Method for de-anodizing an aluminum or aluminum alloy part for an aircraft turbine engine

Abstract

The invention relates to a method for de-anodizing a part (1), the part (1) comprising a base (10) made of aluminum or aluminum alloy and an anodization layer (12) based on oxy-hydroxides which covers at least a portion of the base (10) and which is intended to be removed by the method, the method comprising the following steps: (a) preparing a de-anodizing solution (2) comprising sulfuric acid (H2SO4) and nitric acid (HNO3), (b) immersing the part (1), or a portion of the part (1), in the de-anodizing solution (2), which is maintained at a temperature less than or equal to 25°C, and (c) removing the part (1) after a predetermined immersion time.

Description

[0001] DESCRIPTION

[0002] TITLE: METHOD FOR DESANODIZING AN ALUMINUM OR ALUMINUM ALLOY PART FOR AN AIRCRAFT TURBOMACHINE

[0003] Technical field of the invention

[0004] The present invention relates to the field of surface treatment of aluminum or aluminum alloy parts, and in particular to the field of desanodizing such parts having an anodizing layer based on oxy-hydroxides.

[0005] Technical background

[0006] Aluminum and aluminum alloys are materials of choice for the transportation industry, and particularly for the aerospace industry, due to their excellent mechanical properties-to-weight ratio and relatively low manufacturing cost. However, depending on their environment, these materials are susceptible to various types of localized corrosion, leading to component degradation and potentially resulting in removal or failure. Numerous strategies have been implemented to address this weakness, and among them, the formation or deposition of a protective layer on the surface of aluminum or aluminum alloy parts is the most widely used. This is particularly true of protective coatings obtained through an anodizing process on aluminum or aluminum alloy parts.Anodizing is an electrolytic process that replaces the natural oxide (native oxide), a few nanometers thick, which coats aluminum, with a layer of oxyhydroxides that can be several micrometers thick. The oxyhydroxide layers produced by anodizing range in thickness from two microns to several tens of microns, providing long-term corrosion protection. Anodizing, also called anodic oxidation, consists of forming a porous layer of aluminum oxyhydroxides, known as the anodized layer, on the surface of the part. This is achieved by applying an electric current to the part immersed in an electrolytic bath containing a strong acidic electrolyte. The part acts as the anode in the electrolytic system. Successive impregnation and sealing treatments then reinforce the porous anodized layer by covering it with a thin film of a few hundred nanometers and sealing the pores.The anodized layer thus formed on the surface of the part, particularly after impregnation and sealing treatments, helps to strengthen the corrosion resistance of the part.

[0007] Figure 1 schematically illustrates a process for anodizing a part 1 made of aluminum or aluminum alloy. This part 1 comprises a base 10 (or, alternatively, a main body or substrate) made of aluminum or aluminum alloy and an anodized layer 12 covering this base 10.

[0008] Anodizing treatments are now commonly used in the aerospace industry, primarily to improve the corrosion resistance of parts, and therefore their lifespan, but also to facilitate the adhesion of organic coatings (such as paints). However, the anodizing process is directly impacted by European regulations (REACH), which, since September 2017, have prohibited (or restricted to authorization) the use of certain key components in surface treatments, in particular, hexavalent chromium (Cr₂O). 6 ' or Cr(+VI)). Now, hexavalent chromium is present in:

[0009] - the usual surface preparation pretreatments, aimed at cleaning / stripping the surfaces of the parts before the anodizing treatment, - the electrolyte of certain anodizing treatments such as OAC (Chromic Anodic Oxidation),

[0010] - Certain final treatments, known as sealing treatments, aim to close the pores of the anodized layer formed during the anodizing process. Furthermore, the anodized layer can be damaged during use, and it may be necessary to remove it to apply a new anodized layer to the surface. It may also be necessary to remove the anodized layer to recycle the part or to apply another surface treatment. To do this, detreatment processes are required. Detreatment refers to the removal of the anodized layer from aluminum or aluminum alloy parts.

[0011] The desanodizing process is an industrial process used to remove an anodizing layer, allowing the same part to be re-anodized in the case of a first anodizing layer that has failed, or in the case of repairing parts returning from use, or to recover a previously anodized part in order to apply another surface treatment or to recycle it.

[0012] Figure 2 illustrates very schematically a prior art desanodizing process which is carried out in two sub-steps: - a sub-step (b1) of immersing part 1 in a desanodizing solution (2); and - another sub-step (b2) of immersing this part 1 in a desmuting solution composed of acids 20.

[0013] This substep (b2), known as bleaching, allows any oxide residue obtained in substep (b1) to be dissolved or decomposed.

[0014] It is known in the prior art to use several solutions (or, in other words, baths) for deanodizing, such as:

[0015] - a phospho-chromic solution, that is to say a solution containing phosphoric acid and chromic acid, in particular at 85°C;

[0016] - a sulfo-chromic solution containing sulfuric acid and chromic acid;

[0017] - a sodium hydroxide solution;

[0018] - a solution containing phosphoric acid and sodium molybdate; - a solution containing phosphoric acid and hexafluorosilicic acid.

[0019] However, phospho-chromic and sulfuro-chromic solutions use hexavalent chromium in the deanodizing solution, which is subject to REACH regulations.

[0020] The other aforementioned solutions (i.e., sodium hydroxide, phosphoric acid and sodium molybdate, or hexafluorosilicic acid) can attack and degrade the base of the part beneath the anodized layer. As an example, several degraded areas are identified by arrows in Figures 3 and 4, which are microscopic images of the surface condition of the part after deanodizing it with the solutions of phosphoric acid with hexafluorosilicic acid, and phosphoric acid with sodium molybdate, respectively.

[0021] In this context, it would therefore be advantageous to have a desanodizing solution free of hexavalent chromium, allowing the removal of the anodizing layer, whether clogged, impregnated or not, while guaranteeing safety properties with respect to the aluminum or aluminum alloy base of the part.

[0022] Summary of the invention

[0023] The present invention offers a solution to at least some of the aforementioned problems which is simple, effective and economical.

[0024] To this end, the invention relates to a process for desanodizing a part, the part comprising a base made of aluminium or aluminium alloy and an anodizing layer based on oxy-hydroxides which covers at least part of the base and which is intended to be removed by the desanodizing process, the process comprising the following steps:

[0025] (a) preparation of a desanodizing solution comprising sulfuric acid (H2SO4) at a concentration [H2SO4] of between 60 and 300 g / L, and nitric acid (HNO3) at a concentration [HNOs] of between 40 and 200 g / L, (b) immersion of the part, or part thereof, in the desanodizing solution maintained at a temperature of less than or equal to 25°C, and (c) withdrawal of the part after a predetermined immersion time.

[0026] Thus, this solution makes it possible to achieve the aforementioned objective. In general, the desanodizing process according to the invention allows for the efficient and rapid removal of the oxyhydroxide-based anodizing layer without degrading the aluminum or aluminum alloy base of the part. To this end, the process uses a desanodizing solution containing sulfuric acid and nitric acid, which is therefore free of hexavalent chromium, at the aforementioned concentrations and at a temperature of 25°C or lower.

[0027] The sulfuric acid in the deanodizing solution is capable of dissolving oxyhydroxide (notably alumina (Al2O3)) to form aluminum sulfate (Ah(SO4)3), via the following chemical reaction:

[0028] Al2O3 + 3H2SO4 → 2Al 3+ + 3H2O + 3SO4 2-

[0029] The nitric acid in the deanodizing solution is also capable of dissolving, in particular, alumina, to form aluminum nitrate (Al(NO3)3), via the following chemical reaction:

[0030] Al2O3 + 6HNO3 → 2Al 3+ + 3H2O + 6NO3 -The immersion temperature of 25°C or lower, combined with the sulfuric and nitric acid concentrations according to the invention, can influence the reaction rate of the deanodizing process, as well as the rate of attack on the aluminum or aluminum alloy. Indeed, the low reactivity of the deanodizing solution of the invention towards the aluminum or aluminum alloy base depends on the application temperature of this solution. Thus, the immersion temperature according to the invention (i.e., 25°C or lower), combined with the sulfuric and nitric acid concentrations according to the invention, ensures that the aluminum or aluminum alloy base is not altered by the deanodizing solution. The deanodizing process according to the invention can also be used after or before an anodizing process known from the prior art.

[0031] Furthermore, the anodized layer is completely removed in a single step, thus eliminating the need for a prior art bleaching solution. This achieves the objective of the invention while minimizing handling, cost, and environmental impact.

[0032] In this application, the term "base" or "substrate" means the aluminum or aluminum alloy part on the surface of which the anodizing layer is formed, and by extension the metallic aluminum (elemental or alloy) located under the anodizing layer.

[0033] The terms "anodizing layer" and "anodized layer" are equivalent and both refer to the dtoxy-hydroxide layer formed on the surface of an aluminum or aluminum alloy part, as a result of an anodizing treatment.

[0034] The deanodizing process according to the invention may comprise one or more of the following features, taken individually or in combination with each other:

[0035] - the anodizing layer is based on aluminium oxyhydroxides and / or other oxyhydroxides formed in particular during the impregnation and sealing stages (such as chromium and zirconium oxyhydroxides, silicon oxyhydroxides, etc.);

[0036] - sulfuric acid is present at a concentration [H2SO4] between 100 and 150 g / L;

[0037] - nitric acid [HNO3] is present at a concentration between 50 and 100 g / L;

[0038] - the molar ratio between sulfuric acid and nitric acid is between 1 and 10, and preferably between 1 and 5; - the deanodizing solution further comprises a ferric salt, such as FeCb;

[0039] - the immersion time is less than 15 hours, preferably between 1 and 10 hours, and even more preferably about 8 hours; - said process is devoid, after step (b), of a pickling step of the part, or part of this part, for example in an acid solution.

[0040] The present invention also relates to a method for retouching and / or repairing a part,

[0041] the part comprising an aluminium or alloy base and an oxy-hydroxide-based anodizing layer that covers at least part of the base,

[0042] the process comprising the steps of:

[0043] (i) subject the part to a desanodizing process according to one of the features of the invention, so as to remove the anodizing layer, and (ii) re-anodize said part, or a part of said part, so as to form a new anodizing layer.

[0044] The part retouching and / or repair process may also include an impregnation step and / or a sealing step. The impregnation step forms a first film on the new anodized layer, which may be porous. This first film can be thin, for example, a few hundred nanometers. The first film seals the pores of the new anodized layer.

[0045] The sealing step allows the formation of a second film. This second film can cover the first film, or possibly the new anodized layer formed in step (ii). The second film enhances the corrosion resistance of the part. This second film can be thin, for example, a few hundred nanometers. The present invention also relates to the use of a desanodizing process according to one of the features of the invention, for retouching and / or repairing a part, or a portion thereof.

[0046] This part may include an aluminum or alloy base and an oxy-hydroxide-based anodizing layer that covers at least part of the base.

[0047] The part may be intended for a half-wheel of a landing gear or a part of an aircraft turbomachine.

[0048] Brief description of the figures

[0049] Other features and advantages will become apparent from the following description of a non-limiting embodiment of the invention with reference to the accompanying drawings in which:

[0050] Figure 1 schematically represents a process for anodizing a part made of aluminum or aluminum alloy according to the prior art;

[0051] Figure 2 schematically represents the steps of a prior art desanodizing process of an aluminum or aluminum alloy part having an anodized layer;

[0052] Figure 3 represents a microscopic image of a degraded surface condition of the part deanodized from the process of Figure 2 and with a first example of a prior art deanodizing solution comprising phosphoric acid and hexafluorosilicic acid;

[0053] Figure 4 represents a microscopic image of a degraded surface condition of the part deanodized from the process of Figure 2 and with a second example of a prior art deanodizing solution comprising phosphoric acid with sodium molybdate;

[0054] Figure 5 is a block diagram representing the steps of a desanodizing process according to the invention, of a part which comprises an aluminum or aluminum alloy base and an oxy-hydroxide based anodizing layer; Figure 6 schematically represents a step of immersing the part of Figure 5 in a desanodizing solution according to the invention;

[0055] Figure 7 is a microscopic image representing a smooth surface condition of the unanodized part that has been immersed with a deanodizing solution according to the invention at a temperature of 20 c C

[0056] Figure 8 is a microscopic image representing a surface condition of the unanodized part with the deanodizing solution according to the invention at a temperature of approximately 35°C;

[0057] Figure 9 schematically represents the desanodizing and reanodizing steps according to the invention;

[0058] Figure 10 shows several microscopic images of the surface conditions of the part after the deanodizing and reanodizing steps of Figure 9.

[0059] Elements having the same functions in different implementations have the same references in the figures.

[0060] Detailed description of the invention

[0061] Figures 1 to 4 have been described in the technical background above with reference to an anodizing of an aluminum or aluminum alloy part, and a desanodizing of this part according to the prior art.

[0062] The present invention relates to a method for desanodizing a part 1.

[0063] Part 1 can be a part for a half-wheel of an aircraft landing gear, or a part for an aircraft turbomachine.

[0064] Part 1 includes a base 10 made of aluminum or aluminum alloy and an anodizing layer 12 based on oxy-hydroxides which covers at least part of the base 10.

[0065] The aluminum alloy can be chosen from: - the 2000, 6000 and 7000 series, specifically selected from the group consisting of 2014, 2017, 2024, 2214, 2219, 2618, AU5NKZr, 7175, 5052, 5086, 6061, 6063, 7010, 7020, 7050, 7050 T7451, 7055, 7068, 7085, 7075, 7175 and 7475, - aluminum casting alloys selected from the group consisting of AS7G06, AS7G03, AS10G and AS9U3,

[0066] - the aluminum alloys (so-called difficult) chosen from the group consisting of 2618A, 2214 and AU5NKZr.

[0067] The anodizing layer 12 can be based on aluminium oxyhydroxides, chromium and zirconium oxyhydroxides, and / or silicon oxyhydroxides.

[0068] The thickness of the anodizing layer 12 can be between 1 and 50 pm, for example between 8 and 17 pm.

[0069] The anodizing layer 12 is intended to be removed by the deanodizing process of the invention.

[0070] The present application will now describe the desanodizing process according to the invention, in particular with reference to figures 5 to 7, 9 and 10.

[0071] The deanodizing process includes the following steps:

[0072] (a) preparation of a deanodizing solution 2 comprising sulfuric acid (H2SO4) and nitric acid (HNO3),

[0073] (b) immersion of part 1, or a portion thereof, in the deanodizing solution 2 maintained at a temperature of 25°C or lower, and

[0074] (c) removal of part 1 after a predetermined immersion time.

[0075] In deanodizing solution 2, sulfuric acid may be present at a concentration [H2SO4] between 60 and 300 g / L, and preferably between 100 and 150 g / L.

[0076] Nitric acid may be present at a concentration [HNO3] of between 40 and 200 g / L in the deanodizing solution 2, and preferably between 50 and 100 g / L. The chemical reactions governing the mechanism of action of the deanodizing solution 2 according to the invention at a temperature of 25°C or lower are as follows for the dissolution of the anodized layer 12: Al2O3 + 3H2SO4 → 2Al 3+ + 3H2O + 3SO4 2- Al2O3 + 6HNO3 → 2Al 3+ + 3H2O + 6NO3 - Figure 5 represents the steps of the process of the invention.

[0077] The molar ratio (or in other words the ratio) between sulfuric and nitric acids in the deanodizing solution can be between 1 and 10, and preferably between 1 and 5.

[0078] The deanodizing solution 2 may also include a ferric salt, such as iron chloride (FeCl3). This ferric salt helps to prevent the accumulation of alloying elements (such as copper from an aluminum-copper alloy) on the aluminum alloy base 10.

[0079] In step (a), the deanodizing solution 2 can be prepared by mixing a first sulfuric acid solution with a second nitric acid solution in a container particularly suitable for receiving part 1, or at least part of part 1 to be deanodized.

[0080] The immersion time may be less than 15 hours, preferably between 1 and 10 hours, and even more preferably around 8 hours.

[0081] The immersion time of the part 1 to be desanodized can vary depending on the dimensions (such as thickness, length, etc.) of the anodized layer 12 to be removed, and / or the nature of the anodized layer 12. The desanodizing process may, after step (b), be omitted from a bleaching step of the part 1, or a portion thereof, for example, in an acid solution. Indeed, the process according to the invention allows for the complete removal of the anodized layer 12 in a single step (b).

[0082] Part 1, free from treatment with a desanodizing solution according to the invention at a temperature below 25°C, is treated with a desanodizing solution according to the invention. In other words, part 1 comprises the base 10 made of aluminum alloy from group 2214 and without the anodizing layer 12 of oxy-hydroxides.

[0083] The unanodized part 1 was immersed in the deanodizing solution 2 of the invention with the parameters indicated in Table 1 below:

[0084] [Table 1

[0085] Deanodizing solution

[0086] [H2SO4] in g / L 125

[0087] [HNO3] in g / L 85

[0088] Temperature (°C) 20

[0089] Duration (hours) 8

[0090]

[0091] Figure 7 illustrates the surface condition of part 1 treated according to Example 1. It can be seen that the base 10 has a smooth, undamaged surface. Therefore, no alteration of the base 10 is caused by the deanodizing solution 2 according to Example 1, and the integrity of the base 10 (and consequently of part 1) is preserved.

[0092] Exempt from treatment with a desanodizing solution at a temperature above 25°C

[0093] Another unanodized part 1 is treated by immersing this part 1 in the deanodizing solution 2.

[0094] Deanodizing solution 2 is similar to Example 1 in terms of sulfuric and nitric acid concentrations. The difference between Example 1 and Example 2 is the process temperature (see Table 2). The unanodized part 1 was therefore immersed in deanodizing solution 2 with the parameters indicated in Table 2 below:

[0095] [Table 2

[0096] Deanodizing solution

[0097] [H2SO4] in g / L 125

[0098]

[0099] [HNO3] in g / L 85

[0100] Temperature (°C) 35

[0101] Duration (hours) 2

[0102]

[0103] Figure 8 illustrates the surface condition of part 1 deanodized according to Example 2. It can be observed that the base 10 has a degraded surface condition with numerous cracks annotated by arrows on figure 8.

[0104] It can therefore be concluded that desanodization from the desanodization solution 2 according to the invention, in particular with concentrations of sulfuric and nitric acids identical to Example 1, but with a temperature of 35°C, which is higher than that of the process of the invention, does not prevent the degradation of the base 10 of the part 1.

[0105] With reference to the results of Examples 1 and 2, it is therefore the combination of sulfuric and nitric acid concentrations according to the invention and a temperature of less than or equal to 25°C which has a protective effect on the base 10 of part 1.

[0106] This application also relates to the use of the deanodizing process of the invention for the retouching and / or repair of part 1, or part of part 1. This makes it possible to remove the anodizing layer 12 of oxy-hydroxides from part 1 in order to subsequently carry out, for example, a reanodizing of this part 1 in the case of a first anodizing layer 12 which is defective or in the case of the repair of parts 1 returning from use.

[0107] Alternatively, the deanodized part 1 without anodizing layer 12 can be recycled or another surface treatment can be applied.

[0108] The present application will now describe a process for retouching and / or repairing part 1. This part 1 comprises the base 10 and the anodizing layer 12 as described above.

[0109] The retouching and / or repair process may include the steps of: (i) subjecting part 1 to the deanodizing process described above, so as to remove the anodizing layer 12, and

[0110] (ii) re-anodize part 1, or part of part 1, so as to form a new anodizing layer 14.

[0111] Figure 9 illustrates very schematically the removal of the anodized layer 12 by step (i), then the formation of the new anodized layer 14 by step (ii).

[0112] Step (ii) of reanodizing can be carried out according to one of the anodizing techniques known from the prior art.

[0113] The process of retouching and / or repairing the part may further include an impregnation step and / or a sealing step of the part 1, in particular deanodized by step (i).

[0114] During the impregnation stage, a first film can be formed on the new anodized layer 14, which may be porous. This first film (not shown in the figures) closes the pores of this new anodized layer 14. The first film can be thin, for example, a few hundred nanometers.

[0115] At the sealing stage, a second film can be formed on the first film, or possibly on the new anodizing layer 14. The second film helps to strengthen the corrosion resistance of this part 1. This second film can be thin, for example a few hundred nanometers.

[0116] Example 3 of a desanodizing and retouching and / or repair process according to the invention

[0117] A part 1 is deanodized according to step (i) of the process of the invention. This part 1 has been previously anodized. The part 1 according to Example 3 thus comprises the base 10 made of aluminum alloy of group 2214 and the anodizing layer 12 of oxy-hydroxides.

[0118] Part 1 was immersed in the deanodizing solution 2 of the invention with the parameters indicated in Table 3 below:

[0119] [Table 3] Deanodizing Solution

[0120] [H2SO4] in g / L 125

[0121] [HNO3] in g / L 85

[0122] Temperature (°C) 20

[0123] Duration (hours) 8

[0124]

[0125] Once the anodized layer 12 is removed, part 1 is re-anodized according to step (ii). Part 1 is thus re-anodized with a sulfuric acid solution, then impregnated with a Chromium 3+ bath and sealed with a silicate salt bath to form the new anodized layer 14. Figure 10 illustrates the different surface conditions of part 1 according to Example 3 before step (i) and after steps (i) and (ii). It can be seen that in step (i), the anodized layer 12 has been completely removed and that the base 10 has a surface condition that is substantially smooth with very little damage. It can also be seen that in step (ii), the new anodized layer 14 is formed on the nearly smooth surface of the base 10 of the previously de-anodized part 1.

[0126] The desanodizing process according to the invention is perfectly suited for removing anodized layers known to be difficult to desanodize, as shown in example 3. The desanodizing process is also suitable for anodized layers of older generations.

Claims

DEMANDS 1. A process for desanodizing a part (1), the part (1) comprising a base (10) of aluminium or aluminium alloy and an anodizing layer (12) based on oxy-hydroxides which covers at least a part of the base (10) and which is intended to be removed by the desanodizing process, The process includes the following steps: (a) preparation of a deanodizing solution (2) comprising sulfuric acid (H2SO4) at a concentration ([H2SO4]) of between 60 and 300 g / L, and nitric acid (HNO3) at a concentration ([HNO3]) of between 40 and 200 g / L, (b) immersion of the part (1), or a portion thereof (1), in the desanodizing solution (2) maintained at a temperature of 25°C or lower, and (c) removal of part (1) after a predetermined immersion time.

2. Deanodizing process according to claim 1, characterized in that the sulfuric acid is present at a concentration ([H2SO4]) between 100 and 150 g / L.

3. Deanodizing process according to claim 1 or 2, characterized in that nitric acid ([HNO3]) is present at a concentration between 50 and 100 g / L.

4. A desanodizing process according to any one of the preceding claims, characterized in that the molar ratio between sulfuric acid and nitric acid is between 1 and 10, and preferably between 1 and 5.

5. A desanodizing process according to any one of the preceding claims, characterized in that the desanodizing solution (2) further comprises a ferric salt, such as FeCls.

6. A desanodizing process according to any one of the preceding claims, characterized in that the immersion time is less than 15 hours, preferably between 1 and 10 hours, and even more preferably about 8 hours.

7. A desanodizing process according to any one of the preceding claims, characterized in that said process is devoid, after step (b), of a pickling step of the part (1), or of a part of this part (1), for example in an acid solution.

8. A desanodizing process according to any one of the preceding claims, characterized in that the part (1) is a part for a half-wheel of an aircraft landing gear, or a part of an aircraft turbomachine.

9. Method for retouching and / or repairing a part (1) the part (1) comprising a base (10) of aluminium or alloy and an anodizing layer (12) which covers at least a portion of the base (10), the method comprising the steps of: (i) subjecting the part (1) to a desanodizing process according to one of the preceding claims, so as to remove the anodizing layer (12), and (ii) re-anodize said part (1), or a part of said part (1), so as to form a new anodizing layer (14).

10. Use of a desanodizing process according to any one of claims 1 to 8 for the retouching and / or repair of a part (1), or part of that part (1).

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