WO1997022724A1 - Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom - Google Patents

Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom Download PDF

Info

Publication number
WO1997022724A1
WO1997022724A1 PCT/US1996/019878 US9619878W WO9722724A1 WO 1997022724 A1 WO1997022724 A1 WO 1997022724A1 US 9619878 W US9619878 W US 9619878W WO 9722724 A1 WO9722724 A1 WO 9722724A1
Authority
WO
WIPO (PCT)
Prior art keywords
sheet product
aging
heating
aluminum alloy
sheet
Prior art date
Application number
PCT/US1996/019878
Other languages
French (fr)
Inventor
J. Daniel Bryant
Hideo Yoshida
Hidetoshi Uchida
Original Assignee
Reynolds Metals Company
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24293816&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO1997022724(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Reynolds Metals Company filed Critical Reynolds Metals Company
Priority to DE69628044T priority Critical patent/DE69628044T2/en
Priority to EP96944361A priority patent/EP0874917B1/en
Priority to JP9522922A priority patent/JP2000503069A/en
Publication of WO1997022724A1 publication Critical patent/WO1997022724A1/en

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • C21D9/54Furnaces for treating strips or wire
    • C21D9/56Continuous furnaces for strip or wire
    • 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
    • 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
    • C22F1/05Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • C21D9/54Furnaces for treating strips or wire
    • C21D9/56Continuous furnaces for strip or wire
    • C21D9/60Continuous furnaces for strip or wire with induction heating
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the present invention is directed to a method and apparatus of making aluminum sheet product and products tnerefrom and, in particular, a method of pre-aging aluminum automotive sheet to produce a product which exhibits increased yield strength in response to automotive pamtbake cycles, superior resistance to natural aging prior to stamping, and improved stamping performance.
  • vehicle sheet product is approximately 0.040" m thickness and includes both AA 2000 and AA 6000 series aluminum alloys.
  • Preferred AA 2000 series alloys include AA 2008, AA 2010 and AA 2036.
  • AA 6000 series alloys include AA 6010, AA 6016 and AA 6111.
  • the AA 6000 series alloys are usually employed in automotive outer panel applications, such as deck lids or noods, due to their higher strengtn and superior dent resistance.
  • the standard automotive pamtbake cycle of about 350°F for approximately 30 minutes is generally insufficient to impart a significant aging response (PBR) in AA 6XXX alloys. While a full T6 aging treatment of 8 hours at 350°F can mcrease the yield strength of these alloys by up to 25 ksi, the standard 30 minute aging cycle generally imparts only a 2 to 4 ksi mcrease in yield strength.
  • PBR aging response
  • FIG. 1 A general schematic of a prior art pre-agmg process for AA 6XXX alloys is given in Figure 1.
  • the application of a pre-age treatment generally enhances the kinetics of precipi ;at ⁇ on and decreases the precipitate size and lessens the average interparticle separation.
  • the principle metallurgical effect in these types of pre-aging treatments is the refinement of the strengthening precipitates. It is this latter effect which is mainly responsible for the increased strength pre-aged materials.
  • the pre-aging of AA 6111 alloys offers the potential of increasing the paintbake response substantially.
  • improved PBR would significantly improve the dent resistance (or allow down gauging) , while maintaining the same formability.
  • Other strategies to achieve these improvements may involve using leaner alloy compositions which could deliver low yield strength (lower springback) and superior formability in the T4 condition, and yet have dent resistance comparable to more heavily alloyed Al-Mg-Si-Cu alloys (such as AA 6111 and AA 6010) in the paintbaked condition.
  • An AA 6111-F temper product was subjected to a standard solution heat treatment and quench.
  • a pre-aging cycle of 212°F for 24 hours was imposed following dwell times at 75°F of 20 minutes, 120 minutes, 18 hours, and 96 hours.
  • Subsequent to a 10 day natural aging (75°F) period the specimens were subjected to paintbake cycle of 350°F for 30 minutes.
  • the tensile test results showed that the effectiveness of the pre-aging treatment in enhancing the paintbake response was very sensitive to the dwell time.
  • the post-paintbake yield strength was seen to decay rapidly from 36 ksi to 27 ksi as the dwell time was increased from 20 minutes to 96 hours, with most of the decay occurring in the first 18 hours.
  • Increasing the dwell time from 20 minutes to two hours resulted in a 2 to 3 si loss in post-paintbake response (PBR) .
  • PBR post-paintbake response
  • a first object of the present invention is to provide a method of making aluminum sheet which will have a superior strength following the application of conventional automotive paintbake cycles.
  • Another objective of the present invention is to produce an aluminum sheet product which exhibits superior stability during extended periods of natural aging, so as to provide for consistent stamping performance during its use in the production of automotive and truck components, such as panels.
  • a further object of the present invention is to provide an apparatus for making aluminum sheet having superior strength following the application of conventional automotive paintbake cycles.
  • a still further object of the present invention is to provide a method and apparatus of making aluminum ;;heet which is adaptable for aluminum alloys typically used in vehicle component applications such as Al-Mg-Si alloys, Al-Mg-Si-Cu alloys and more preferably AA 2000 and AA 6000 series type aluminum alloys.
  • the inventive method is an improvement over the known processing of making aluminum alloy sheet based on either Al-Mg-Si or Al-Mg-Si-Cu containing aluminum alloys wherein the alloy is hot rolled and cold rolled to form a cold rolled sheet.
  • the cold rolled sheet is then further subjected to continuous solution heat treating, continuous quenching and continuous coiling to provide the sheet in coil form.
  • the sheet is continuously and rapidly heated to a pre-aging temperature after the continuous quenching step and prior to the continuous coiling step. After rapid heating, the sheet in coil form is ambiently cooled, the rapid heating and ambient cooling improving the paintbake response of the aluminum alloy sheet.
  • the rapid heating raises the coiled sheet temperature to between 150 and 250°F, more preferably about 200°F.
  • the ambient cooling rate will be a function of ambient conditions but is preferred to be between 2° and 6°F per hour and more preferably about 3°F per hour.
  • the rapid heating step is designed to raise the temperature of the aluminum sheet after quenching to the target pre-aging temperature as fast as possible, preferably by induction heating.
  • /22724 In the apparatus of the invention, /22724
  • a means for continuously rapidly heating the sheet to a pre- aging temperature is disposed between a conventional solution heat treating/quenching apparatus and the coiling station of a conventional continuous aluminum alloy heat treating line.
  • the means for rapid heating is preferably an induction heater so that the sheet temperature is rapidly brought up to the pre-aging temperature for subsequent ambient cooling and yet provides sufficient uniformity and control in the event of line slowdowns or stoppages.
  • a sheet product made by the method described above is disclosed, the sheet product exhibiting significant improvement in paintbake response, e.g. up to 14 ksi or more, as well as resistance to natural aging and improved formability as a result of increased elongation values, superior workhardening character and lower strength in the pre-paintbaked condition.
  • solution heat treated and quenched aluminum sheet is rapidly heated to a temperature between about 150°F and about 250°F in a continuous process, such heating occurring as soon as possible after the application of the quench and leveling which follow solution heat treatment.
  • the aluminum sheet is then coiled and allowed to cool as a coiled product without the necessity of additional furnace treatments.
  • the natural cooling of the coil on the plant floor provides for an acceptable pre-aging treatment which avoids the need for subsequent re-heating and is subject to only minimal losses in performance due to the phenomenon of dwell time decay.
  • Figure 1 is a schematic diagram of a prior art processing technique for pre-aging of aluminum alloy sheets
  • Figure 2 is a graph showing the effect of dwell time on post paintbake yield stress
  • FIG. 3 is a schematic diagram of one mode of the inventive processing
  • Figure 4 is an ambient cooling curve for an aluminum coil
  • Figure 5 is a graph showing the effect of rapid heating to temperatures between 175°F and 250°F followed by simulated coil cooling on yield strength both before and after a simulated paintbake treatment;
  • Figure 6 is a graph showing the effect of rapid heating and simulated coil cooling on yield strength and paintbake response.
  • Figure 7 is a graph showing the effect of rapid heating and simulated coil cooling on the total elongation and uniform elongation. Description of the Preferred Embodiments
  • the inventive method and apparatus are effective at significantly improving the strength of Al-Mg-Si and Al-Mg- Si-Cu- type aluminum alloy autobody sheet, while simultaneously improving its formability and stamping performance.
  • Use of the inventive processing method on these types of aluminum alloy sheet products enhances the artificial aging response obtained during the standard automotive paintbake cycles by up to 4-fold.
  • the aluminum sheet is subjected to rapid heating to a pre-aging temperature following the standard solution heating and quenching and prior to sheet coiling.
  • the pre-aging temperature is defined as that temperature which does not cause excessive aging and increased T4 yield strength while still providing a significant paintbake response, resistance to natural aging and improved formability.
  • the pre-aging temperature is between 150° and 250°F.
  • the heating rate is such that the material being continuously and rapidly treated is brought up to the pre-aging temperature substantially instantaneously, i.e. without any ramping or other slow heat up.
  • the heating occurs as soon as possible after the application of the quench which follows solution heat treatment.
  • the aluminum is then coiled and allowed to cool as a coiled product without the necessity of additional furnace treatments.
  • the natural cooling of the coil usually on a plant floor, provides for an acceptable pre-aging treatment which avoids the need for subsequent re-heating and is subject to only minimal losses in performance due to the phenomenon of dwell time decay.
  • the method described provides distinct advantages over the standard practice and over batch pre-aging strategies discussed above.
  • the most significant advantages are: Paintbake response can be increased from the standard 2 ksi to 14 ksi; Natural aging in the product is suspended; Formability of the product is increased.
  • the application of the continuous pre-age cycle offers a method to produce an aluminum sheet product with improved dent resistance, greater stability for consistency of stamping and superior stamping performance.
  • the processing method avoids additional metal handling, and thus promises to be a low cost method to improve product performance and reduce product variability.
  • a schematic diagram showing one embodiment of a coil pre-aging apparatus is shown in Figure 3.
  • a freshly quenched alloy 6111 sheet 1 exiting the accumulator 3 at the exit of a continuous heat treater (CHT) 5 is re ⁇ heated to a temperature of between 150°F and 250°F usmg an induction heater 7.
  • Figure 3 also shows a leveler 9 downstream of the CHT 5 and an exit accumulator 3 disposed between the leveler 9 and the induction heater 7.
  • the sheet 1 After the sheet 1 is pre-aged by the induction heater 7, it is coiled into coil form 13 for subsequent processing.
  • the induction heater 7 is a preferred device for rapidly heating the solution heat treated and quenched sheet 1 prior to formation of the coil form 13. Any means for this rapid heating can be utilized accordine; to the invention.
  • the rapid heating means is designed to rapidly heat the sheet 1 to a target pre-age temperature.
  • the following provides an exemplary calculation to determine the power requirement or heating rate ;:or a rapid heating means based on a target pre-aging temperature of 250°F, a specified line speed, a specified entry temperature and a specified size and type for the sheet to be rapidly heated.
  • the power requirement may vary depending on the particular variables selected.
  • test work was performed with respect to paintbake response, natural aging resistance and improved formability.
  • the tests described below further explain the ambient cooling rates used in conjunction with the rapid heating pre-aging treatment, as well as the enhanced physical properties achieved by the invention. It should be understood that the experiments described below are only exemplary of the invention and the invention is not so limited.
  • Cooling rates near the outer wraps and near the center of the coil are nearly the same. This implies that cooling occurs largely through the sheet ends (axially) rather than through the surface of the outer wraps (radially) , as would be expected given the relative heat transfer coefficients of aluminum and alumina/air/oil barriers .
  • the T4 aluminum alloy sheet prior to paint baking shows a relatively flat curve for yield strength over 60 days. What this means is that, by pre-aging according to the invention, resistance to natural aging is increased. Thus, the aluminum sheet does not exhibit the typical yield strength increase in T4 yield strength, i.e. one or two ksi, which can adversely affect stamping performance. The T4 yield strength is also lowered, reducing the problem of springback that is common with automotive aluminum stampings.
  • Figure 6 also reaffirms the significant paintbake response achieved when the aluminum sheet is pre-aged according to the invention, even after 60 days of natural aging time.
  • Figure 7 quite surprisingly along with improved paintbake response, aluminum sheet subjected to the inventive processing also exhibits significant improvements in T4 total elongation and uniform elongation.
  • the curves noted in Figure 7 as measuring elongation show significant improvements over the standard unleveled T4 elongation of 24%. Using a 200°F start temperature and 60 days of natural aging time, a 4% increase over the prior art standard is realized (28%) .
  • Concerning uniform elongation typically, this value for a -standard AA 6111 - T4 alloy is about 18%.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

A method and apparatus for making aluminum alloy sheet product with improved paintbake response during automotive paintbake cycles, resistance to natural aging and better formability includes rapidly heating the aluminum alloy sheet product between a solution heat treating (5)/quenching operation (1) and a sheet coiling operation (13). Performing the rapid heating at this stage in the sheet manufacture minimizes the adverse effect of early natural aging (dwell time) on the paintbake response of these types of aluminum sheet alloy products. According to the invention, this dwell time is minimized by the application of a rapid heating step (7) immediately following quenching from the solution heat treatment. After the aluminum sheet product has been rapidly heated, it is immediately coiled and cools under ambient conditions in coil form (13), this ambient cooling providing a pre-aging treatment which contributes to the improved performance of the sheet product in paintbake response, improved formability and natural aging resistance.

Description

PROCESS AND APPARATUS TO ENHANCE THE
PAINTBAKE RESPONSE AND AGING
STABILITY OF ALUMINUM SHEET MATERIALS AND PRODUCT THEREFROM
Field of the Invention
The present invention is directed to a method and apparatus of making aluminum sheet product and products tnerefrom and, in particular, a method of pre-aging aluminum automotive sheet to produce a product which exhibits increased yield strength in response to automotive pamtbake cycles, superior resistance to natural aging prior to stamping, and improved stamping performance.
Background Art In the automotive industry, the use of aluminum alloys is increasing due to the their desirable combination of properties, such as corrosion resistance, low density and compatibility with existing manufacturing methods and equipment. Typically, vehicle sheet product is approximately 0.040" m thickness and includes both AA 2000 and AA 6000 series aluminum alloys. Preferred AA 2000 series alloys include AA 2008, AA 2010 and AA 2036. AA 6000 series alloys include AA 6010, AA 6016 and AA 6111. The AA 6000 series alloys are usually employed in automotive outer panel applications, such as deck lids or noods, due to their higher strengtn and superior dent resistance.
One advantage certain aluminum alloys have for automotive applications is the ability tc improve their properties using heat treatment. Ideally, these aluminum alloys have sufficient formability so that they can be formed or stamped into a desired panel or other component configuration and then subsequently strengthened during an automotive pamtbaking cycle to improve dent resistance. Alternatively, a significant strengthening during the automotive pamtbaking cycle could be exploited to allow for down gauging of the panel thickness, promoting even greater component weight savings. This strengthening LS commonly referred to as the "pamtbake response" (PBR) .
The standard automotive pamtbake cycle of about 350°F for approximately 30 minutes is generally insufficient to impart a significant aging response (PBR) in AA 6XXX alloys. While a full T6 aging treatment of 8 hours at 350°F can mcrease the yield strength of these alloys by up to 25 ksi, the standard 30 minute aging cycle generally imparts only a 2 to 4 ksi mcrease in yield strength.
To obtain improved PBR, the application of a pre-aging treatment to AA 6XXX alloys to enhance artificial, aging and minimize natural aging has been proposed. A general schematic of a prior art pre-agmg process for AA 6XXX alloys is given in Figure 1. The application of a pre-age treatment generally enhances the kinetics of precipi ;atιon and decreases the precipitate size and lessens the average interparticle separation. The principle metallurgical effect in these types of pre-aging treatments is the refinement of the strengthening precipitates. It is this latter effect which is mainly responsible for the increased strength pre-aged materials. The pre-aging of AA 6111 alloys offers the potential of increasing the paintbake response substantially. As stated above, improved PBR would significantly improve the dent resistance (or allow down gauging) , while maintaining the same formability. Other strategies to achieve these improvements may involve using leaner alloy compositions which could deliver low yield strength (lower springback) and superior formability in the T4 condition, and yet have dent resistance comparable to more heavily alloyed Al-Mg-Si-Cu alloys (such as AA 6111 and AA 6010) in the paintbaked condition.
While the pre-aging of aluminum alloys may offer improvements with respect to the manufacture of vehicle components, prior art pre-aging techniques are not without their disadvantages. In one prior art approach, aluminum alloy coils which have been solution heat treated and quenched are subjected to batch furnace heating. The use of batch (or coil) pre-aging approaches suffers from the phenomenon uncovered in our research and referred to as "dwell time decay". The dwell time is defined as the duration of time between the application of the quench and the application of the pre-age (Figure 1) . It was found that the potential PBR of the alloy was severely compromised as the dwell time increased. To determine the effect of ambient temperature dwell time on the effectiveness of a pre-aging treatment, a series of experiments were conducted. An AA 6111-F temper product was subjected to a standard solution heat treatment and quench. A pre-aging cycle of 212°F for 24 hours was imposed following dwell times at 75°F of 20 minutes, 120 minutes, 18 hours, and 96 hours. Subsequent to a 10 day natural aging (75°F) period, the specimens were subjected to paintbake cycle of 350°F for 30 minutes. The tensile test results showed that the effectiveness of the pre-aging treatment in enhancing the paintbake response was very sensitive to the dwell time. As shown in Figure 2 in a semi-log plot, the post-paintbake yield strength was seen to decay rapidly from 36 ksi to 27 ksi as the dwell time was increased from 20 minutes to 96 hours, with most of the decay occurring in the first 18 hours. Increasing the dwell time from 20 minutes to two hours resulted in a 2 to 3 si loss in post-paintbake response (PBR) . After 18 hours, the PBR had decayed to a level near that of the standard AA 611.1 product.
Some of the obvious problems with batch treatment are: 1. The coiling time after heat treatment can be up to an hour, even without stoppages. Under most production conditions, autobody sheet is run at 75 to
200 fpm on a continuous heat treater (CHT) . Coils could not be transferred, even under the best of conditions, until the head of the coil and tie tail of the coil are wrapped onto the same arbor. At these speeds and the common coil sizes, the material near the arbor will have experienced a minimum of ore hour of dwell time, compromising the performance of the product.
2. Heat transfer to the coil in a batch heat treating furnace would be sluggish. High furnace heads could not be tolerated as they would cause premature aging. The effective dwell time would increase significantly as the coil was brought to the pre-aging temperature. Again, performance would be compromisecL
3. Heat transfer out of the coil (cooling) would be sluggish. Excessive pre-aging would also compromise performance.
4. A furnace load would require 6 to 8 coils per batch to be economical; the dwell time could be conceivably multiplied by this factor as the furnace load is accumulated. Other technical difficulties are encountered if a continuous pre-aging approach is considered. Using a continuous pre-aging approach, sheet would be paid off the coil and pass through a low temperature heater and be cooled and coiled again. The obvious problem with applying this approach is the long soak times involved. Using the known successful pre-aging cycle of 212°F soak for 24 hours would result in an unacceptable through-put from an economic standpoint. Alternative continuous pre-aging treatments also have their disadvantages. Applying a high temperature "spike" (soak times of several seconds to several minutes), see U.S. Patent No. 4,808,247 to Komatsubura et al. , as a pre-age using a continuous heat treater results in accelerated natural aging, a phenomenon which results in product instability and limited shelf life. This coiling- uncoiling-coiling approach also suffers from the economic barrier of having to pass the coil through yet one more processing line, incurring expense and possible handling damage and the associated losses. In view of the disadvantages noted above in prior art processing utilizing both batch and continuous pre-aging treatments, a need has developed to provide an improved aluminum alloy sheet product which has improved paintbake response, resistance to natural aging, improved formability, and that can be produced with a viable economic process on an industrial scale. Responsive to this need, the present invention sets forth a method and an apparatus which produces an aluminum alloy sheet having an improved paintbake response and, quite surprisingly, also provides resistance to natural aging and improved formability.
Summary of the Invention
A first object of the present invention is to provide a method of making aluminum sheet which will have a superior strength following the application of conventional automotive paintbake cycles.
Another objective of the present invention is to produce an aluminum sheet product which exhibits superior stability during extended periods of natural aging, so as to provide for consistent stamping performance during its use in the production of automotive and truck components, such as panels.
A further object of the present invention is to provide an apparatus for making aluminum sheet having superior strength following the application of conventional automotive paintbake cycles.
A still further object of the present invention is to provide a method and apparatus of making aluminum ;;heet which is adaptable for aluminum alloys typically used in vehicle component applications such as Al-Mg-Si alloys, Al-Mg-Si-Cu alloys and more preferably AA 2000 and AA 6000 series type aluminum alloys.
Other objects and advantages of the present invention will become apparent as a description thereof proceeds.
In satisfaction of the forgoing objects and advantages, in its broadest embodiment, the inventive method is an improvement over the known processing of making aluminum alloy sheet based on either Al-Mg-Si or Al-Mg-Si-Cu containing aluminum alloys wherein the alloy is hot rolled and cold rolled to form a cold rolled sheet. The cold rolled sheet is then further subjected to continuous solution heat treating, continuous quenching and continuous coiling to provide the sheet in coil form. According to the invention, the sheet is continuously and rapidly heated to a pre-aging temperature after the continuous quenching step and prior to the continuous coiling step. After rapid heating, the sheet in coil form is ambiently cooled, the rapid heating and ambient cooling improving the paintbake response of the aluminum alloy sheet.
Preferably, the rapid heating raises the coiled sheet temperature to between 150 and 250°F, more preferably about 200°F. The ambient cooling rate will be a function of ambient conditions but is preferred to be between 2° and 6°F per hour and more preferably about 3°F per hour.
The rapid heating step is designed to raise the temperature of the aluminum sheet after quenching to the target pre-aging temperature as fast as possible, preferably by induction heating. In the apparatus of the invention, /22724
a means for continuously rapidly heating the sheet to a pre- aging temperature is disposed between a conventional solution heat treating/quenching apparatus and the coiling station of a conventional continuous aluminum alloy heat treating line. The means for rapid heating is preferably an induction heater so that the sheet temperature is rapidly brought up to the pre-aging temperature for subsequent ambient cooling and yet provides sufficient uniformity and control in the event of line slowdowns or stoppages. In a further aspect of the invention a sheet product made by the method described above is disclosed, the sheet product exhibiting significant improvement in paintbake response, e.g. up to 14 ksi or more, as well as resistance to natural aging and improved formability as a result of increased elongation values, superior workhardening character and lower strength in the pre-paintbaked condition.
More preferably, solution heat treated and quenched aluminum sheet is rapidly heated to a temperature between about 150°F and about 250°F in a continuous process, such heating occurring as soon as possible after the application of the quench and leveling which follow solution heat treatment. The aluminum sheet is then coiled and allowed to cool as a coiled product without the necessity of additional furnace treatments. The natural cooling of the coil on the plant floor provides for an acceptable pre-aging treatment which avoids the need for subsequent re-heating and is subject to only minimal losses in performance due to the phenomenon of dwell time decay. Brief Description of the Drawings;
Reference is now made to the drawings of the invention wherein:
Figure 1 is a schematic diagram of a prior art processing technique for pre-aging of aluminum alloy sheets;
Figure 2 is a graph showing the effect of dwell time on post paintbake yield stress;
Figure 3 is a schematic diagram of one mode of the inventive processing;
Figure 4 is an ambient cooling curve for an aluminum coil;
Figure 5 is a graph showing the effect of rapid heating to temperatures between 175°F and 250°F followed by simulated coil cooling on yield strength both before and after a simulated paintbake treatment;
Figure 6 is a graph showing the effect of rapid heating and simulated coil cooling on yield strength and paintbake response; and
Figure 7 is a graph showing the effect of rapid heating and simulated coil cooling on the total elongation and uniform elongation. Description of the Preferred Embodiments
The inventive method and apparatus are effective at significantly improving the strength of Al-Mg-Si and Al-Mg- Si-Cu- type aluminum alloy autobody sheet, while simultaneously improving its formability and stamping performance. Use of the inventive processing method on these types of aluminum alloy sheet products enhances the artificial aging response obtained during the standard automotive paintbake cycles by up to 4-fold. In the present invention, the aluminum sheet is subjected to rapid heating to a pre-aging temperature following the standard solution heating and quenching and prior to sheet coiling. The pre-aging temperature is defined as that temperature which does not cause excessive aging and increased T4 yield strength while still providing a significant paintbake response, resistance to natural aging and improved formability. Preferably, the pre-aging temperature is between 150° and 250°F. The heating rate is such that the material being continuously and rapidly treated is brought up to the pre-aging temperature substantially instantaneously, i.e. without any ramping or other slow heat up. The heating occurs as soon as possible after the application of the quench which follows solution heat treatment. The aluminum is then coiled and allowed to cool as a coiled product without the necessity of additional furnace treatments. The natural cooling of the coil, usually on a plant floor, provides for an acceptable pre-aging treatment which avoids the need for subsequent re-heating and is subject to only minimal losses in performance due to the phenomenon of dwell time decay.
The method described provides distinct advantages over the standard practice and over batch pre-aging strategies discussed above. The most significant advantages are: Paintbake response can be increased from the standard 2 ksi to 14 ksi; Natural aging in the product is suspended; Formability of the product is increased. The application of the continuous pre-age cycle offers a method to produce an aluminum sheet product with improved dent resistance, greater stability for consistency of stamping and superior stamping performance. The processing method avoids additional metal handling, and thus promises to be a low cost method to improve product performance and reduce product variability. A schematic diagram showing one embodiment of a coil pre-aging apparatus is shown in Figure 3. In this apparatus, a freshly quenched alloy 6111 sheet 1 exiting the accumulator 3 at the exit of a continuous heat treater (CHT) 5 is re¬ heated to a temperature of between 150°F and 250°F usmg an induction heater 7. Figure 3 also shows a leveler 9 downstream of the CHT 5 and an exit accumulator 3 disposed between the leveler 9 and the induction heater 7.
After the sheet 1 is pre-aged by the induction heater 7, it is coiled into coil form 13 for subsequent processing.
It should be understood that the induction heater 7 is a preferred device for rapidly heating the solution heat treated and quenched sheet 1 prior to formation of the coil form 13. Any means for this rapid heating can be utilized accordine; to the invention. The rapid heating means is designed to rapidly heat the sheet 1 to a target pre-age temperature.
The following provides an exemplary calculation to determine the power requirement or heating rate ;:or a rapid heating means based on a target pre-aging temperature of 250°F, a specified line speed, a specified entry temperature and a specified size and type for the sheet to be rapidly heated. Of course, the power requirement may vary depending on the particular variables selected.
The theoretical power requirements for such a unit were calculated based on a line speed of 100 fpm, a 75°F entry temperature, a 250°F exit temperature, a sheet thickness of 0.041", a width of 72" and the physical properties of AA 6111 alloy. This calculation results in an estimated power requirement of 280 kW, a power requirement which is well within standard industrial capabilities.
To further demonstrate the improvements associated with the inventive apparatus and method, test work was performed with respect to paintbake response, natural aging resistance and improved formability. The tests described below further explain the ambient cooling rates used in conjunction with the rapid heating pre-aging treatment, as well as the enhanced physical properties achieved by the invention. It should be understood that the experiments described below are only exemplary of the invention and the invention is not so limited.
Using empirical data from plant trials and laboratory tests, experiments were conducted which investigated the natural cooling rate of metal coils on a plant floor to apply a low cost pre-aging treatment. In these experiments, the effect of changes in the time-temperature profile of the pre- aging treatment on paintbake response and T4 properties were studied.
These experiments also simulated reheating freshly quenched (6111-W[2 min.]) autobody sheet to a relatively low temperature (less than 250°F) immediately before it was coiled at the exit end of the CHT. The thermal mass of the coil dictates that the cooling down to room temperature will be governed by classical Newtonian cooling. From empirical data as shown in Fig. 4, this cooling rate is surprisingly slow.
In Figure 4, a coil cooling curve for aluminum is shown. In this specific case, the data were taken from points within the wraps of a 72" wide coil of AA 6111-F (0.037" cold rolled) . Several important points are worth noting:
1. Cooling rates near the outer wraps and near the center of the coil are nearly the same. This implies that cooling occurs largely through the sheet ends (axially) rather than through the surface of the outer wraps (radially) , as would be expected given the relative heat transfer coefficients of aluminum and alumina/air/oil barriers .
2. Below 250°F, the cooling rate drops significantly. Though the cooling rate is logarithmic, it can be closely approximated as linear at 3°F/hour. Based on the empirical data on coil cooling, laboratory furnaces were programmed to simulate the low temperature end of the cooling curve and impose this declining temperature profile on freshly quenched AA 6111-W. A dwell time of 2 minutes was selected, as this best approximates the time required for the metal to thread through the CHT leveler 9 and the accumulator 11 (See Fig. 3) . Using a 3°F/hour cooling rate, five starting temperatures were tested: 250°F, 225°F, 200°F, 175°F, 150°F. Cooling times to ambient temperature were 57, 48, 40, 32 and 23 hours, respectively. A representation of these five cooling paths is also given in Figure .
Following the rapid heating pre-aging treatment, samples were allowed an additional 10 days of natural aging (T4 treatment) and then specimens were taken for tensile examination and to prepare foil for transmission electron microscopy. Half of the specimens were given a standard paintbake simulation (350°F/30 min.) and half were tested the as pre-aged + 10 days natural aged condition. The tensile yield strength, both before and after simulated paintbake cycles, is shown in Figure 5 for the five starting temperatures of the coil cooling simulation. From these data it can be concluded:
1. A starting temperature between 200°F and 225°F appears optimum. Temperatures above 225°F while providing a good PBR appear to cause premature aging
(increased T4 yield strength), and temperatures below this range begin to reduce the paintbake response. 2. For the specimens given a 200°F starting temperature, a 14.4 ksi PBR was achieved. This should be contrasted with the 2 ksi PBR in standard AA 6111-T4 and a 9 ksi response seen in AA 6111 given a "square wave" pre-age cycle at 212°F for 24 hours after a 2 hour dwell time.
Thus, by rapidly heating a solution heat treated and quenched aluminum alloy sheet prior to coiling, significant paintbake response is achieved, together with improved stamping performance due to the reduction in T4 yield strength.
Referring now to Figures 6 and 7, the effect of natural aging time on AA 6111 aluminum alloys previously subjected to the inventive pre-aging practice is shown. Referring specifically to Figure 6, the T4 aluminum alloy sheet prior to paint baking shows a relatively flat curve for yield strength over 60 days. What this means is that, by pre-aging according to the invention, resistance to natural aging is increased. Thus, the aluminum sheet does not exhibit the typical yield strength increase in T4 yield strength, i.e. one or two ksi, which can adversely affect stamping performance. The T4 yield strength is also lowered, reducing the problem of springback that is common with automotive aluminum stampings. Figure 6 also reaffirms the significant paintbake response achieved when the aluminum sheet is pre-aged according to the invention, even after 60 days of natural aging time. Referring now to Figure 7, quite surprisingly along with improved paintbake response, aluminum sheet subjected to the inventive processing also exhibits significant improvements in T4 total elongation and uniform elongation. The curves noted in Figure 7 as measuring elongation show significant improvements over the standard unleveled T4 elongation of 24%. Using a 200°F start temperature and 60 days of natural aging time, a 4% increase over the prior art standard is realized (28%) . Concerning uniform elongation, typically, this value for a -standard AA 6111 - T4 alloy is about 18%. When using the inventive processing, uniform elongation is vastly improved, extending up to 23% for a pre-aging temperature of 200°F. In summary, the data discussed above incicate that superior stability and PBR are achieved when practicing the invention, particularly when using a 3°F per hour ambient cooling rate from a 200°F pre-aging temperature. Tensile tests performed on samples prior to the application of a paintbake cycle indicate that elongation to failure which closely parallels formability and stamping performance is increased up to 28%, a full 4% improvement over standard AA 6111 - T4 aluminum alloy elongation. Similarly, uniform elongation is also improved when practicing the invention. In addition, a paintbake response far exceeding the normal 2 ksi is achieved when rapidly heating an aluminum sheet directly after continuous heat treatment and quenching and ambiently cooling the coil. In conjunction with these improvements, the aluminum sheet also shows resistance to natural aging by not showing an increase in yield strength over time. This aging resistance is significant since increases in yield strength over time can adversely effect stamping performance. As such, an invention has been disclosed in terms of preferred embodiments thereof which fulfill each and every one of the objects of the present invention as set forth above and provides a new and improved method and apparatus for making aluminum alloy sheet product for vehicle component use. Of course, various changes, modifications and alterations from the teachings of the present invention may be contemplated by those skilled in the art without departing from the intended spirit and scope thereof. Accordingly, it is intended that the present invention only be limited by the terms of the appended claims.

Claims

What is claimed is:
1. In a method of making a Mg-Si containing aluminum alloy sheet product from an aluminum alloy having magnesium and silicon as alloying elements which comprises the steps of providing an Al-Mg-Si-contam g aluminum alloy, subjecting said aluminum alloy to hot rolling and subsequent cold rolling to form a cold rolled sheet product, and further subjecting said cold rolled sheet product to continuous solution heat treating, quenching and coiling to provide said sheet product in coil form, the improvement comprising: a) continuously rapidly heating said sheet product to a pre-aging temperature after said continuous quenching step and prior to said continuous coiling step; and b) ambient cooling said sheet in coil form from said pre-aging temperature to ambient temperature, said heating and ambient cooling improving paintbake response of said aluminum alloy sheet product.
2. The method of claim 1 wherein said pre-aging temperature is between about 150° and 250°F.
3. The method of claim 2 wherein said pre-aging temperature is between about 175° and 225°F.
4. The method of claim 3 wherein said pre-aging temperature is about 200°F.
5. The method of claim 1 wherein the ambient cooling is at a cooling rate of between about 2 and 6°F per hour.
6. The method of claim 1 wherein said heating is by induction heating.
7. The method of claim 1 further comprising the step of leveling said sheet product after said quenching step and prior to said heating step.
8. The method claim 1 wherein said coil form is uncoiled and subjected to stamping to form a vehicle component part.
9. The method of claim 8 wherein said vehicle component part is heated as part of a painting cycle.
10. The method of claim 5 wherein said cooling rate is about 3°F per hour.
11. The method of claim 1 wherein a time between an end of said continuous quenching and said heating is less than about 5 minutes.
12. In an apparatus for making an Mg-Si containing aluminum alloy sheet product comprising means for continuously solution heat treating, quenching and coiling a cold rolled Mg-Si containing aluminum alloy sheet product to provide said sheet product in coil form, the improvement comprising means for improving paintbake response of said aluminum alloy sheet product, said means for improving comprising means for continuously rapidly heating said sheet product to a pre-aging temperature, said heating means being disposed between said means for continuous quenching and said means for coiling so that said sheet product ambiently cools in coil form from said pre-aging temperature to ambient temperature.
13. The apparatus of claim 12 wherein said means for heating is an induction heater.
14. The apparatus of claim 12 further comprising a leveler disposed between said means for continuous quenching and said means for heating.
15. The apparatus of claim 14 further comprising an exit accumulator disposed between the leveler and the means for heating.
16. The method of claim 1 wherein said pre-aging and ambient cooling steps improve stamping performance by increasing formability and further improve resistance to natural aging prior to forming of said sheet product.
17. The method of claim 1 wherein said Al-Mg-Si- containing aluminum alloy is an AA 6000 series aluminum alloy.
18. A sheet product made by the method of claim 1.
19. A sheet product made by the method of claim 3,
20. A sheet product made by the method of claim 8,
PCT/US1996/019878 1995-12-18 1996-12-17 Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom WO1997022724A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE69628044T DE69628044T2 (en) 1995-12-18 1996-12-17 METHOD AND DEVICE FOR INCREASING THE HEAT RESISTANCE AND AGING STABILITY OF ALUMINUM SHEETS AND PRODUCTS MADE THEREOF
EP96944361A EP0874917B1 (en) 1995-12-18 1996-12-17 Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom
JP9522922A JP2000503069A (en) 1995-12-18 1996-12-17 Method and apparatus for improving paint baking reaction and aging stability of aluminum sheet material and product thereof

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/573,895 US5718780A (en) 1995-12-18 1995-12-18 Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom
US08/573,895 1995-12-18

Publications (1)

Publication Number Publication Date
WO1997022724A1 true WO1997022724A1 (en) 1997-06-26

Family

ID=24293816

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1996/019878 WO1997022724A1 (en) 1995-12-18 1996-12-17 Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom

Country Status (6)

Country Link
US (1) US5718780A (en)
EP (1) EP0874917B1 (en)
JP (1) JP2000503069A (en)
CA (1) CA2240441A1 (en)
DE (1) DE69628044T2 (en)
WO (1) WO1997022724A1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009135244A1 (en) * 2008-05-09 2009-11-12 Amag Rolling Gmbh Method for heat treating a rolling stock made of a heat-treatable aluminum alloy
US7666267B2 (en) 2003-04-10 2010-02-23 Aleris Aluminum Koblenz Gmbh Al-Zn-Mg-Cu alloy with improved damage tolerance-strength combination properties
WO2011000635A1 (en) * 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
WO2012059419A1 (en) 2010-11-05 2012-05-10 Aleris Aluminum Duffel Bvba Formed automotive part made from an aluminium alloy product and method of its manufacture
EP2687616A1 (en) * 2011-03-15 2014-01-22 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Aluminum alloy plate having superior baking finish hardening
EP3409811A1 (en) * 2017-05-29 2018-12-05 Andritz AG Method for controlling the coiling temperature of a metal strip
US10472707B2 (en) 2003-04-10 2019-11-12 Aleris Rolled Products Germany Gmbh Al—Zn—Mg—Cu alloy with improved damage tolerance-strength combination properties
CN114959386A (en) * 2022-05-30 2022-08-30 中国第一汽车股份有限公司 Aluminum alloy with rapid aging response and heat treatment process thereof
US11578921B2 (en) 2018-01-16 2023-02-14 Ebner Industrieofenbau Gmbh Continuous furnace for aluminum strips

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT408763B (en) * 2000-09-14 2002-03-25 Aluminium Ranshofen Walzwerk G ALUMINUM ALLOY EXHAUST HARDNESS
US6679417B2 (en) * 2001-05-04 2004-01-20 Tower Automotive Technology Products, Inc. Tailored solutionizing of aluminum sheets
JP4708555B2 (en) * 2000-12-13 2011-06-22 株式会社神戸製鋼所 Continuous solution quenching method for rolled aluminum alloy sheets with excellent formability and flatness
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
US20060032560A1 (en) * 2003-10-29 2006-02-16 Corus Aluminium Walzprodukte Gmbh Method for producing a high damage tolerant aluminium alloy
WO2006005573A1 (en) * 2004-07-09 2006-01-19 Corus Aluminium Nv Process for producing aluminium alloy sheet material with improved bake-hardening response
US7491278B2 (en) * 2004-10-05 2009-02-17 Aleris Aluminum Koblenz Gmbh Method of heat treating an aluminium alloy member and apparatus therefor
US7883591B2 (en) * 2004-10-05 2011-02-08 Aleris Aluminum Koblenz Gmbh High-strength, high toughness Al-Zn alloy product and method for producing such product
FR2907796B1 (en) * 2006-07-07 2011-06-10 Aleris Aluminum Koblenz Gmbh ALUMINUM ALLOY PRODUCTS OF THE AA7000 SERIES AND METHOD FOR MANUFACTURING THE SAME
US8088234B2 (en) * 2006-07-07 2012-01-03 Aleris Aluminum Koblenz Gmbh AA2000-series aluminum alloy products and a method of manufacturing thereof
US8663405B2 (en) * 2011-01-24 2014-03-04 GM Global Technology Operations LLC Stamping of age-hardenable aluminum alloy sheets
WO2014135367A1 (en) * 2013-03-07 2014-09-12 Aleris Aluminum Duffel Bvba Method of manufacturing an al-mg-si alloy rolled sheet product with excellent formability
CN103695820B (en) * 2013-12-28 2015-11-25 无锡透平叶片有限公司 A kind of forging of 7050 aluminium alloys and heat-treatment technology method
JP6894849B2 (en) * 2015-05-29 2021-06-30 アーコニック テクノロジーズ エルエルシーArconic Technologies Llc New 6xxx Aluminum Alloy Manufacturing Method
US10030295B1 (en) 2017-06-29 2018-07-24 Arconic Inc. 6xxx aluminum alloy sheet products and methods for making the same
CA3070003A1 (en) * 2017-08-29 2019-03-07 Novelis Inc. 7xxx series aluminum alloy products in a stabilized t4 temper and methods of making the same
KR102201131B1 (en) * 2018-04-24 2021-01-12 한국생산기술연구원 Heat treatment method of Al-Mg-Si alloy
WO2019209015A1 (en) * 2018-04-24 2019-10-31 한국생산기술연구원 Heat treatment method for al-mg-si alloy

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3135633A (en) * 1959-09-08 1964-06-02 Duralumin Heat treatment process improving the mechanical properties of aluminiummagnesium-silicon alloys
US4282044A (en) * 1978-08-04 1981-08-04 Coors Container Company Method of recycling aluminum scrap into sheet material for aluminum containers
US4838958A (en) * 1986-09-09 1989-06-13 Sky Aluminum Co., Ltd. Aluminum-alloy rolled sheet and production method therefor
US4840852A (en) * 1985-11-04 1989-06-20 Aluminum Company Of America Aluminum alloy vehicular member
US5362341A (en) * 1993-01-13 1994-11-08 Aluminum Company Of America Method of producing aluminum can sheet having high strength and low earing characteristics
US5441582A (en) * 1993-09-30 1995-08-15 Nkk Corporation Method of manufacturing natural aging-retardated aluminum alloy sheet exhibiting excellent formability and excellent bake hardenability

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3947297A (en) * 1973-04-18 1976-03-30 The United States Of America As Represented By The Secretary Of The Air Force Treatment of aluminum alloys
FR2435535A1 (en) * 1978-09-08 1980-04-04 Cegedur PROCESS FOR THE HEAT TREATMENT OF ALUMINUM, COPPER, MAGNESIUM, SILICON ALLOYS
US4614552A (en) * 1983-10-06 1986-09-30 Alcan International Limited Aluminum alloy sheet product
JPS62142753A (en) * 1985-12-16 1987-06-26 Showa Alum Corp Heat treatment of 7000 type aluminum alloy
US4808247A (en) * 1986-02-21 1989-02-28 Sky Aluminium Co., Ltd. Production process for aluminum-alloy rolled sheet
US4812178A (en) * 1986-12-05 1989-03-14 Bruno Dubost Method of heat treatment of Al-based alloys containing Li and the product obtained by the method
US4790884A (en) * 1987-03-02 1988-12-13 Aluminum Company Of America Aluminum-lithium flat rolled product and method of making
US4897124A (en) * 1987-07-02 1990-01-30 Sky Aluminium Co., Ltd. Aluminum-alloy rolled sheet for forming and production method therefor
JPH0674480B2 (en) * 1987-09-03 1994-09-21 本田技研工業株式会社 Forming and welding alloy sheet excellent in weldability, rust resistance, formability and bake hardenability, and method for producing the same
JP2764176B2 (en) 1989-02-09 1998-06-11 株式会社神戸製鋼所 Continuous annealing furnace incorporating reheating device
DE69107392T2 (en) 1990-10-09 1995-06-08 Sumitomo Light Metal Ind Process for producing a material from an aluminum alloy with excellent press formability and baking hardenability.
ZA925491B (en) * 1991-07-23 1993-03-05 Alcan Int Ltd Aluminum alloy.
JPH05302154A (en) * 1992-04-27 1993-11-16 Furukawa Electric Co Ltd:The Method for heat-treating al-mg-si aluminum alloy sheet
JP2614686B2 (en) * 1992-06-30 1997-05-28 住友軽金属工業株式会社 Manufacturing method of aluminum alloy for forming process excellent in shape freezing property and paint bake hardenability
JPH0665695A (en) * 1992-08-17 1994-03-08 Furukawa Electric Co Ltd:The Heat treatment method of al-mg-si aluminum alloy forged material
JP2997145B2 (en) * 1993-03-03 2000-01-11 日本鋼管株式会社 Method for producing aluminum alloy sheet having delayed aging at room temperature
JPH06272002A (en) 1993-03-19 1994-09-27 Furukawa Alum Co Ltd Production of al-mg-si series alloy metal plate high in curing performance for baking

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3135633A (en) * 1959-09-08 1964-06-02 Duralumin Heat treatment process improving the mechanical properties of aluminiummagnesium-silicon alloys
US4282044A (en) * 1978-08-04 1981-08-04 Coors Container Company Method of recycling aluminum scrap into sheet material for aluminum containers
US4840852A (en) * 1985-11-04 1989-06-20 Aluminum Company Of America Aluminum alloy vehicular member
US4838958A (en) * 1986-09-09 1989-06-13 Sky Aluminum Co., Ltd. Aluminum-alloy rolled sheet and production method therefor
US5362341A (en) * 1993-01-13 1994-11-08 Aluminum Company Of America Method of producing aluminum can sheet having high strength and low earing characteristics
US5441582A (en) * 1993-09-30 1995-08-15 Nkk Corporation Method of manufacturing natural aging-retardated aluminum alloy sheet exhibiting excellent formability and excellent bake hardenability

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP0874917A4 *

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7666267B2 (en) 2003-04-10 2010-02-23 Aleris Aluminum Koblenz Gmbh Al-Zn-Mg-Cu alloy with improved damage tolerance-strength combination properties
US10472707B2 (en) 2003-04-10 2019-11-12 Aleris Rolled Products Germany Gmbh Al—Zn—Mg—Cu alloy with improved damage tolerance-strength combination properties
WO2009135244A1 (en) * 2008-05-09 2009-11-12 Amag Rolling Gmbh Method for heat treating a rolling stock made of a heat-treatable aluminum alloy
US10047422B2 (en) 2009-06-30 2018-08-14 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
WO2011000635A1 (en) * 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
US10612115B2 (en) 2009-06-30 2020-04-07 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
DE112011103667T5 (en) 2010-11-05 2013-08-01 Aleris Aluminum Duffel Bvba Automobile molding of aluminum alloy product and process for its production
US9254879B2 (en) 2010-11-05 2016-02-09 Aleris Aluminum Duffel Bvba Formed automotive part made from an aluminium alloy product and method of its manufacture
WO2012059419A1 (en) 2010-11-05 2012-05-10 Aleris Aluminum Duffel Bvba Formed automotive part made from an aluminium alloy product and method of its manufacture
US9399808B2 (en) 2011-03-15 2016-07-26 Kobe Steel, Ltd. Aluminum alloy sheet excellent in baking finish hardenability
EP2687616A4 (en) * 2011-03-15 2014-10-22 Kobe Steel Ltd Aluminum alloy plate having superior baking finish hardening
EP2687616A1 (en) * 2011-03-15 2014-01-22 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Aluminum alloy plate having superior baking finish hardening
EP3409811A1 (en) * 2017-05-29 2018-12-05 Andritz AG Method for controlling the coiling temperature of a metal strip
US11578921B2 (en) 2018-01-16 2023-02-14 Ebner Industrieofenbau Gmbh Continuous furnace for aluminum strips
CN114959386A (en) * 2022-05-30 2022-08-30 中国第一汽车股份有限公司 Aluminum alloy with rapid aging response and heat treatment process thereof
CN114959386B (en) * 2022-05-30 2022-11-15 中国第一汽车股份有限公司 Aluminum alloy with rapid aging response and heat treatment process thereof

Also Published As

Publication number Publication date
EP0874917A4 (en) 1999-08-11
JP2000503069A (en) 2000-03-14
US5718780A (en) 1998-02-17
DE69628044T2 (en) 2004-03-25
DE69628044D1 (en) 2003-06-12
EP0874917A1 (en) 1998-11-04
EP0874917B1 (en) 2003-05-07
CA2240441A1 (en) 1997-06-26

Similar Documents

Publication Publication Date Title
US5718780A (en) Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom
KR100374104B1 (en) Heat treatment process for aluminum alloy sheet
JP5815947B2 (en) How to produce a coating on a steel strip
US4151013A (en) Aluminum-magnesium alloys sheet exhibiting improved properties for forming and method aspects of producing such sheet
JP2019173176A (en) Aluminum sheet for automobile having reduced or no surface roping and capable of being molded at high level, and manufacturing method therefor
KR102639005B1 (en) New 6xxx aluminum alloy and its manufacturing method
CN103146969A (en) High strength al-zn alloy and method for producing such an alloy product
WO2020182506A1 (en) Method of manufacturing a 5xxx-series sheet product
AU2017375790B2 (en) Aluminum alloys and methods of making the same
US4200476A (en) Process for the thermal treatment of thick products made of copper-containing aluminum alloys of the 7000 series
EP1190109B1 (en) Heat treatment of formed aluminum alloy products
EP0761837A1 (en) Method of producing aluminum alloys having superplastic properties
JP2004527658A (en) Method of manufacturing aluminum alloy sheet with improved bending characteristics and aluminum alloy sheet manufactured by the method
WO1998014626A1 (en) Aluminium alloy for rolled product process
CA2111706C (en) Improved aluminium alloy
US3966506A (en) Aluminum alloy sheet and process therefor
WO2000003052A1 (en) Process for producing heat-treatable sheet articles
US4528042A (en) Method for producing superplastic aluminum alloys
US4579603A (en) Controlling distortion in processed copper beryllium alloys
JP2004204352A (en) Crash resistant aluminum alloy sheet product and its manufacturing method
US4294632A (en) Method for overaging of hot dip metal coated steel material
US4591395A (en) Method of heat treating low carbon steel strip
JPS6487752A (en) Manufacture of aluminum alloy material for forming
JP2871731B2 (en) Aluminum alloy material for forming and its manufacturing method
JPS61204332A (en) Production of metal hot dipped thin steel sheet having excellent ridging resistance and plating adhesiveness

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): CA JP

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
ENP Entry into the national phase

Ref document number: 2240441

Country of ref document: CA

Ref country code: CA

Ref document number: 2240441

Kind code of ref document: A

Format of ref document f/p: F

WWE Wipo information: entry into national phase

Ref document number: 1996944361

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 1996944361

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1996944361

Country of ref document: EP