This disclosure relates to corrosion inhibitors and, more particularly, to a corrosion inhibitor that is effective for use on aluminum alloys having relatively high amounts of zinc.
Components made from metallic alloys, such as aluminum alloys, achieve higher strengths through inclusion of alloying elements. However, the presence of these alloying elements tends to make the alloy vulnerable to corrosion. Typically, the component utilizes a protective coating containing a corrosion-inhibitor to protect the underlying alloy from corrosion.
One type of corrosion-inhibitor includes hexavalent chromium in the form of a barium or strontium chromate compound, for example. Although effective, hexavalent chromium is commonly recognized as a carcinogen and is therefore undesirable for use as a coating.
Chrome-free corrosion-inhibitors have been used as an alternative to hexavalent chromium inhibitors. For example, chrome-free corrosion inhibitors utilize anodic and cathodic corrosion inhibitors to resist corrosion of the underlying alloy. One drawback of existing chrome-free corrosion inhibitors is that they do not provide equal corrosion protection for all alloy compositions.
New compositions of aluminum alloys are being developed and are finding use in industries such as the aerospace industry. Although conventional corrosion inhibitors, such as EcoTuff®, have been effective in providing corrosion protection, an even greater degree of corrosion protection is desired. Accordingly, there is a need for a corrosion-inhibiting substance that provides enhanced corrosion protection of aluminum alloys.
A method of selecting a corrosion-inhibiting substance according to a non-limiting example of this disclosure includes selecting a corrosion-inhibiting substance to include a non-tungstate anodic corrosion inhibitor with respect to an amount of zinc in an aluminum alloy substrate that is to be coated with the corrosion-inhibiting substance.
A further example according to the previous embodiment includes selecting the corrosion inhibiting substance to include the non-tungstate anodic corrosion inhibitor with respect to the amount of the zinc being between about 5.1 and 6.1 wt % of the aluminum alloy.
A further example according to any of the previous embodiments includes selecting the corrosion inhibiting substance also with respect to an amount of copper in the aluminum alloy substrate that is to be coated with the corrosion-inhibiting substance.
A further example according to any of the previous embodiments includes selecting the corrosion inhibiting substance to include the non-tungstate anodic corrosion inhibitor with respect to the amount of the copper being between 1.2 wt % and 2.0 wt %.
A further example according to any of the previous embodiments includes selecting the non-tungstate anodic corrosion inhibitor to include at least one of vanadium and molybdenum.
A further example according to any of the previous embodiments includes selecting the non-tungstate anodic corrosion inhibitor to include zinc molybdate.
A further example according to any of the previous embodiments includes selecting the corrosion inhibiting substance to include a cathodic corrosion inhibitor comprising at least one Group IIIB Periodic Table element.
A method of selecting a corrosion-inhibiting substance according to a non-limiting example of this disclosure includes selecting a corrosion-inhibiting substance to include a non-tungstate anodic corrosion inhibitor based upon an amount of at least one alloying element in an aluminum alloy substrate that is to be coated with the corrosion-inhibiting substance.
In a further example according to any of the previous embodiments, the at least one alloying element comprises zinc, and further includes selecting the corrosion inhibiting substance to include the non-tungstate anodic corrosion inhibitor based upon the amount of the zinc being between greater than 0.25 wt % of the aluminum alloy.
In a further example according to any of the previous embodiments, the at least one alloying element comprises zinc, and further including selecting the corrosion inhibiting substance to include the non-tungstate anodic corrosion inhibitor based upon the amount of the zinc being between about 5.1 and 6.1 wt % of the aluminum alloy.
A further example according to any of the previous embodiments includes selecting the non-tungstate anodic corrosion inhibitor to include at least one of vanadium and molybdenum.
A further example according to any of the previous embodiments includes selecting the non-tungstate anodic corrosion inhibitor to include zinc molybdate.
A further example according to any of the previous embodiments includes selecting the corrosion inhibiting substance to include a cathodic corrosion inhibitor comprising at least one Group IIIB Periodic Table element.
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows.
In this example, the substrate 12 is an aluminum alloy having a relatively high amount of zinc. For example, the aluminum alloy includes greater than 0.25 wt % zinc. In a further example, the aluminum alloy includes greater than about 5 wt % zinc. In yet a further example, the aluminum alloy includes about 5.1-6.1 wt % zinc. The term “about” as used in this description relative to numerical values such as compositions refers to possible variation in the value, such as normally accepted variations or tolerances in the art.
The composition of the protective coating 14, as will be described below, is selected to provide corrosion protection for the aluminum alloy substrate 12 having a relatively high amount of zinc. For example, tungsten may react with zinc at the surface of a zinc-containing substrate to the detriment of the corrosion protection of the coating. For alloys such as aluminum 2024, the amount of zinc is below 0.25 wt % and the amount of copper is above 3.0 wt %, which results in a copper-rich surface that is not susceptible to reaction between tungsten and zinc. However, with lower amounts of copper and higher amounts of zinc, such as in aluminum 7075, there is a zinc-rich surface that is susceptible to reacting with tungsten from a corrosion inhibitor. In the disclosed example, the protective coating 14 is tungstate-free and thereby the benefit of avoiding the reaction between the tungsten and zinc.
In one example, the aluminum alloy of the substrate 12 is aluminum 7075 and includes about 1.2-2.0 wt % copper, about 0.3 wt % manganese, about 2.1-2.9 wt % magnesium, about 0.4 wt % silicon, about 0.5 wt % iron, about 5.1-6.1 wt % zinc, about 0.18 to 0.35 wt % chromium, about 0.2 wt % titanium, and a balance of aluminum. The aluminum 7075 may include additional impurities or other elements that do not materially affect the properties of the alloy, or elements that are unmeasured or undetectable in the alloy. Likewise, the substrate 12 may be another type of high zinc aluminum alloy having greater than 0.25 wt % zinc.
In the illustrated example, the protective coating 14 includes a non-tungstate anodic corrosion inhibitor 16 and a cathodic corrosion inhibitor 18 that protects the underlying substrate 12 against corrosion. For example, the non-tungstate anodic corrosion inhibitor suppresses metal oxidation reactions, and the cathodic corrosion inhibitor 18 suppresses reduction reactions.
In one example, the non-tungstate anodic corrosion inhibitor includes at least one of a vanadate compound or a molybdate compound. In a further example, the non-tungstate anodic corrosion inhibitor is zinc molybdate. The cathodic corrosion inhibitor includes at least one element selected from the Group IIIB Periodic Table elements. In a further example, the cathodic corrosion inhibitor includes cerium. For example, the cerium is in the form of cerium citrate. In yet a further example, the non-tungstate anodic corrosion inhibitor 16 includes only zinc molybdate, and the cathodic corrosion inhibitor includes only the cerium citrate, which may ensure that other elements of unknown reactivity are not present within the protective coating 14.
The protective coating 14 may be used in any of a variety of different forms. For example, the non-tungstate anodic corrosion inhibitor 16 and the cathodic corrosion inhibitor 18 may be used as an additive or pigment in adhesives, paints, primers, sealants, or the like. In another example, the non-tungstate anodic corrosion inhibitor 16 and the cathodic corrosion inhibitor 18 are used as an additive in a conversion coating process for forming the protective coating 14. In one example, the non-tungstate anodic corrosion inhibitor 16 and the cathodic corrosion inhibitor 18 comprise about 1 to 50 wt % of the protective coating 14 with the remaining amount comprising a matrix surrounding the corrosion inhibitors 16 and 18.
Referring to
In one example, the zinc-inert anodic corrosion inhibitor 36 is a corrosion inhibitor that is suitable for avoiding reaction with zinc when exposed to an aluminum alloy having greater than 0.25 wt % zinc. For example, the zinc-inert anodic corrosion inhibitor 36 includes a vanadate or molybdate compound. In a further example, the compound is zinc molybdate. The cathodic corrosion inhibitor 34 includes at least one element selected from the Group IIIB Periodic Table elements. In a further example, the cathodic corrosion inhibitor 34 includes cerium. For example, the cerium is in the form of cerium citrate.
The amounts of the cathodic corrosion inhibitor 34 and the zinc-inert anodic corrosion inhibitor 36 within the carrier fluid 32 depends upon the desired composition of the protective coating 14. In one example, the concentration of each of the corrosion inhibitors 34 and 36 within the carrier fluid is about 0.1 to 100 grams per liter (0.01-13.3 ounces per gallon) of the carrier fluid 32. Given this description, one of ordinary skill in the art will be able to determine suitable concentrations of the corrosion inhibitors 34 and 36 for forming the protective coating 14 with a desirable composition.
As indicated in the above examples, the corrosion inhibiting substance 30 is selected to include the non-tungstate anodic corrosion inhibitor 16 based upon the amount of the zinc within the aluminum alloy of the substrate 12. In one non-limiting example to demonstrate the effectiveness of the non-tungstate anodic corrosion inhibitor 16 on high zinc aluminum alloys, specimens of aluminum 2024 and 7075 were coated with various compositions of corrosion-inhibiting substances and subsequently evaluated for corrosion. The specimens were coated with one or more of three different corrosion inhibiting substances. As shown in Table 1 below, a cerium citrate cathodic inhibitor is indicated as inhibitor 1, a zinc molybdate anodic inhibitor is indicated as inhibitor 2, and a strontium tungstate anodic inhibitor is indicated as inhibitor 3. The specimens were then tested according to ASTM G85 Annex 5 and evaluated with a numerical rating between 1 and 10, where 10 indicates no corrosion and 0 indicates complete corrosive failure. In other examples, other test conditions or standards may be used.
As shown in Table 1, the corrosion-inhibiting combination of all three corrosion inhibitors provides a rating of nine for the 2024 alloy. However, the corrosion-inhibiting combination of all three corrosion inhibitors provides only a rating of six for protecting the 7075 alloy. In this test, the combination of the cerium citrate cathodic inhibitor 1 and the zinc molybdate anodic inhibitor 2 provided a rating of nine for the 2024 alloy and a rating of 8 for the 7075 alloy. Thus, the tungstate-containing combination protects the 2024 alloy but does not protect the 7075 alloy as well, whereas the tungstate-free combination provides corrosion protection for the 2024 alloy and the 7075 alloy.
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.
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.
This application is a continuation of U.S. application Ser. No. 14/230,293 filed Mar. 31, 2014, which is a divisional of U.S. application Ser. No. 11/768,955 filed on Jun. 27, 2007.
Number | Name | Date | Kind |
---|---|---|---|
2387528 | Patterson | Oct 1945 | A |
2430589 | Sloan | Nov 1947 | A |
2902394 | Jeremias | Sep 1959 | A |
3063877 | Schiffman | Nov 1962 | A |
3279958 | Maurer | Oct 1966 | A |
4138353 | Lipinski | Feb 1979 | A |
5030285 | Vallvey | Jul 1991 | A |
5130052 | Kreh | Jul 1992 | A |
5266611 | Teschendorf | Nov 1993 | A |
5806327 | Lord et al. | Sep 1998 | A |
5871839 | Boyd et al. | Feb 1999 | A |
5948147 | Sinko | Sep 1999 | A |
5948267 | Whittemore et al. | Sep 1999 | A |
6074495 | Sung et al. | Jun 2000 | A |
6135195 | Lee et al. | Oct 2000 | A |
6190780 | Shoji et al. | Feb 2001 | B1 |
6537678 | Putnam | Mar 2003 | B1 |
6582530 | Hanlon | Jun 2003 | B1 |
6613390 | Jaworowski et al. | Sep 2003 | B2 |
6648986 | Tang | Nov 2003 | B1 |
6758887 | Bhatia | Jul 2004 | B2 |
6941770 | Taras et al. | Sep 2005 | B1 |
20020110642 | Jaworowski | Aug 2002 | A1 |
20030150525 | Briles | Aug 2003 | A1 |
20030217787 | Parkos | Nov 2003 | A1 |
20040256030 | Tang | Dec 2004 | A1 |
20040262580 | Yu | Dec 2004 | A1 |
20050179010 | Lin | Aug 2005 | A1 |
20060113007 | Morris | Jun 2006 | A1 |
20060247335 | Bhaatia | Nov 2006 | A1 |
20070000560 | Jaworowski | Jan 2007 | A1 |
Number | Date | Country |
---|---|---|
2491359 | Dec 2003 | CA |
0429180 | May 1991 | EP |
1191073 | Mar 2002 | EP |
1493846 | Jan 2005 | EP |
1493846 | May 2005 | EP |
1717279 | Nov 2006 | EP |
9923280 | May 1999 | WO |
Entry |
---|
European Search Report for European Patent Application No. 08252162.6 completed Jun. 26, 2009. |
Data Sheet. 7075 Alloy Data Sheet. 2006 Capital Aluminum Extrusions Limited. Retrieved Jul. 22, 2009 from: http://www.capalex.co.uk/7075_alloy.html. |
Data Sheet. Aluminum 7075-T6, 7075-T651 1996-2004. Automation Creation, Inc. p. 1. |
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20180073152 A1 | Mar 2018 | US |
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Parent | 11768955 | Jun 2007 | US |
Child | 14230293 | US |
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Parent | 14230293 | Mar 2014 | US |
Child | 15817654 | US |