BACKGROUND
[0001] This disclosure relates to anodizing aluminum alloys.
[0002] Anodized coatings are used to protect aluminum alloys from corrosion and to provide
good adhesive bond strength. Some anodized coatings provide relatively good corrosion
protection, but also have a relatively smooth surface that does not promote good bonding
strength. Alternatively, other anodized coatings are textured and thus have good bonding
strength but are porous and do not provide good corrosion resistance.
SUMMARY
[0003] A method of anodizing according to an example of the present disclosure includes
immersing an aluminum alloy workpiece in a phosphoric acid anodizing solution, and
applying a voltage to the aluminum alloy workpiece in the phosphoric acid anodizing
solution. The phosphoric acid anodizing solution and the voltage act to form a porous
oxide layer on the aluminum alloy workpiece. The method includes the steps of removing
the aluminum alloy workpiece from the phosphoric acid anodizing solution and then
immersing the aluminum alloy workpiece in a controlled anodizing solution, and applying
a voltage to the aluminum alloy workpiece in the controlled anodizing solution. The
controlled anodizing solution and the voltage act to form a dense oxide layer on the
aluminum alloy workpiece under the porous oxide layer. The method includes the step
of controlling dissolution of the porous oxide layer during the formation of the dense
oxide layer by using tartaric acid in the controlled acid solution such that the thickness
of the porous oxide layer is substantially equivalent before and after the formation
of the dense oxide layer.
[0004] In an embodiment of the foregoing embodiment, the controlled anodizing solution includes
the tartaric acid and sulfuric acid.
[0005] In a further embodiment of any of the foregoing embodiments, the step of applying
the voltage to the aluminum alloy workpiece in the controlled anodizing solution includes
ramping the voltage to a predetermined hold voltage within three minutes, and then
holding at the predetermined hold voltage for no more than 30 minutes.
[0006] In a further embodiment of any of the foregoing embodiments, the controlled anodizing
solution has a temperature of 20-35°C during the step of applying the voltage.
[0007] In a further embodiment of any of the foregoing embodiments, the tartaric acid has
a concentration in the controlled acid solution of 60-100 gram/L.
[0008] In a further embodiment of any of the foregoing embodiments, the controlled anodizing
solution consists essentially of the tartaric acid and sulfuric acid.
[0009] In a further embodiment of any of the foregoing embodiments, the controlled anodizing
solution has a ratio of the tartaric acid to the sulfuric acid from 1:1 to 4:1.
[0010] In a further embodiment of any of the foregoing embodiments, the controlled anodizing
solution has a ratio of the tartaric acid to the sulfuric acid of approximately 2:1.
[0011] In a further embodiment of any of the foregoing embodiments, the phosphoric acid
anodizing solution is a 7.5 volume % phosphoric acid aqueous solution, and the phosphoric
acid anodizing solution is at room temperature of 20-25°C during the step of applying
the voltage to the aluminum alloy workpiece in the phosphoric acid anodizing solution.
[0012] In a further embodiment of any of the foregoing embodiments, the phosphoric acid
anodizing solution consists essentially of an aqueous phosphoric acid solution, and
the controlled anodizing solution consists essentially of the tartaric acid and sulfuric
acid.
[0013] A further embodiment of any of the foregoing embodiments includes immersing the aluminum
alloy workpiece that has the porous oxide layer and the dense oxide layer in a nitrilotrismethylene
solution.
[0014] A further embodiment of any of the foregoing embodiments includes immersing the aluminum
alloy workpiece that has the porous oxide layer and the dense oxide layer in an aqueous
trivalent chromium-containing sealing solution to deposit a chromium compound in the
dense oxide layer.
[0015] An anodized article according to an example of the present disclosure includes an
aluminum alloy substrate with a surface portion that is converted to a porous oxide
layer of aluminum oxides/phosphates, a dense oxide layer under the surface portion,
wherein the porous oxide layer of aluminum oxides/phosphates and the dense oxide layer
together are a duplex coating that has an electric resistance of at least 10
9 Ohms, and an electrically conductive material adjacent the duplex coating. The electrically
conductive material is different in composition from the aluminum alloy, and the electric
resistance of the duplex coating provides a galvanic corrosion barrier between the
aluminum alloy substrate and the electrically conductive material.
[0016] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
includes residual tartaric acid and sulfate ions.
[0017] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
is sealed with a chromium compound.
[0018] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
is thicker than the porous oxide layer.
[0019] An anodized airfoil according to an example of the present disclosure includes an
aluminum alloy airfoil extending between a leading end and a trailing end, with at
least a surface portion of the leading end being converted to a porous oxide layer
of aluminum oxides/phosphates, a dense oxide layer under the surface portion, wherein
the porous oxide layer of aluminum oxides/phosphates and the dense oxide layer together
are a duplex coating that has an electric resistance of at least 10
9 Ohms, and a sheath formed of an electrically conductive material and mounted adjacent
the duplex coating at the leading end of the aluminum alloy airfoil. The electrically
conductive material is different in composition from the aluminum alloy, and the electric
resistance of the duplex coating provides a galvanic corrosion barrier between the
aluminum alloy airfoil and the electrically conductive material of the sheath.
[0020] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
includes residual tartaric acid and sulfate ions.
[0021] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
is sealed with a chromium compound.
[0022] In a further embodiment of any of the foregoing embodiments, the dense oxide layer
is thicker than the porous oxide layer.
BRIEF DESCRIPTION OF THE DRAWINGS
[0023] The various features and advantages of the present disclosure will become apparent
to those skilled in the art from the following detailed description. The drawings
that accompany the detailed description can be briefly described as follows.
Figure 1 illustrates an example method of anodizing.
Figure 2 illustrates an example anodized article.
Figure 3 illustrates another example anodized article.
Figure 4 illustrates a micrograph of an in-process workpiece during the method of
Figure 1.
Figure 5 illustrates a workpiece after the method of Figure 1.
Figure 6 illustrates an anodized airfoil.
DETAILED DESCRIPTION
[0024] Figure 1 schematically illustrates an example method 20 of anodizing an aluminum
alloy workpiece. As will be described, the method 20 can be employed to anodize the
aluminum alloy workpiece to provide good corrosion resistance, good bonding strength,
and good electrical barrier properties.
[0025] As will be appreciated, the steps or actions described with respect to the method
20 can be employed with additional steps or other processes as desired. In this example,
the method 20 includes a first immersion step 22, a first voltage application step
24, a second immersion step 26, a second voltage application step 28, a third immersion
step 30, and a third voltage application step 32.
[0026] The first immersion step 22 includes immersing the aluminum alloy workpiece in a
phosphoric acid deoxidizing solution. At the first voltage application step 24, a
voltage is applied to the aluminum alloy workpiece in the phosphoric acid deoxidizing
solution. The phosphoric acid deoxidizing solution and the voltage act to remove surface
contaminants and native oxide on the aluminum alloy workpiece. In addition, the phosphoric
acid deoxidizing solution and the voltage act to form a thin porous oxide layer with
very fine filaments on the aluminum alloy workpiece.
[0027] The second immersion step 26 includes immersing the aluminum alloy workpiece from
step 24 in a phosphoric acid anodizing solution. At the second voltage application
step 28, a voltage is applied to the aluminum alloy workpiece in the phosphoric acid
anodizing solution. The phosphoric acid anodizing solution and the voltage act to
form a porous oxide layer on the aluminum alloy workpiece. For example, the porous
oxide layer has aluminum oxides and phosphates.
[0028] The aluminum alloy workpiece is then removed from the phosphoric acid anodizing solution
and in the third immersion step 30 is immersed in a controlled anodizing solution.
At the third voltage application step 32, a voltage is applied to the aluminum alloy
workpiece in the controlled anodizing solution. The controlled anodizing solution
and the voltage act to form a dense oxide layer under the porous oxide layer.
[0029] The resulting coating is a duplex coating with the porous oxide layer exposed at
the surface and the dense oxide layer formed underneath. The porous oxide layer is
relatively fragile and can be susceptible to dissolution in during the anodization.
In this regard, dissolution of the porous oxide layer during the formation of the
dense oxide layer is controlled by using tartaric acid in the controlled acid solution.
The tartaric acid facilitates the formation of the dense oxide layer, but its action
is not so severe such to dissolve the porous oxide layer. Therefore, the thickness
of the porous oxide layer is substantially equivalent before and after the formation
of the dense oxide layer.
[0030] As an example, the porous oxide layer has a filament structure of an amorphous oxide.
The filament structure is also substantially preserved by use of the controlled acid
solution. By preserving these features and thickness of the porous oxide layer, the
properties of the porous oxide layer can also be preserved in the resulting duplex
coating. In this regard, the duplex coating that is formed has an electric resistance
of at least 10
9 ohms. Particularly where the duplex layer is used both as a corrosion resistant layer
and for adhesive bonding with another, dissimilar and electrically conductive material,
the high electrical resistance of the duplex layer serves as a galvanic barrier between
the underlying aluminum alloy and the overlying electrically conductive material.
Thus, the duplex layer in some examples can serve the multiple functions of corrosion
resistance, adhesion promotion, and galvanic protection.
[0031] In a further example, the controlled anodizing solution includes the tartaric acid
and also sulfuric acid in a mixed acid solution. For example, the concentration of
the tartaric acid in the mixed acid solution can be 60-100 gram/L. In further examples,
the controlled anodizing solution includes only the tartaric acid and the sulfuric
acid, and possibly impurities. The ratio of tartaric acid to the sulfuric acid is
from 1:1 to 4:1, and can be 2:1 for best control over preserving the porous oxide
layer. In further examples, the tank temperature of the controlled anodizing solution
during the formation of the dense oxide layer is 20-35°C.
[0032] The resulting duplex layer can be further treated to improve the properties as desired.
In one example, the duplex coating is further treated by immersion in a nitrilotrismethylene
(NTMP) solution, as in step 34. The NTMP solution acts to stabilize the porous oxide
layer, to enhance bonding with a later-applied adhesive, such as epoxy, and to improve
the corrosion barrier properties of the duplex oxide layer. Without being bound, the
NTMP adsorbs onto the porous oxide layer to form a monolayer that renders the porous
oxide layer hydrophobic and promotes bonding with epoxy or other later-applied adhesives.
[0033] Alternatively, or in addition to the NTMP solution, the duplex coating can also be
treated to further enhance corrosion resistance by immersion in an aqueous trivalent
chromium-containing sealing solution. In this regard, the aqueous chromium solution
seals the dense oxide layer through formation of a chromium compound in the dense
oxide layer. Therefore, the NTMP solution and the aqueous chromium solution can be
used singly or in cooperation, with the NTMP solution enhancing bonding and the aqueous
chromium solution enhancing corrosion resistance.
[0034] Figures 4 and 5 are micrographs of a workpiece at various points through the example
method 20. Figure 4 shows a workpiece having an aluminum alloy substrate 42 and a
porous oxide layer 44 formed during the voltage application step 28 but prior to the
formation of a dense oxide layer 46. Figure 5 shows the workpiece after the formation
of the dense oxide layer 46. The thickness of the porous oxide layer 44, along a direction
substantially perpendicular to the surface of the aluminum alloy substrate 42, is
substantially equivalent before and after the formation of the dense oxide layer 46.
[0035] The following examples illustrate further embodiments of the method 20.
[0036] An Al alloy sheet (Al2024) was washed with organic solvent to remove surface paints
or stains. The sheet was then etched with sodium hydroxide aqueous solution and rinsed
with water. The etched Al alloy sheet was then deoxidized in nitric acid solution
and rinsed with water. The Al alloy sheet was then electrochemically deoxidized in
phosphoric acid under the following conditions:
15 v% phosphoric acid aqueous solution;
29°C solution temperature;
voltage ramp from 0V to 7.5V within a minute;
maintain voltage at 7.5V for 15 minutes.
[0037] The Al alloy sheet was removed from the deoxidizing bath and rinsed with water.
[0038] The Al alloy sheet was then anodized in phosphoric acid anodizing solution under
the following condition, to form the porous oxide layer:
7.5 v% phosphoric acid aqueous solution;
room temperature (approximately 23°C);
voltage ramp at approximately 5V/min to 15V within 3 minutes;
maintain the voltage at 15V for 20 minutes.
[0039] The Al alloy sheet was removed from the phosphoric acid anodizing bath and rinsed
with water. The Al alloy sheet was then immersed in the controlled anodizing solution
of a mixture of sulfuric acid and tartaric acid, under the following conditions:
tartaric acid 80g/L + Sulfuric acid 40g/L;
35°C electrolyte bath temperature;
voltage ramp at approximately 5V/min to 13V within 3 minutes;
maintain the voltage at 13V for 20 minutes.
[0040] The Al alloy sheet was removed from the controlled anodizing solution and rinsed
with water.
[0041] The Al alloy sheet was then immersed in a 300ppm nitrilotrismethylene phosphoric
acid (NTMP) at room temperature for 15 minutes for sealing.
[0042] Figure 2 illustrates an example anodized article 40 produced by the method 20. In
this example, the anodized article 40 includes the aluminum alloy substrate 42 with
a surface portion 42a that is converted to the porous oxide layer 44, corresponding
to the steps 22 to 28 above. The porous oxide layer 44 includes aluminum oxides/phosphates
that are formed during the voltage application step 28 of the method 20. The porous
oxide layer 44 can be 0.2-0.8 micrometers in thickness and more specifically may be
0.3-0.5 micrometers in thickness.
[0043] The anodized article 40 also includes the dense oxide layer 46 that is under the
surface portion 42a. The dense oxide layer 46 can be 1-4 micrometers in thickness,
but is usually 2-3 micrometers for enhanced fatigue resistance. The dense oxide layer
46 can include residual tartaric acid and sulfate ions from the method 20 described
above. The porous oxide layer 44 and the dense oxide layer 46 together are a duplex
coating 48 that has an electric resistance of at least 10
9 ohms.
[0044] The article 40 also includes an electrically conductive material 50 adjacent the
duplex coating 48. For example, the electrically conductive material 50 is bonded
to the duplex coating 48 with an intermediate adhesive layer 52. The intermediate
adhesive layer 52 can be a polymeric-based adhesive. One example polymeric-based adhesive
is epoxy-based adhesive, but this disclosure is not limited to epoxy-based adhesives.
[0045] The electrically conductive material 50 is different in composition from the aluminum
alloy of the substrate 42. Due to the electrical conductivity of the electrically
conductive material 50 and of the aluminum alloy substrate 42, along with the close
proximity of these materials to each other, a galvanic couple could form and accelerate
corrosion. However, the relatively high electric resistance of the duplex coating
48 provides a galvanic corrosion barrier between the aluminum alloy of substrate 42
and the electrically conductive material 50 to prevent galvanic corrosion.
[0046] Figure 3 illustrates a modified example of an anodized article 140. In this disclosure,
like reference numerals designate like elements where appropriate and reference numerals
with the addition of one-hundred or multiples thereof designate modified elements
that are understood to incorporate the same features and benefits of the corresponding
elements. In this example, the article 140 also includes a surface portion 142a that
has a porous oxide layer 144, but the porous oxide layer 144 has been treated with
the NTMP solution as described above, as represented at areas 144a. The article 140
also includes a dense oxide layer 146. Alternatively to the NTMP treatment, or in
addition thereto, the dense oxide layer 146 can be treated with an aqueous chromium
solution to locally form chromium compounds, represented at 146a. The chromium compounds
seal the dense oxide layer 146 and further enhance the corrosion resistance of the
duplex coating 48.
[0047] Figure 6 illustrates another example of an anodized article, namely an anodized airfoil
240. The anodized airfoil include an aluminum alloy airfoil (substrate) 242 that extends
between a leading end 250 and a trailing end 252, with at least a surface portion
of the leading end 250 being converted to a porous oxide layer of aluminum oxides/phosphates,
as described herein above. In this example, the anodized airfoil 240 is substantially
as described with reference to the article 40 of Figure 2, and the electrically conductive
material 50 is a sheath that is mounted adjacent the duplex coating at the leading
end 250 of the anodized airfoil 240. For example, the electrically conductive material
50 of the sheath is titanium or a titanium-based alloy. The duplex coating (Figure
2) provides a galvanic corrosion barrier between the aluminum alloy airfoil 242 and
the electrically conductive material 50 of the sheath.
[0048] Although a combination of features is shown in the illustrated examples, not all
of them need to be combined to realize the benefits of various embodiments of this
disclosure. In other words, a system designed according to an embodiment of this disclosure
will not necessarily include all of the features shown in any one of the Figures or
all of the portions schematically shown in the Figures. Moreover, selected features
of one example embodiment may be combined with selected features of other example
embodiments.
[0049] The preceding description is exemplary rather than limiting in nature. Variations
and modifications to the disclosed examples may become apparent to those skilled in
the art that do not necessarily depart from the essence of this disclosure. The scope
of legal protection given to this disclosure can only be determined by studying the
following claims.
1. A method of anodizing comprising:
immersing an aluminum alloy workpiece in a phosphoric acid anodizing solution;
applying a voltage to the aluminum alloy workpiece in the phosphoric acid anodizing
solution, the phosphoric acid anodizing solution and the voltage acting to form a
porous oxide layer on the aluminum alloy workpiece;
removing the aluminum alloy workpiece from the phosphoric acid anodizing solution
and then immersing the aluminum alloy workpiece in a controlled anodizing solution;
applying a voltage to the aluminum alloy workpiece in the controlled anodizing solution,
the controlled anodizing solution and the voltage acting to form a dense oxide layer
on the aluminum alloy workpiece under the porous oxide layer; and
controlling dissolution of the porous oxide layer during the formation of the dense
oxide layer by using tartaric acid in the controlled acid solution such that the thickness
of the porous oxide layer is substantially equivalent before and after the formation
of the dense oxide layer.
2. The method as recited in claim 1, wherein the controlled anodizing solution includes
the tartaric acid and sulfuric acid.
3. The method as recited in claim 1 or 2, wherein the applying of the voltage to the
aluminum alloy workpiece in the controlled anodizing solution includes ramping the
voltage to a predetermined hold voltage within three minutes, and then holding at
the predetermined hold voltage for no more than 30 minutes.
4. The method as recited in any preceding claim, wherein the controlled anodizing solution
has a temperature of 20-35°C during the applying of the voltage.
5. The method as recited any preceding claim, wherein the tartaric acid has a concentration
in the controlled acid solution of 60-100 gram/L.
6. The method as recited in any preceding claim, wherein the controlled anodizing solution
consists essentially of the tartaric acid and sulfuric acid.
7. The method as recited in claim 6, wherein the controlled anodizing solution has a
ratio of the tartaric acid to the sulfuric acid from 1:1 to 4:1, for example approximately
2:1.
8. The method as recited in any preceding claim, wherein the phosphoric acid anodizing
solution is a 7.5 volume % phosphoric acid aqueous solution, and the phosphoric acid
anodizing solution is at room temperature of 20-25°C during the applying of the voltage
to the aluminum alloy workpiece in the phosphoric acid anodizing solution.
9. The method as recited in any preceding claim, wherein the phosphoric acid anodizing
solution consists essentially of an aqueous phosphoric acid solution, and the controlled
anodizing solution consists essentially of the tartaric acid and sulfuric acid.
10. The method as recited in any preceding claim, further comprising immersing the aluminum
alloy workpiece that has the porous oxide layer and the dense oxide layer in a nitrilotrismethylene
solution.
11. The method as recited in any preceding claim, further comprising immersing the aluminum
alloy workpiece that has the porous oxide layer and the dense oxide layer in an aqueous
trivalent chromium-containing sealing solution to deposit a chromium compound in the
dense oxide layer.
12. An anodized article comprising:
an aluminum alloy substrate with a surface portion that is converted to a porous oxide
layer of aluminum oxides/phosphates;
a dense oxide layer under the surface portion, wherein the porous oxide layer of aluminum
oxides/phosphates and the dense oxide layer together are a duplex coating that has
an electric resistance of at least 109 Ohms; and
an electrically conductive material adjacent the duplex coating, the electrically
conductive material being different in composition from the aluminum alloy, and the
electric resistance of the duplex coating providing a galvanic corrosion barrier between
the aluminum alloy substrate and the electrically conductive material.
13. The anodized article of claim 12 being an anodized airfoil comprising:
an aluminum alloy airfoil extending between a leading end (26) and a trailing end
(252), with at least a surface portion of the leading end being converted to said
porous oxide layer of aluminum oxides/phosphates; and
a sheath formed of said electrically conductive material and mounted adjacent the
duplex coating at the leading end of the aluminum alloy airfoil, the electric resistance
of the duplex coating providing a galvanic corrosion barrier between the aluminum
alloy airfoil and the electrically conductive material of the sheath.
14. The anodized article as recited in claim 12 or 13, wherein the dense oxide layer includes
residual tartaric acid and sulfate ions.
15. The anodized article as recited in claim 12, 13 or 14, wherein the dense oxide layer
is sealed with a chromium compound, and/or wherein the dense oxide layer is thicker
than the porous oxide layer.