Assembly and method of pretreating localized areas of parts for joining

Abstract

An assembly and a method of joining a first part with a second part at an attachment area that includes a localized area on the first part. The localized area is cleaned and activated by a plasma jet. An organosilicon composition is applied by plasma-enhanced chemical vapor deposition to the localized area. An adhesive is applied to the localized area and the second part is mechanically fastened to the first part in the localized area.

Claims

1. An assembly comprising: a first part; a plasma-enhanced vapor deposition film coating of an organosilicon composition applied to localized areas on the first part; a layer of adhesive applied to the film coating; a second part assembled to the first part; and a mechanical joint connecting the first part to the second part with the film coating and layer of adhesive disposed between the first part and the second part.

2. The assembly of claim 1 wherein the plasma-enhanced vapor deposition film coating is a hexamethyldisiloxane film.

3. The assembly of claim 2 wherein the hexamethyldisiloxane film includes exposed OH groups that bond with the layer of adhesive.

4. The assembly of claim 1 wherein the mechanical joint is a self-piercing rivet.

5. The assembly of claim 1 wherein the plasma-enhanced vapor deposition film coating is applied to localized areas on the second part, and wherein the layer of adhesive is bonded to the film coating on the first part and the second part.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a flowchart showing a method of joining metal components together.

(2) FIG. 2 is a front schematic cross-sectional view of a plasma generator that may be used in the method of FIG. 1.

(3) FIG. 3 is an illustration of a chemical transformation occurring on a surface of a metal component when executing the steps of the method of FIG. 1.

(4) FIG. 4 is a perspective view of a plasma jet directed toward a first metal component having a localized area for cleaning, activating, and then coating with a polymer coating.

(5) FIG. 5 is a perspective view of the first metal component of FIG. 4 showing adhesives being applied to the localized areas.

(6) FIG. 6 is a perspective view of a second metal component being secured to the first metal component of FIG. 5 at the localized areas using self-piercing rivets.

(7) FIG. 7 is a cross-section view taken from lines 7-7 in FIG. 6 showing the adhesive reinforcing the joint by the fastener to secure the first part to the second part.

(8) FIG. 8 is an electron diffraction spectrograph showing the presence of the polymer coating between the first and second metal components.

(9) FIGS. 8A-8C are spectrogram of Spectrums 20-22 in FIG. 8.

DETAILED DESCRIPTION

(10) The illustrated embodiments are disclosed with reference to the drawings. However, it is to be understood that the disclosed embodiments are intended to be merely examples that may be embodied in various and alternative forms. The figures are not necessarily to scale and some features may be exaggerated or minimized to show details of particular components. 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.

(11) The metal parts described in this disclosure may be alternative parts formed of different metals or composite materials. The metal components may also be made by casting, extrusion, sheet metal forming, or other processes. Examples of assemblies that may be made with the disclosed method include, but are not limited to, shock tower assemblies, rail/sledge runner transitions, front ends, and other automotive body structures.

(12) Referring to FIG. 1, flowchart 20 shows the steps of a method of assembling component parts of a vehicle. At step 22, one or more localized areas are identified on a first part that is to be assembled to a second part. As used herein, the term localized area should be interpreted as less than 25% of the surface area of the part. At step 24, atmospheric pressure plasma is directed to the localized areas to clean the areas to activate and clean the surface of the part. Cleaning and activating the localized areas improves bonding with paints, coatings, or adhesives applied to the parts in the localized areas. At step 26, a pretreatment coating, for example an organosilicon compound, is applied to the localized areas by plasma enhanced chemical vapor deposition. The pretreatment coating may be formed by combining a precursor gas with plasma. The precursor gas may be a gaseous form of hexamethyldisiloxane (HMDSO). After reacting chemically with plasma, the HMDSO becomes a plasma-polymerized silane coating that serves as an adhesion promoter for adhesive bonding and may add local corrosion protection. At step 28, an adhesive is applied to the localized areas. At step 30, a second part is mechanically attached to the first part at the localized areas to mechanically fasten the second part to the first part with self-piercing rivets, clinch joints or threaded fasteners. At step 34, the joined parts are assembled to the vehicle.

(13) Referring to FIG. 2, a plasma generator 40 is diagrammatically illustrated that may be used to discharge plasma in steps 24 and 26 of the method of FIG. 1. The plasma generator 40 includes a housing 42 having an insulation layer 43. The housing receives a process gas, for example, compressed air, through a gas inlet 42. A voltage supply 46 is connected to a high voltage source to generate an electric arc. An electrode 44 disposed in the housing 41 is connected to the high voltage supply 46. Compressed air is continuously injected through the gas inlet 42 and is ionized by the electric arc created by the electrode 44 to produce plasma 47. The plasma 47 is directed to a discharge area 48 of the housing 41 where the plasma rotates at high potential. The housing 41 defines a plasma nozzle 50 that directs the plasma jet toward a desired treatment location. A precursor gas inlet 54 is provided that opens into the plasma nozzle 50.

(14) The precursor gas inlet 54 is closed when the localized plasma cleaning area is cleaned at step 24. The plasma nozzle 50 directs plasma 47 toward the part and activates and cleans the surface of the part 56 in the localized area. The cleaned and activated surface promotes adhesion of coatings, adhesives and paints.

(15) At step 26, the precursor gas inlet 54 is opened and precursor gas, such as HMDSO, reacts with the plasma 47 to form a polymerized silane coating. The polymerized silane coating is discharged through the nozzle 50 and is directed to the localized area of the part 56. The polymerized silane coating forms a thin film on the part 56. Adhesives used in the joining process durably bond to the film. The film may also serve as an anti-corrosion coating.

(16) Referring to FIG. 3, a diagram 58 is provided of the chemical reaction between the HMDSO and plasma. The thin film of polymerized silane coating has highly reactive exposed OH groups 49 that promote bonding with the adhesives or coatings that are applied to the film.

(17) Referring to FIG. 4, a part 56 is shown after undergoing the plasma cleaning step 24 and coating step 26. The localized areas are identified by reference numerals 60 and 62. The plasma nozzle 50 of the plasma generator 40 is shown being directed to the localized area 60. The plasma generator 40 is preferably located on-line in the assembly facility where the parts are joined as sub-assemblies because surface activation created by the plasma may decrease over time.

(18) Referring to FIGS. 5 and 6, an adhesive 64 is shown applied to localized areas 60 and 62. The joining adhesive 64 cooperates with fasteners 68, such as self-piercing rivets, to join the first part 56 to a second part 66, as shown in FIG. 6. The fasteners 68 mechanically fasten the first part 56 to the second part 66 at the localized areas 60 and 62 of the first part 56.

(19) Referring to FIG. 7, a cross-section view is provided of the parts 58 and 66 joined by the self-piercing rivet 68 and adhesive 64. The self-piercing rivet 68 is driven through the second part 66 and into the first part 56, as shown. The rivet 68 may also be inserted in the opposite way. The fastening adhesive 64 is squeezed between the parts 56 and 58 to increase the strength of the joint between the parts. The polymerized silane film on the first part or the second part is not visible in FIG. 7.

(20) FIG. 8 is an electron diffraction spectrograph of a portion of the first part at one of the localized areas. The adhesive composition is shown as Spectrum 20 and the composition of the adhesive is shown in the spectrogram shown in FIG. 8A. The thin film of polymerized silane coating 70 adhering to the first part 56 is evidenced by the enhanced silicon (Si) deposit seen at Spectrum 21 is shown in the spectrogram shown in FIG. 8B. The composition of the metal alloy of the first part 56 is shown as Spectrum 22 is shown in the spectrogram shown in FIG. 8C. This spectrographic analysis establishes that a thin film of enhanced silicon 70 remains between the first part and the adhesive after assembling the parts together.

(21) 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.