The present invention relates to a method of removing a work-affected layer, and relates particularly to a method of removing a work-effected layer formed on the surface of a TiAl-based alloy by machining work.
Conventionally, Ni-based alloys have been used as the base material for aircraft engine blades, but in recent years, the use of TiAl-based alloys, which exhibit high specific strength, has become possible.
However, as disclosed in Patent Citation 1, TiAl-based alloys exhibit poor formability, and are difficult to cut. Further, TiAl-based alloys are more brittle than Ni-based alloys, and tend to be prone to the generation of a work-affected layer on the worked surface when machining work such as cutting or grinding is performed.
A work-affected layer has increased hardness compared with the base material, and therefore the surface of a TiAl-based alloy with a work-affected layer formed thereon tends to be prone to cracking.
Patent Citation 1: Japanese Unexamined Patent Application, Publication No. Hei 6-269927 (paragraph [0003])
Consideration is now being given to machining conditions that do not result in the formation of a work-affected layer, but with current technology, performing machining work with absolutely no formation of a work-affected layer is difficult. Further, no technique has been developed for efficiently removing a work-affected layer formed on the surface of a TiAl-based alloy.
In those cases where a work-affected layer is formed on the surface of a TiAl-based alloy, a method of removing the work-affected layer by dipping the alloy in an etchant may be used. However, when a TiAl-based alloy is dipped in an etchant, defects such as large erosion holes and fissures that have an adverse effect on the base material tend to be generated.
The present invention has been developed in light of these circumstances, and has an object of providing a method of removing a work-affected layer formed on the worked surface of a TiAl-based alloy (base material) by machining work, without exerting any adverse effect on the base material.
In order to achieve the above object, the present invention provides a method of removing a work-affected layer, the method including a step of dipping a TiAl-based alloy having a work-affected layer formed on the surface thereof by machining work in an etchant containing predetermined concentrations of hydrofluoric acid and nitric acid, wherein within the etchant, the concentration of the hydrofluoric acid is not less than 5 g/L and not more than 56 g/L, and the concentration of the nitric acid is selected from within a range from not less than 50 g/L to not more than 260 g/L in accordance with a combination of the concentration of the hydrofluoric acid within the etchant and the etching treatment temperature.
Within the work-affected layer, the grains have moved and been compressed, meaning the grain boundaries are closer together. As a result, etching that originates at the grain boundaries tends to occur readily. In the present invention, by using an etchant that contains hydrofluoric acid and nitric acid in a predetermined ratio, the occurrence of surface defects such as large erosion holes and fissures that have an adverse effect on the base material can be suppressed, while the work-affected layer is preferentially removed.
In one aspect of the invention described above, it is preferable that phosphoric acid is also added to the etchant. By employing this aspect, the surface of the base material following the etching treatment is able to be provided with a smoother finish.
According to the present invention, a work-affected layer can be removed effectively without damaging the base material.
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The method of removing a work-affected layer according to the present invention is applied to aircraft engine components such as engine turbines.
An embodiment of the method of removing a work-affected layer according to the present invention is described below with reference to the drawings.
In the present embodiment, a base material having a work-affected layer formed on the surface as a result of machining work such as cutting or grinding is dipped in an etchant, thereby removing the work-affected layer formed on the surface.
The base material is a TiAl-based alloy having a full lamellar structure. The thickness of the work-affected layer is approximately 5 μm to 20 μm.
The base material with the work-affected layer formed thereon is subjected to an appropriate pretreatment such as ultrasonic cleaning or alkali cleaning prior to dipping in the etchant.
The etchant is formed as an aqueous solution containing predetermined proportions of hydrofluoric acid (HF) and nitric acid (HNO3). The hydrofluoric acid concentration within the etchant is not less than 5 g/L and not more than 56 g/L. The nitric acid concentration within the etchant is selected from within a range from not less than 50 g/L to not more than 260 g/L in accordance with a combination of the hydrofluoric acid concentration within the etchant and the temperature of the etchant during the etching treatment.
The temperature of the etchant is preferably within a range from 20° C. to 40° C. The etching rate is preferably within a range from 1 μm/minute to 15 μm/minute.
The etchant may include other components that are typically contained within the reagents marketed commercially as hydrofluoric acid and nitric acid.
Further, the etchant may also contain phosphoric acid.
The amount of nitric acid in the etchant is typically 4 times to 45 times (by weight) the amount of hydrofluoric acid.
For example, when the etchant temperature is set to 35° C., the amount of nitric acid in the etchant is typically 4 times to 45 times (by weight), preferably 4.5 times to 22.5 times (by weight), and more preferably 4.5 times to 9 times (by weight), the amount of hydrofluoric acid.
For example, when the etchant temperature is set to 50° C., the amount of nitric acid in the etchant is typically 4.5 times to 45 times (by weight), preferably 4.5 times to 22.5 times (by weight), and more preferably 9 times to 22.5 times (by weight), the amount of hydrofluoric acid. However, if a ratio of 4.5 times (by weight) is used, then the hydrofluoric acid concentration within the etchant is preferably higher than 28 g/L.
For example, when the etchant temperature is set to 65° C., the amount of nitric acid in the etchant is typically 4.5 times to 45 times (by weight), and preferably 9 times to 45 times (by weight) the amount of hydrofluoric acid.
By using concentrations that satisfy the above ranges, a base material can be obtained for which, even following etching treatment, the depth of the largest pit (erosion hole) in the base material surface is not more than 10 μm, and the surface is free of fissures (steep cracks) caused by the etching treatment.
The time for which the base material having the work-affected layer formed thereon is dipped in the etchant may be selected appropriately in accordance with the thickness of the work-affected layer. The thickness of the work-affected layer varies depending on the machining conditions employed during the machining work. Accordingly, a preliminary test may be performed to ascertain the thickness of the work-affected layer that is formed when machining is performed under predetermined machining conditions, with the etching treatment time then determined on the basis of the etching rate of the etchant being used and the thickness of the work-affected layer.
Following dipping in the etchant, the base material may be subjected to appropriate post-treatments such as neutralization, water washing and drying.
A TiAl-based alloy containing mainly Ti-45Al was used as the base material, and this base material was subjected to cutting to prepare test pieces. A grinding process was used to achieve the cutting.
Etchant A: Nitric acid (purchased product, concentration: 61%) and hydrofluoric acid (purchased product, concentration: 47%) were mixed together in a ratio (by volume) of 14:1.
Etchant B: Nitric acid, hydrofluoric acid and distilled water were mixed together to achieve final concentration levels of 185 g/L of nitric acid and 13 g/L of hydrofluoric acid.
Etchant C: Nitric acid, hydrochloric acid, iron chloride and distilled water were mixed together to achieve final concentration levels of 16 g/L of nitric acid, 295 g/L of hydrochloric acid and 160 g/L of iron chloride.
The test pieces described above were subjected to ultrasonic cleaning and a degreasing treatment (acetone cleaning), and a test piece was then dipped in each of the etchants A to C for 10 minutes or 30 minutes. The temperature of the etchant A was 51° C. The temperature of the etchant B and the etchant C was 24° C. Subsequently, each test piece was cut, and the cross-section was inspected under an optical microscope (×500).
Based on
TiAl-based alloys exhibit excellent corrosion resistance. This is because a passivation film is formed on the surface of the TiAl-based alloy. In order to remove a work-affected layer from a TiAl-based alloy by etching, this passivation film must first be destroyed. Passivation films are more readily destroyed in the presence of halide ions and the like. The fluoride ion contained within hydrofluoric acid is one type of halide ion. The effect of these fluoride ions causes destruction of the passivation film on the TiAl-based alloy. Accordingly, in the etchant B, it is thought that the passivation film was destroyed by the hydrofluoric acid, while the mixture containing the nitric acid caused subsequent gradual etching of the work-affected layer. On the other hand, in the case of the etchant A, although the etchant included the same components as the etchant B, similar effects were unobtainable. It is thought that this observation is due to the nitric acid concentration within the etchant A being too high.
Based on the results of the preliminary tests described above, investigations were conducted into the effects of the concentrations of the hydrofluoric acid and nitric acid contained within the etchant, and the etching temperature.
The test pieces described above were subjected to ultrasonic cleaning and a degreasing treatment (alkali cleaning), half of each test piece 3 was then masked with an epoxy resin 4 in the manner shown in
Further, a test piece 3 described above was subjected to etching in the same manner as that described above without masking, and the test piece 3 was then cut and the cross-section was inspected under an optical microscope (×500). Furthermore, as comparative examples, test pieces described above were also dipped for 10 minutes or 30 minutes in an etchant (35° C.) composed of hydrofluoric acid 80 g/L, nitric acid 125 g/L and distilled water (the remainder).
Table 1 lists the concentrations of hydrofluoric acid and nitric acid within the etchants used when the etchant temperature was 35° C., and also lists the etching rates achieved.
The results in Table 1 showed that as the concentration of hydrofluoric acid within the etchant was increased, the etching rate also tended to increase.
According to
Table 2 lists the concentrations of hydrofluoric acid and nitric acid within the etchants used when the etchant temperature was 50° C., and also lists the etching rates achieved.
According to
Table 3 lists the concentrations of hydrofluoric acid and nitric acid within the etchants used when the etchant temperature was 65° C., and also lists the etching rates achieved.
According to
A test piece described above was subjected to ultrasonic cleaning and a degreasing treatment (alkali cleaning), half of the test piece was then masked with an epoxy resin, and the test piece was then dipped for 90 seconds in an etchant (35° C.) having final concentrations of hydrofluoric acid 10 g/L, nitric acid 80 g/L, phosphoric acid 57 g/L and distilled water (the remainder). Following the etching treatment, the epoxy resin was removed, and the test piece was cut and inspected under an optical microscope (×200). The etching rate was calculated in the same manner as that described above in Section 3. The calculated etching rate was 1.4 μm/minute.
Further, a test piece described above was subjected to etching in the same manner as that described above without masking, and the test piece was then cut and the cross-section was inspected under an optical microscope (×500).
Number | Date | Country | Kind |
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2012-107713 | May 2012 | JP | national |