Patent Application
20140305371
This disclosure relates to a method of manufacturing and preparing aluminum body panels and other parts that use adhesives and sealants that are painted after application of a conversion coating.
Corrosion of aluminum alloys on vehicles is a complex and costly issue for vehicle manufacturers. Aluminum corrosion is generally associated with joints between parts, hem flanges and trimmed edges. As more aluminum is used in vehicle designs the potential for greater aluminum corrosion is an increasingly important issue. The root cause of aluminum corrosion is complex but is believed to relate to five key elements: surface finishing, paint shop-applied pretreatment, aluminum alloy chemistry, the presence or absence of a sealer, and craftsmanship (placement of adhesive, inner/outer overlap, inner/outer gap, burr size and orientation). All of the above elements must be addressed to achieve superior aluminum corrosion performance.
Manufacturing materials and processes are not solely optimized to provide the best aluminum corrosion performance. New vehicle designs are trending towards deeper draws and stronger alloys that necessitate the need for improved forming manufacturing methods and materials. Aluminum vehicles depend on substantial amounts of structural adhesive that is applied to parts being joined to provide the vehicle with the necessary strength and rigidity to improve noise, vibration and harshness (NVH) performance. The interaction between the aluminum surface, the forming lubes, and the adhesive must be balanced to provide an effective manufacturing process.
All aluminum surfaces normally have a native oxide/hydroxide layer due to the reactive nature of aluminum. The native oxide/hydroxide layer forms very rapidly when the aluminum is exposed to air. This reaction is self-passivating and results in a thin oxide/hydroxide layer. When pretreating an aluminum coil, an alkaline and/or acid etch is performed to remove the native oxide/hydroxide layer. A thin film pretreatment layer (such as Alcoa 951 a trademarked product of Alcoa Aluminum for a vinyl phosphonic/phosphinic acid, polyacrylate solution) may be applied to the newly etched surface. Some of the native oxide/hydroxide layer may reform on the surface before the Alcoa 951 is applied which is then modified by the Alcoa 951 pretreatment.
The general problem addressed is how to deliver superior formability, adhesive bond durability, and corrosion performance on an aluminum vehicle at high production volumes.
The above problems and other problems are addressed by the disclosed method as summarized below.
According to one aspect of this disclosure, a method is provided for pretreating an aluminum assembly comprising selecting a blank having a thin film pretreatment functionalized coating (thin film pretreatment layer) and a lubricant coating applied to a surface of a coil prior to forming blanks into parts. The blank is formed to a desired shape and assembled with an adhesive or sealant being applied to a selected portion of the surface when the parts are joined. As used in this application the term “sealant” means an adhesive and is equivalent in that the sealant adheres to the surface like an adhesive. The assembly is cleaned with a cleaner including surfactants that is formulated to partially or completely remove the thin film pretreatment layer. The cleaner also substantially completely removes the lubricant coating from the surface except at the selected portion. A conversion coating is applied to the assembly as a final step prior to painting.
According to another aspect of this disclosure, a system is provided for pretreating a part formed from a blank that is coated with a thin film pretreatment layer and a lubricant coating. The part has an adhesive applied to a selected portion of the part, such as a hem flange joint, a structural adhesive joint, or a hem flange sealant. The system comprises a cleaner immersion tank for applying a cleaner to the part to remove the thin film pretreatment layer and the lubricant except where the adhesive or sealant is applied to the selected portion of the part. A series of other immersion tanks and spray tanks are provided for applying the conversion coating to the assembly.
According to other aspects of this disclosure relating to the disclosed method and system, the thin film pretreatment layer and the lubricant coating may be pre-applied to a coil that is cut to form the blanks that are formed into parts. The adhesive is applied to selected portions of the parts that are to be assembled and, in particular, to areas that receive a structural adhesive, hem flange adhesive, hem flange sealant, or the like. The selected portion may be two parts that are joined by a structural adhesive, a hem flange that receives hem flange adhesive, or a hem flange edge that is sealed with a hem flange sealant. The conversion coating may be a thin film zirconium oxide coating, or other type of conversion coating that is applied to promote paint adhesion and resist corrosion.
The above aspects of this disclosure and other aspects will be more fully described in the following detailed description.
The disclosed embodiments are intended to be merely examples that may be embodied in various and alternative forms. The specific structural and functional details disclosed are not to be interpreted as limiting, but as a representative basis for teaching one skilled in the art how to practice the disclosed concepts. The thickness of the thin film pretreatment layer, dry lubricant coating layer, adhesive deposits and sealant deposits are greatly exaggerated to be visible in the drawings.
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The thin film pretreatment layer 18 and the dry lubricant layer 20 are intact on the surfaces of the part 26 and the inner panel 36. An over-hem sealer 39, or hem flange sealant, may be applied to the hem flange 42 that covers the thin film pretreatment layer 18 and the dry lubricant layer 20 in the area indicated by reference numeral 44.
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A method of pretreating an aluminum part 26 is disclosed that begins with selecting a blank 24 having a thin film pretreatment layer 18 and a lubricant coating 20 applied to a surface. The thin film pretreatment layer 18 is applied to the coil 10 that is cut to form the blank 24. The dry lubricant 20 may also be applied to the coil 10 to facilitate forming the blank 24 in a conventional sheet metal forming production process. The blank 24 is formed into a part 26. An adhesive 38 may be applied to the surface to provide structural strength and rigidity. The adhesive 38 is bonded to a selected area 42 of the surface, such as a joining area. The part 26 may then be cleaned in a paint shop or other cleaning process to partially or fully remove the thin film pretreatment layer 18 and substantially remove the lubricant coating 20 from the surface except at the selected portion 28. A conversion coating 52 is applied to the part 26 before painting.
In one embodiment, the thin film pretreatment layer 18 is a thin film formed by the reaction of vinyl phosphonic/phosphinic acid pretreatment with the native oxide/hydroxide layer. The type of surface oxide layer is important for achieving good bonding performance. For example, the thin film pretreatment layer 18 may be Alcoa 951, or another coating made in accordance with U.S. Pat. No. 5,059,258. Alcoa 951 is a trademark of Aluminum Company of America. It should be noted that over etching the oxide prior to application of Alcoa 951 may result in poor bond durability. A silane based adhesion promoter may be applied to the surface of the aluminum coil 10 or blank 24. Mixed metal oxide conversion coatings, such as Ti/Zr oxide film pretreatments, or Trivalent Cr (Cr3+) conversion coatings may also be used.
The lubricant coating 20 may be a dry lubricant. In particular, the dry lubricant may be a dry lubricant that is a blend of mineral oil and paraffin wax. The lubricant coating 20 may be Quaker DryCote® 290. Quaker Drycote° is a trademark of Quaker Chemical Corporation. The composition of this dry lubricant is 30-40% by weight mineral oil, 30-40% paraffin wax (or hydrocarbon wax), 10-15% slack wax (petroleum), 1-5% calcium sulfonate, 1-5% ethoxylated alcohols c16-c18, and 1-5% sodium sulfonate.
The conversion coating 52 may be a thin film zirconium oxide coating. Other conversion coatings that may be used include zinc phosphate, a two-stop zinc phosphate, or similar conversion coatings.
A system is disclosed for pre-treating an aluminum part 26 formed from a blank 24 that is coated with an thin film pretreatment layer 18 and a lubricant coating 20, as previously described. The part 26 has an adhesive 38 applied to a selected portion 48 of the surface 44, such as at a structural joint or possibly a hem flange. The system comprises a cleaner immersion or spray tank 48 for applying a cleaner to the part to partially or fully remove the thin film pretreatment layer and the lubricant except at the portion 44 of the part 26 where the adhesive 38 is applied to the selected portion 48 of the surface 44. Next, a zirconium oxide conversion coating 52 is applied to the part 26 in subsequent immersion or spray tanks
Several examples of different combinations that were tested are described below:
An assembly including a blank of 6111 aluminum alloy was pre-treated with zirconium oxide paint pretreatment and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep averaged about 0.7 mm but the part failed formability and bond durability testing.
An assembly including a blank of 6111 aluminum alloy was pre-treated with a silane based adhesion promoter, dry lubricant Dry Cote 290, zirconium oxide paint pretreatment and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep was about 2.5 but failed bond durability testing.
EXAMPLE 3
An assembly including a blank of 6111 aluminum alloy was pre-treated with a coil applied adhesion promoter Alcoa-951 and dry lubricant DryCote 290 received zinc phosphate paint pretreatment and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep was about 4.0 and failed corrosion testing.
EXAMPLE 4
An assembly including a blank of 6111 aluminum alloy was pre-treated with dry lubricant DryCote 290 received zirconium oxide paint pretreatment and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep was about 2.2 but failed bond durability testing.
EXAMPLE 5
An assembly including a blank of 6111 aluminum alloy was pre-treated with a coil applied adhesion promoter Alcoa-951 and dry lubricant DryCote 290. A cleaner is applied to the assembly to remove the thin film pretreatment layer and the lubricant coating from the surface. The assembly received zirconium oxide paint pretreatment and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep was about 1.8 and passed all testing requirements for formability, bond durability, and corrosion resistance.
EXAMPLE 6
An assembly including a blank of 6111 aluminum alloy was pre-treated with a coil applied adhesion promoter Alcoa-951 and dry lubricant DryCote 290. The assembly received a two-step zinc phosphate paint pretreatment (or the DuPlex process) and painted. The blank was scribed and subjected to 6 weeks in an accelerated corrosion test. After the test the extent of scribe creep was about 1.6 and passed all testing requirements for formability, bond durability, and corrosion resistance. However, the two-stop zinc phosphate pretreatment that is intended for high aluminum content was determined to be not feasible for full 100% aluminum content production applications.
While exemplary embodiments are described above, it is not intended that these embodiments describe all possible forms of the disclosed apparatus and method. Rather, the words used in the specification are words of description rather than limitation, and it is understood that various changes may be made without departing from the spirit and scope of the disclosure as claimed. The features of various implementing embodiments may be combined to form further embodiments of the disclosed concepts.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 13751412 | Jan 2013 | US |
| Child | 14315644 | US |
