
  • the conditioned ingot is then hot-rolled at a temperature not in excess of about 100 F. above the annealing temperature of the alloy, cold rolled as before, and annealed at a temperature appropriate for the alloy.
  • the soaking period is limited to a maximum of about 8 to 10 hours and preferably is limited to a maximum of about 6 hours.
  • a soaking period of about 4 hours presently appears to be satisfactory for conventional aluminum alloys such, for example, as 3003, 3004 and 3005.
  • the soaking temperature which is used in practicing the invention is the same as that heretofore used. This temperature is generally close to, but below, the solidus temperature of the alloy being treated. Soaking temperatures usually are within the range of 850 to 1170 F. depending on the alloy and are chosen to be between about 10 and F. below the solidus temperature of the alloy under treatment. By way of example, the solidus temperature of 3003, 3004 and 3005 aluminum alloys are 1190, 1165 and 1175 F., respectively, and the preferred soaking or homogenization temperature for these alloys is between about 1100 and 1l50.
  • the soaked ingot is cooled at an unusually slow rate, pursuant to the invention, in order to prepare the ingot for hot rolling, the cooling operation being carried out in a suitable furnace or other temperature-controlled chamber in air or in any other conventional atmosphere.
  • the slow cooling rate employed promotes maximum precipitation of the non-primary phases and thus insures minimum retention of these phases in solid solution.
  • the slow cooling rate also appears to produce the precipitated phases in a particle size range that resists re-solution during subsequent thermal treatment while the metal is being hot rolled and/or annealed.
  • the particle size and particle distribution obtained by slow cooling is very effective in acting as a grain refiner during the recrystallization which takes place during annealing.
  • the slow cooling rate used in the practice of the invention is less than 50 F. per hour and is generally within the range of about 15 to 35 F. per hour.
  • a cooling rate of about 25 F. per hour is generally satisfactory for all conventional aluminum alloys, including those mentioned herein before.
  • the slow cooling of the soaked ingot is used to obtain maximum precipitation of the non-primary phases of the alloy ingot, it is advantageous to slow cool the soaked ingot to a temperature close to the initial hot rolling temperature. Cooling to a temperature not in excess of about 100 F. above the hot rolling temperature has been found to be satisfactory. For example, if the initial hot rolling temperature is between about 800 and 850 F. as is usually the case with 3003, 3004 and 3005 aluminum alloys, the ingot is advantageously slow cooled to a temperature of about 900 F.
  • Hot rolling is carried out, pursuant to the invention, at the lowest practicable temperature so as to minimize re-solution of the precipitated non-primary phases.
  • a temperature I have found, is initially within about F., and preferably not more than about 100 F., above the appropriate annealing temperature for the aluminum alloy being treated.
  • the initial hot rolling temperature depends upon the alloy, and in the case of the 3003, 3004 and 3005 alloys, an initial temperature of about 800 to 850 F., is presently preferred.
  • the sheet is cold rolled to final gage in the usual manner, the sheet being annealed following each series of cold rollings at the annealing temperature established for the alloy being treated.
  • the annealing temperature for 3003 aluminum alloy is between about 775 to 850 F.
  • the annealing temperature of 3004 and 3005 aluminum alloys is between about 650 and 850 F., the higher temperatures within the aforesaid ranges being ordinarily preferred.
  • the annealing of the rolled sheet pursuant to the invention not only elfects recrystallization of the aluminum schedules employed in accordance with the invention to produce rolled sheet from ingots of representative aluminum alloys obtained by conventional direct chill casting procedures:
  • Example I A chill cast ingot of 3003 aluminum alloy was soaked for four hours at 1140 F., and the soaked ingot was then cooled at a rate of 25 F. per hour until it reached a temperature of 900 F. The initial hot rolling temperature of the ingot was 850 F. After 12 passes through Example 11 An ingot of 3004 aluminum alloy obtained by conventional direct chill casting was soaked at 4 hours at a temperature of 1120 F. The homogenized ingot was cooled at a rate of 25 F. per hour to a temperature of 900 F. and then was subjected to a hot rolling operation at an initial temperature of 850 F. The sheet was then cold rolled to final gage with one interanneal and a final anneal. perature of 750 F. with a 2 hour soak period. The resulting sheet had a fine and uniform grain size.

Description

United States Patent 3,304,208 PRODUCTION OF FINE GRAIN ALUMINUM ALLOY SHEET Albert Jager, Rome, N.Y., assignor to Revere Copper and Brass Incorporated, New York, N.Y., a corporation of Maryland No Drawing. Filed Aug. 3, 1964, Ser. No. 387,169
5 Claims. (Cl. 148-115) aluminum alloy at elevated temperatures, and generally they consist of intermetallic compounds of iron and manganese. However, despite the relative insolubility of these non-primary phases, they tend to be retained in supersaturated solid solution in aluminum ingots produced by the direct chill casting process where rapid cooling and solidification of the ingots are an essential part of the process. In subsequent conventional processing of the ingot to sheet, which involves homogenization (soaking the ingot at a temperature close to the solidus temperature of the alloy) followed by hot rolling, cold rolling and annealing of the sheet, partial precipitation of the non-primary constituents takes place and phase changes occur which bring the constituent system closer to equilibrium conditions. Conventional treatment to effect this result often requires soaking the ingot for twelve hours or more and then air-cooling the ingot at a rate between 200 and 400 F. per hour or furnace cooling the ingot at a rate of approximately 50 F. per hour.
I have now found that a significant improvement in grain size and uniformity of grain size of aluminum alloy sheet can be achieved by interrelated control of the thermal aspects of the homogenizing, hot rolling and annealing of the aluminum sheet. Specifically, I have found that by shortening the soaking time, by cooling the soaked ingot more slowly to a temperature close to the hot rolling temperature, and by subsequent controlled hot rolling and annealing procedures I am able able to induce the proper precipitation of the non-primary phases so as to produce a uniformly fine grained product. Pursuant to the present invention, homogenization of the aluminum alloy ingot is carried out at a soaking temperature close to but below the solidus temperature of the alloy for a period not in excess of about 10 hours, the soaked ingot is then controllably cooled at a maximum rate of less than about 50 F. per hour to a temperature not in excess of 100 F. above the initial hot rolling temperature. The conditioned ingot is then hot-rolled at a temperature not in excess of about 100 F. above the annealing temperature of the alloy, cold rolled as before, and annealed at a temperature appropriate for the alloy.
During the soaking period while the aluminum alloy ingot is maintained at an elevated temperature, the nonprimary phases are predominantly dissolved and phase changes take place in those phases which remain undissolved. I have found that if soaking is carried out for over 10 hours the grain structure and micro-structure are changed to such an extent as to adversely affect the final grain size in the rolled sheet obtained from such an ingot. In practicing the present invention, however,
the soaking period is limited to a maximum of about 8 to 10 hours and preferably is limited to a maximum of about 6 hours. A soaking period of about 4 hours presently appears to be satisfactory for conventional aluminum alloys such, for example, as 3003, 3004 and 3005.
The soaking temperature which is used in practicing the invention is the same as that heretofore used. This temperature is generally close to, but below, the solidus temperature of the alloy being treated. Soaking temperatures usually are within the range of 850 to 1170 F. depending on the alloy and are chosen to be between about 10 and F. below the solidus temperature of the alloy under treatment. By way of example, the solidus temperature of 3003, 3004 and 3005 aluminum alloys are 1190, 1165 and 1175 F., respectively, and the preferred soaking or homogenization temperature for these alloys is between about 1100 and 1l50.
The soaked ingot is cooled at an unusually slow rate, pursuant to the invention, in order to prepare the ingot for hot rolling, the cooling operation being carried out in a suitable furnace or other temperature-controlled chamber in air or in any other conventional atmosphere. The slow cooling rate employed promotes maximum precipitation of the non-primary phases and thus insures minimum retention of these phases in solid solution. The slow cooling rate also appears to produce the precipitated phases in a particle size range that resists re-solution during subsequent thermal treatment while the metal is being hot rolled and/or annealed. In addition, the particle size and particle distribution obtained by slow cooling is very effective in acting as a grain refiner during the recrystallization which takes place during annealing. The slow cooling rate used in the practice of the invention is less than 50 F. per hour and is generally within the range of about 15 to 35 F. per hour. A cooling rate of about 25 F. per hour is generally satisfactory for all conventional aluminum alloys, including those mentioned herein before.
Inasmuch as the slow cooling of the soaked ingot is used to obtain maximum precipitation of the non-primary phases of the alloy ingot, it is advantageous to slow cool the soaked ingot to a temperature close to the initial hot rolling temperature. Cooling to a temperature not in excess of about 100 F. above the hot rolling temperature has been found to be satisfactory. For example, if the initial hot rolling temperature is between about 800 and 850 F. as is usually the case with 3003, 3004 and 3005 aluminum alloys, the ingot is advantageously slow cooled to a temperature of about 900 F.
Hot rolling is carried out, pursuant to the invention, at the lowest practicable temperature so as to minimize re-solution of the precipitated non-primary phases. Such a temperature, I have found, is initially within about F., and preferably not more than about 100 F., above the appropriate annealing temperature for the aluminum alloy being treated. The initial hot rolling temperature, of course, depends upon the alloy, and in the case of the 3003, 3004 and 3005 alloys, an initial temperature of about 800 to 850 F., is presently preferred.
Following hot rolling, the sheet is cold rolled to final gage in the usual manner, the sheet being annealed following each series of cold rollings at the annealing temperature established for the alloy being treated. For example, the annealing temperature for 3003 aluminum alloy is between about 775 to 850 F. and the annealing temperature of 3004 and 3005 aluminum alloys is between about 650 and 850 F., the higher temperatures within the aforesaid ranges being ordinarily preferred. The annealing of the rolled sheet pursuant to the invention not only elfects recrystallization of the aluminum schedules employed in accordance with the invention to produce rolled sheet from ingots of representative aluminum alloys obtained by conventional direct chill casting procedures:
Example I A chill cast ingot of 3003 aluminum alloy was soaked for four hours at 1140 F., and the soaked ingot was then cooled at a rate of 25 F. per hour until it reached a temperature of 900 F. The initial hot rolling temperature of the ingot was 850 F. After 12 passes through Example 11 An ingot of 3004 aluminum alloy obtained by conventional direct chill casting was soaked at 4 hours at a temperature of 1120 F. The homogenized ingot was cooled at a rate of 25 F. per hour to a temperature of 900 F. and then was subjected to a hot rolling operation at an initial temperature of 850 F. The sheet was then cold rolled to final gage with one interanneal and a final anneal. perature of 750 F. with a 2 hour soak period. The resulting sheet had a fine and uniform grain size.
From the foregoing description of my new process for producing aluminum sheet of uniform fine grain, it will be seen that I have made an important contribution to the art to which my invention relates.
I claim:
1. A method for producing a uniformly fine grained sheet product from a chill cast ingot of an aluminum alloy in which there is present a non-primary manganesecontaining phase and which is processed by homogenizing, hot rolling, cold rolling and annealing by means of the inter-related control of the thermal aspects of homog- Both anneals were performed at a tem-- enizing, hot rolling and annealing so as to induce proper precipitation of the non-primary phase, said method com-- prising (a) homogenizing the ingot at a temperature: just below the solidus temperature for the alloy for a period not in excess of about 10 hours, (b) slowly cooling the ingot at a rate less than F. per hour to a tern-- perature which is not in excess of F. above the initial hot rolling temperature, (c) hot rolling at the low-- est practical temperature, (d) cold rolling the resulting: sheet to final gage, and (e) annealing following cold. rolling at the annealing temperature of the aluminum. sheet so as to continue the aforestated phenomena of proper precipitation of the non-primary phase.
2. The method according to claim 1 in which the homogenizing of the ingot is carried out at a temperature between 10 and 100 F. below the solidus temperature of the alloy.
3. The method according to claim 1 in which the slow cooling of the homogenized ingot is carried out at a rate of between about 15 to 35 F. per hour.
4. The method according to claim 1 in which the hot rolling is carried out at an initial temperature of not more than F. above the annealing temperature of the alloy.
5. The method according to claim 1 in which the homogenizing of the ingot is carried out at a temperature between 10 and 100 F. below the solidus temperature of the alloy for a period not in excess of about 6 hours, the slow cooling of the homogenized ingot is carried out at a rate of between 15 to 35 F. per hour, and the hot rolling is carried out at an initial temperature of not more than about 100 F. above the annealing temperature of the alloy.
References Cited by the Examiner UNITED STATES PATENTS 2,262,696 11/1941 Nock et al. 14811.5 3,219,491 11/1965 Anderson et al. 14811.5 3,219,492 11/1965 Anderson et al. 148--11.5
FOREIGN PATENTS 7 80,570 8/ 1957 Great Britain.
DAVID L. RECK, Primary Examiner- H. F. SAITO, Assistan,tEXamine11-.

Claims (1)

1. A METHOD FOR PRODUCING A UNIFORMLY FINE GRAINED SHEET PRODUCT FROM A CHILL CAST INGOT OF AN ALUMINUM ALLOY IN WHICH THERE IS PRESENT A NON-PRIMARY MANGANESECONTAINING PHASE AND WHICH IS PROCESSED BY HOMOGENIZING, HOT ROLLING, COLD ROLLING AND ANNEALING BY MEANS OF THE INTER-RELATED CONTROL OF THE THERMAL ASPECTS OF HOMOGENIZING, HOT ROLLING AND ANNEALING TO AS TO INDUCE PROPER PRECIPITATION OF THE NON-PRIMARY PHASE, SAID METHOD COMPRISING (A) HOMOGENIZING THE INGOT AT A TEMPERATURE JUST BELOW THE SOLIDUS TEMPERATURE FOR THE ALLOY FOR A PERIOD NOT IN EXCESS OF ABOUT 10 HOURS, (B) SLOWLY COOLING THE INGOT AT A RATE LESS THAN 50*F. PER HOUR TO A TEMPERATURE WHICH IS NOT IN EXCESS OF 100*F. ABOVE THE INITIAL HOT ROLLING TEMPERATURE, (C) HOT ROLLING AT THE LOWEST PRACTICAL TEMPERATURE, (D) COLD ROLLING THE RESULTING SHEET TO FINAL GAGE, AND (E) ANNEALING FOLLOWING COLD ROLLING AT THE ANNEALING TEMPERATURE OF THE ALUMINUM SHEET SO AS TO CONTINUE THE AFORESTATED PHENOMENA OF PROPER PRECIPITATION OF THE NON-PRIMARY PHASE.
US387169A 1964-08-03 1964-08-03 Production of fine grain aluminum alloy sheet Expired - Lifetime US3304208A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US387169A US3304208A (en) 1964-08-03 1964-08-03 Production of fine grain aluminum alloy sheet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US387169A US3304208A (en) 1964-08-03 1964-08-03 Production of fine grain aluminum alloy sheet

Publications (1)

Publication Number Publication Date
US3304208A true US3304208A (en) 1967-02-14

Family

ID=23528770

Family Applications (1)

Application Number Title Priority Date Filing Date
US387169A Expired - Lifetime US3304208A (en) 1964-08-03 1964-08-03 Production of fine grain aluminum alloy sheet

Country Status (1)

Country Link
US (1) US3304208A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4000009A (en) * 1975-03-26 1976-12-28 National Steel Corporation Wrought pure grade aluminum alloy and process for producing same
EP0039211A1 (en) * 1980-04-28 1981-11-04 Alcan International Limited Production of aluminium alloy sheet
US4483719A (en) * 1983-08-23 1984-11-20 Swiss Aluminium Ltd. Process for preparing fine-grained rolled aluminum products
US5141820A (en) * 1991-01-04 1992-08-25 Showa Aluminum Corporation Aluminum pipe for use in forming bulged portions thereon and process for producing same

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2262696A (en) * 1939-10-21 1941-11-11 Aluminum Co Of America Method of treating aluminum alloys
GB780570A (en) * 1955-04-06 1957-08-07 Oesterreichische Metallwerke A Method of making sheet or strip of aluminium or aluminium alloys
US3219491A (en) * 1962-07-13 1965-11-23 Aluminum Co Of America Thermal treatment of aluminum base alloy product
US3219492A (en) * 1962-11-16 1965-11-23 Aluminum Co Of America Thermal treatment of aluminum base alloy product

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2262696A (en) * 1939-10-21 1941-11-11 Aluminum Co Of America Method of treating aluminum alloys
GB780570A (en) * 1955-04-06 1957-08-07 Oesterreichische Metallwerke A Method of making sheet or strip of aluminium or aluminium alloys
US3219491A (en) * 1962-07-13 1965-11-23 Aluminum Co Of America Thermal treatment of aluminum base alloy product
US3219492A (en) * 1962-11-16 1965-11-23 Aluminum Co Of America Thermal treatment of aluminum base alloy product

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4000009A (en) * 1975-03-26 1976-12-28 National Steel Corporation Wrought pure grade aluminum alloy and process for producing same
EP0039211A1 (en) * 1980-04-28 1981-11-04 Alcan International Limited Production of aluminium alloy sheet
US4483719A (en) * 1983-08-23 1984-11-20 Swiss Aluminium Ltd. Process for preparing fine-grained rolled aluminum products
US5141820A (en) * 1991-01-04 1992-08-25 Showa Aluminum Corporation Aluminum pipe for use in forming bulged portions thereon and process for producing same

Similar Documents

Publication Publication Date Title
US3418177A (en) Process for preparing aluminum base alloys
US4618382A (en) Superplastic aluminium alloy sheets
US3219491A (en) Thermal treatment of aluminum base alloy product
US3847681A (en) Processes for the fabrication of 7000 series aluminum alloys
US3522112A (en) Process for treating copper base alloy
US3945860A (en) Process for obtaining high ductility high strength aluminum base alloys
US5098490A (en) Super position aluminum alloy can stock manufacturing process
GB907228A (en) Method of producing solution heat treated extrusions of aluminum base alloys
US5662750A (en) Method of manufacturing aluminum articles having improved bake hardenability
US4067750A (en) Method of processing copper base alloys
US4000009A (en) Wrought pure grade aluminum alloy and process for producing same
US3379583A (en) Heat treatment of aluminum alloys
US3304208A (en) Production of fine grain aluminum alloy sheet
US4295901A (en) Method of imparting a fine grain structure to aluminum alloys having precipitating constituents
US3874213A (en) Extrusion method for high strength heat treatable aluminum alloys
US2412447A (en) Working and treating be-cu alloys
US3486947A (en) Enhanced structural uniformity of aluminum based alloys by thermal treatments
NO162082B (en) PROCEDURE FOR THE MANUFACTURE OF THIN TAPE OR FILM OF ALUMINUM AND USE OF TAPE OR FILM OF THIS ART.
US3008857A (en) Process for the production of grain oriented magnetizable strips and sheets
Grimes Grain control in aluminium
US4709742A (en) Method for producing a thin casting of Cr-series stainless steel
US3753791A (en) Heat-treatment of zinc/aluminium alloys
JPH0588302B2 (en)
US1278207A (en) Producing wrought shapes of manganese steel.
US3484307A (en) Copper base alloy