GB2141139A - Pretreatment of aluminium prior to bonding electroplating or painting - Google Patents

Pretreatment of aluminium prior to bonding electroplating or painting Download PDF

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Publication number
GB2141139A
GB2141139A GB08413731A GB8413731A GB2141139A GB 2141139 A GB2141139 A GB 2141139A GB 08413731 A GB08413731 A GB 08413731A GB 8413731 A GB8413731 A GB 8413731A GB 2141139 A GB2141139 A GB 2141139A
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GB
United Kingdom
Prior art keywords
acid
aluminium
anodising
etch
chromic
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.)
Granted
Application number
GB08413731A
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GB8413731D0 (en
GB2141139B (en
Inventor
Dr Andrew Winslow Clifford
Dr David John Arrowsmith
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UK Secretary of State for Defence
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UK Secretary of State for Defence
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
Priority claimed from GB838315203A external-priority patent/GB8315203D0/en
Application filed by UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB08413731A priority Critical patent/GB2141139B/en
Publication of GB8413731D0 publication Critical patent/GB8413731D0/en
Publication of GB2141139A publication Critical patent/GB2141139A/en
Application granted granted Critical
Publication of GB2141139B publication Critical patent/GB2141139B/en
Expired legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • C25D11/18After-treatment, e.g. pore-sealing
    • C25D11/24Chemical after-treatment
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/34Pretreatment of metallic surfaces to be electroplated
    • C25D5/42Pretreatment of metallic surfaces to be electroplated of light metals
    • C25D5/44Aluminium

Abstract

A method of surface pretreatment for aluminium or aluminium alloys before adhesive coating, electroplating or painting comprises a first anodising step using an acid selected to produce a dense- packed, thick-walled anodic oxide coating followed by an etching step to modify the outer surface of the oxide coating while leaving the inner part unaffected. The anodising acid may be sulphuric acid or chromic acid and the etch acid may be phosphoric acid, chromic acid or a mixture of sulphuric and chromic acids.

Description

SPECIFICATION Surface pretreatment of aluminium and aluminium alloys prior to adhesive bonding, electroplating or painting This invention relates to methods of improving adhesion to aluminium surfaces and to methods which give long term environmental stability of bonded aluminium. As used herein the word "aluminium" includes high purity aluminium, commercial purity aluminium and aluminium based alloys.
It is often desirable to coat aluminium with another material. These coatings may be organic coatings such as paint, lacquers, varnishes, or inorganic coatings such as vitreous enamel, glass, porcelain, magnetic ferrites, and refractory material. It is also often desir- able to bond materials such as plastics, foams or metals to aluminium with organic adhesives. In ail these applications it is desirable to treat the surface of the aluminium so that the coating material will adhere strongly to the aluminium.
Examples of important industrial applications include the structural bonding of metal to metal and composite type assembly widely used in the aircraft industry and increasingly used in the chemical engineering industry, in the automobile industry and in general engineering. Other examples include the powder painting of aluminium and the bonding of PTFE to aluminium to give low friction and non-stick surfaces.
Durability of the adhesive joint in service is important in most applications but particularly important in aircraft. Adhesively bonded joints in aircraft are exposed in service to a wide range of environmental conditions with ex- tremes of temperature from the arctic to the tropical sun and in humid, marine and other highly corrosive environments. To avoid failures of the aircraft structures as well as to meet the stringent requirements of military aircraft standards and the standards established by the aircraft industry for commercial passenger and cargo aircraft, bonded metal to metal and composite type assemblies must be able to withstand the environmental conditions to be encountered.Of particular importance is resistance to corrosion and disbonding of adhesively bonded joints in humid environments especially those laden with salt from sea spray or from deicing materials.
Faiiure of such joints frequently starts with diffusion of water through the adhesive followed by corrosion of the aluminium. To delay the onset of such corrosion, corrosion inhibitors may be incorporated in the adhesive or in a primer applied to the surface prior to the adhesive. Alternatively the aluminium may be pretreated in one of several ways. Various types of chemical conversion coatings (formed by processes such as chromating or phosphating) have been developed to give the pretreatment necessary for bonding to an aluminium substrate. Other pretreatments include anodizing to form relatively thick coatings of alumina. It is important that the alumina is not hydrated by water to form a weak layer of hydrated alumina which markedly reduces the strength of the joint and leads to premature failure. Hunter et al. (M.S. Hunter, P.F. Towner and D.L.Robinson, Proc. Amer. Electroplaters Soc 1959, 46, 220) compared the hydration rates of alumina formed in sulphuric, chromic, oxalic and phosphoric acids and found that the hydration rates of the first three were practically the same but alumina coatings formed in phosphoric acid hydrated at a slower rate than the others. They further found that alumina films that could be hydrated after boiling in water for about three minutes were not hydrated at all after boiling in dilute phosphoric acid or in a solution containing only nine parts per million of sodium dihydrogen orthophosphate.
The importance of this resistance to hydration was recognised by Marceau of the Boeing Aircraft Company who patented the use of phosphoric acid anodizing for providing environmentally stable aluminium surfaces for adhesive bonding (U.S. Patents 4, 085, 012, and 4, 127, 451). This process is incorporated in the Boeing Process Specification BAC 5555.
The oxide film produced on aluminium by phosphoric acid anodizing (PAA) is rougher and has larger diameter pores than that produced by sulphuric acid anodizing (SAA). The outer surface of PAA aluminium has whiskerlike spikes of alumina which interlock with adhesive to form a reinforced bond of high strength as shown by Venables et al. (J.D.
Venables, D.K. McNamara, J.M. Chen, T.S.
Sun and R.L. Hopping, Appl. Surface Science 1979, 3, 88). This structure is due to the solubility of alumina in phosphoric acid. Alumina is less soluble in sulphuric acid so the outer surface of SAA aluminium is smoother and has smaller diameter pores than PAA aluminium. Consequently, penetration of adhesive into the pores of SAA aluminium is restricted and the bond strength is poorer.
The disadvantage of using phosphoric acid is that it is about five times as expensive as sulphuric acid and it continues to dissolve the alumina after cessation of anodizing current encountered in commercial anodizing. Poor bonding results wherever the alumina surface is excessively dissolved. Rinsing/neutralising can prevent dissolution after anodising, however plants very often operate automatic systems. This usually means a drain time, and time for carriage from the anodising tank to the rinse-tank of up to 1 min during which time dissolution can occur. The net result is a film which can be loose and weak in places with the protrusions partly removed.
It is an object of the invention to prepare adhesively bonded aluminium wherein the adhesive-aluminium interface exhibits environmental stability in an aqueous environment. It is a further object of this invention to provide a method of forming adhesively bonded aluminium in which adhesive failures at the aluminium-adhesive interface are minimised. It is a still further object of this invention to produce environmentally stable surfaces on aluminium for subsequent bonding to non-metallic materials, for electroplating and for painting.
The present invention comprises a method for producing environmentally stable surfaces on aluminium for adhesive bonding, electroplating or painting comprises the successive steps of: a) anodising the aluminium in an acid selected to produce a dense-packed thick-walled anodic oxide coating (alumina); and b) etching the anodised surface to modify the outer surface of the oxide coating while leaving the inner part of the alumina unaffected.
The present invention enables the use of, for example, sulphuric acid or chromic acid anodizing to prepare environmentally stable surfaces on aluminium for adhesive bonding which were hitherto not suitable as intermediate layers to improve bonding to aluminium.
The aluminium is anodized in the acid under conditions that produce relatively thick dense coatings with very small diameter pores.
These conditions favour corrosion resistance.
Preferably sulphuric acid is used to anodize the aluminium but alternatively chromic acid may be used as chromic acid anodized surfaces may be etched as well as sulphuric acid anodized surfaces may be.
At this stage the outer surface of the alumina is not rough enough for adhesive bonding and the pores are too narrow for penetration by adhesive. The main feature of this invention is a controlled dip in a solution containing phosphoric acid in order to develop an outer surface of the alumina with a tailored topography for maximum reinforcement of the subsequent adhesive bond and distribution of the load on a stressed joint over a relatively thick interfacial region of alumina and adhesive. At the same time the inner part of the alumina remains dense and corrosion resistant, and furthermore the phosphoric acid renders the alumina hydration resistant. To produce the requisite surface topography, the processing parameters for both the sulphuric acid anodizing and the phosphoric acid dip have to be carefully selected.
Preferably the anodising solution is 10% sulphuric acid in deionised water at a temperature of approximately -- 5"C. Lead or stainless steel cathodes may be used and the anodising solution agitated by air. The processing time is preferably selected to produce a surface coating approximately 1-50pm thick.
At this stage the surface of the anodic oxide coating is too flat for adhesive bonding, but by etching the oxide coating the surface becomes modified to a form suitable for adhesive bonding while at the same time retaining advantages arising from the sulphuric acid anodising process. After the anodising treatment the aluminium surface is stable and the anodised aluminium can be stored for long periods of times before the final acid etch treatment and bonding. Advantageously phosphoric acid is used for the etch treatment: preferably 25% phosphoric acid (85%)-in deionised water. In the preferred method the aluminium is given a water rinse and is then air dried prior to long term storage and/or acid etching.Using 25% phosphoric acid at 60 C the etch process is continued for one minute-the timing including the time to transfer to the water rinse. Alternatively the etching may be achieved using 10% phosphoric acid at 90"C for one minute.
After said etching the aluminium is again water rinsed and air dried and advantageously the adhesive bonding, electroplating or painting is carried out within 72 hours.
In an alternative arrangement the etch acid may comprise a mixture of phosphoric acid and one or more other acids, or a mixture of one or more acids and phosphate ions from, for example, sodium phosphate.
Alternatively, chromic acid may be used instead of phosphoric acid for the etch acid.
In another alternative arrangement a specific mixed acid system of chromic acid and sulphuric acid may be used for the etch acid.
Preferably the mixed acid system comprises
Chromic acid 17 Sulphuric acid 10 Ratio by weight Water 39 wherein fhe chromic acid is added to the mixture as sodium dichromate. The process is then continued for 1 minute at 60"C.
Other acids may be used singly or in mixtures thereof for the anodising step providing they are capable of producing an anodic oxide film greater than about 1 5 /V ie a film thicker than a barrier layer.
The pretreatment of aluminium according to the invention is suitable not only in manufacturing industry but also for hand applications to localised areas and for repair systems.
In order that the invention may be more readily understood one example of the pretreatment of aluminium prior to adhesive bonding, electroplating or painting will now be given.
In order to prepare an aluminium object for adhesive bonding, painting or electroplating, the surface of the object is first degreased using a solvent: trichlorethylene vapour. After solvent cleaning the surface is then alkaline cleaned using a 10% solution of sodium hydroxide or a proprietary alkaline cleaner. The aluminium is then given a water rinse by immersion in tap water for 2-5 minutes.
Ater this cleaning the aluminium is anodised in sulphuric acid to form a surface anodic oxide coating approximately 40 ym thick. The aluminium is immersed in a 10% solution of sulphuric acid in deionised water at a temperature of - 5"C. Lead or stainless steel cathodes are immersed in the electrolyte and a voltage of 24V is applied between the aluminium and the cathodes. At the same time the electrolyte is agitated by bubbling air through it. The anodising treatment is continued for 5-30 minutes. After anodising, the aluminium is rinsed by immersion in tap water for 2-5 minutes followed by a water spray.
The anodised aluminium is then dried in warm air not exceeding about 60"C. At this stage the surface of the anodised aluminium is stable and not readily contaminated. The aluminium can therefore be stored for long periods prior to requirement for bonding or surface treatment.
Electron micrographs show that the anodised aluminium has a generally smooth outer surface which would not provide a suitable keying structure for the bonding of a primer or an adhesive.
The surface of the anodised aluminium is etched by treatment with 85% phosphoric acid made up to a 25% solution in deionised water. The anodised aluminium is immersed in the phosphoric acid at 60"C for 1 minute and then the aluminium is rinsed by immersion in tap water for 2-5 minutes and then dried in warm air, not exceeding 60"C.
After acid etching of the anodised aluminium electron micrographs show that the surface layer of the anodic oxide coating comprises a plurality of needle-like projections, considered important for good bonding.
After the final etching step in the pretreatment process, the aluminium should be stored for no more than about 72 hours before application of a primer or an adhesive as is required to achieve maximum bond strength.
Applications of aluminium treated according to the invention include: a) adhesive bonding of aluminium alloys for air frames and cars etc; b) paint adhesion, particularly if corrosion resistance is important as in air frames; c) polymer adhesion, for example PTFE bearings on aluminium etc; and d) electroplate adhesion.
The invention makes use of the hard, corrosion-resistant coating produced by acid anodising using an acid such as sulphuric acid, the coating being modified in such a way as to improve the ability of the anodic coating to bond to other materials.
It will be appreciated by those skilled in the art that modifications may be made to the example of the method of pretreatment described, all falling within the scope of the invention described in the specification. For example the treatment times and conditions for the anodising and etching processes may be varied from those specifically disclosed so as to produce a surface structure which is mechanically strong and corrosion resistant and provided with outward protrusions or needles, desirable for good bonding strength.
Sulphuric acid has the advantage of cheapness and produces a structurally strong anodic coating, desirable as a substrate for paints, adhesives etc. By then modifying the outer surface of this anodic coating by acid etching, better bonding becomes possible. Phosphoric acid has a further advantage as the etching acid since it leaves a phosphonate coating as well and this has been shown to promote chemical bonding to the surface film. The amount of phosphoric acid used in the etching step is much less than would be required by conventional phosphoric acid anodising and is also used at a lower concentration.
Other additives known in the art may be included in the etching process to further improve the bonding to the aluminium. Other acids which may be used singly or in mixture thereof for the anodising step include oxalic, chromic and malonic acids.

Claims (18)

1. A method for surface pretreatment of aluminium or aluminium alloy prior to adhesive bonding, electroplating or painting comprising the successive steps of: a) anodising the aluminium in an acid selected to produce a dense-packed thick-walled anodic oxide coating (alumina); and b) etching the anodised surface to modify the outer surface of the oxide coating while leaving the inner part of the alumina unaffected.
2. A method as claimed in claim 1 wherein the anodising acid is sulphuric acid.
3. A method as claimed in claim 1 wherein the anodising acid is chromic acid.
4. A method as claimed in claim 2 wherein the acid is 10% sulphuric acid in deionised water at a temperature of - 5"C.
5. A method as claimed in claim 3, or claim 4 wherein the anodising step is timed to produce a surface coating in the thickness range 1-50 ym.
6. A method as claimed in any one of claims 1 to 5 wherein the anodising acid is agitated by air.
7. A method as claimed in any one preceding claim wherein the etch acid is phosphoric acid.
8. A method as claimed in claim 7 wherein 25% phosphoric acid (85%) in deionised water is used.
9. A method as claimed in any one of claims 1 to 6 wherein the etch acid is chromic acid.
10. A method as claimed in any one of claims 1 to 6 wherein the etch acid is a mixture of chromic and sulphuric acids.
11. A method as claimed in claim 10 wherein the mixture of acids comprises by weight ratio: 1 part chromic acid 10 parts sulphuric acid 30 parts water
1 2. A method as claimed in claim 8 or claim 11 wherein the acid is at 60"C and the etching step lasts for one minute before rinsing in deionised water.
1 3. A method as claimed in any one of claims 1 to 6 wherein the etch acid is a mixture of phosphoric acid and one or more other acids.
14. A method as claimed in any one of claims 1 to 6 wherein the etch acid is a mixture of one or more acids and phosphate ions.
1 5. A method as claimed in claim 7 wherein 10% phosphoric acid is used.
1 6. A method as claimed in claim 1 5 wherein the acid is at 90"C and the etching step lasts for 1 minute before rinsing in deionised water.
1 7. A method as claimed in any one preceding claim wherein the anodised aluminium is adhesively bonded, electroplated or painted within 72 hours of the etching step.
18. A method of surface pretreatment of aluminium or aluminium alloy prior to adhesive bonding, electroplating or painting substantially as described hereinbefore.
GB08413731A 1983-06-02 1984-05-30 Pretreatment of aluminum prior to bonding electroplating or painting Expired GB2141139B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08413731A GB2141139B (en) 1983-06-02 1984-05-30 Pretreatment of aluminum prior to bonding electroplating or painting

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838315203A GB8315203D0 (en) 1983-06-02 1983-06-02 Surface pretreatment of aluminium and aluminium alloys
GB08413731A GB2141139B (en) 1983-06-02 1984-05-30 Pretreatment of aluminum prior to bonding electroplating or painting

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GB8413731D0 GB8413731D0 (en) 1984-07-04
GB2141139A true GB2141139A (en) 1984-12-12
GB2141139B GB2141139B (en) 1986-07-30

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2171333A (en) * 1985-02-23 1986-08-28 Bl Tech Ltd Method and apparatus for preparing the surface of a component for bonding to another component
GB2271729A (en) * 1992-10-20 1994-04-27 Lo Chung Ching Aluminum frame of a door or window

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB602857A (en) * 1944-10-07 1948-06-03 Mallory Metallurg Prod Ltd Improvements in and relating to overlay metals of aluminium or aluminium base alloy bonded to an iron group metal, or metal base alloy
US3808000A (en) * 1972-03-28 1974-04-30 Grace W R & Co Printing plate and method of preparation
GB1410768A (en) * 1971-10-22 1975-10-22 Vickers Ltd Lithographic printing plates comprising anodised aluminium
GB1412004A (en) * 1972-10-05 1975-10-29 Oce Van Der Grinten Nv Process for preparing presensitised printing plates and printing plates obtained thereby
GB1517746A (en) * 1974-09-12 1978-07-12 Fuji Photo Film Co Ltd Method of producing a support for a printing plate

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB602857A (en) * 1944-10-07 1948-06-03 Mallory Metallurg Prod Ltd Improvements in and relating to overlay metals of aluminium or aluminium base alloy bonded to an iron group metal, or metal base alloy
GB1410768A (en) * 1971-10-22 1975-10-22 Vickers Ltd Lithographic printing plates comprising anodised aluminium
US3808000A (en) * 1972-03-28 1974-04-30 Grace W R & Co Printing plate and method of preparation
GB1412004A (en) * 1972-10-05 1975-10-29 Oce Van Der Grinten Nv Process for preparing presensitised printing plates and printing plates obtained thereby
GB1517746A (en) * 1974-09-12 1978-07-12 Fuji Photo Film Co Ltd Method of producing a support for a printing plate

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2171333A (en) * 1985-02-23 1986-08-28 Bl Tech Ltd Method and apparatus for preparing the surface of a component for bonding to another component
GB2271729A (en) * 1992-10-20 1994-04-27 Lo Chung Ching Aluminum frame of a door or window

Also Published As

Publication number Publication date
GB8413731D0 (en) 1984-07-04
GB2141139B (en) 1986-07-30

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940530