Effects of Cryogenic Forging and Anodization on the Mechanical Properties and Corrosion Resistance of Aa6066–t6 Aluminum Alloys

In this study, AA6066 alloy samples were cryogenically forged after annealing and then subjected to solution and aging treatments. Compared with conventional 6066-T6 alloy samples, the cryoforged samples exhibited a 34% increase in elongation but sacrificed about 8%–12% in ultimate tensile strength (UTS) and yield stress (YS). Such difference was affected by the constituent phases that changed in the samples' matrix. Anodization and sealing did minor effect on tensile strength of the 6066-T6 samples with/without cryoforging but it decreased samples' elongation about 8%–10%. The anodized/sealed anodic aluminum oxide (AAO) film enhanced the corrosion resistance of the cryoforged samples.


Introduction
Al-xMg-ySi alloys (6xxx series Al alloys) are commonly used as extruded shapes and forged for making bicycle parts.Their characteristics include ample formability, machinability, weldability, and corrosion resistance, as well as good strength and elongation after heat treatment.These alloys are also readily available on the market.
Aluminum possesses a high stacking fault energy and readily undergoes dynamic recovery during deformation.Plastic deformation at low temperatures, such as cryorolling, is beneficial for refining grains in an aluminum alloy matrix [1,2].Chen studied equal-channel deformation of an Al-Mg alloy at cryogenic temperatures and found that high-density dislocations distorted grains to a refining grain size [3].Lee et al. also found that cryorolling 5083 alloy could obtain 200 nm fine grains to increase the ultimate tensile strength (UTS) from 315 to 522 MPa [4].For an Al-Mg-Si alloy, cryorolling with a 90% reduction could cause heavy plastic deformation to produce nanosized extra-fine grains [5][6][7].
Aluminum alloys that become deformed at cryogenic temperatures could suppress the dynamic recovery that occurs during plastic deformation, and could acquire fine grains featuring high-angle grain boundaries [8,9].The interaction of high-density dislocations enhanced the precipitation capability for producing a high density of nanosized precipitates [10].Yin et al. found nanograins that were less than 500 nm in size in 7075 alloy samples subjected to compression forging at cryogenic temperatures [11].
Krishina et al. [8,12] produced ultrafine-grained Al-4Zn-2Mg alloys by cryorolling and indicated that the driving force for precipitation could be enhanced by differential scanning calorimetry.As a result, the precipitates of the η phase became finer compared with conventional aging treatment.Sarma [13] found that cryorolling significantly changed aging behavior, leading to a reduction in the aging temperature from 190 to 125 ˝C and in aging time from 24 to 8 h for treating 2219 alloy (Al-Cu alloy).Jayaganthan [14] used X-ray analyses to study the aging behavior of 6061 alloy subjected to solution treatment then cryorolling.They found that increasing true strain in cryorolling tended to enhance the dissolution of alloys in the alloy matrix and promoted the driving force for precipitation.The UTS was improved from 300 to 365 MPa and elongation was raised from 11% to 13%.Cryorolling apparently reduced the size of intermetallic compounds contained in the matrix of 7075-T73 alloys.As a result, the corrosion resistance of anodized and sealed 7075-T73 alloy could be significantly enhanced [15].
Anodization and sealing improves the corrosion resistance of Al alloys by forming amorphous alumina and hydrate alumina in the anodized film.This process has been widely used in industry.Forging is a common process used for making bicycle and automobile parts.Determining the influence of cryoforging on the corrosion resistance of Al alloys with or without anodization should provide more values for designing and using Al alloys.
Copper was added as an alloying element in a 6xxx series alloy to enhance mechanical strength by precipitation hardening after heat treatment.For example, 6066 Al alloy contains some high-strength Cu (0.8-1.4 Mg, 0.9-1.8Si, 0.6-1.1 Mn, and 0.7-1.2Cu) to obtain a UTS of 393 MPa and a yield stress (YS) of 359 MPa after a T6 treatment.This study introduced cryoforging to further improve the toughness of 6066-T6 alloys and their corrosion resistance.The effects of anodization and sealing on the tensile properties and corrosion resistance of AA6066-T6 with and without cryoforging were also evaluated.
After annealing at 688 K for 120 min, the samples were divided into two groups.The first group was subjected to a solution treatment (803 K for 120 min) and artificial aging (450 K for 480 min); these samples were coded as T6 samples.The second group was subjected first to cryogenic forging, achieving a 40% reduced thickness (from 28 to 16.8 mm), then immersed in liquid nitrogen again, rotated by 90 ˝, and subjected to a second round of cryogenic forging.A 500-ton hydraulic press equipped with one open die set was used to conduct compression forging.After forging, the second group of samples was subjected to the solution to get CFT4 sample and followed by artificial aging treatments: 450 K for 480 min for CFT6a samples and 540 min for CFT6b samples.

Tensile and Fatigue Tests
The specimens used for testing tensile and rotating bending fatigue strengths were machined from heat-treated samples according to the ASTM B557 [16] (gage diameter: 6 mm) and JIS Z2274 [17] (gage diameter: 8 mm) specifications as shown in Figure 1a,b.The machined test bars were polished by a series of abrasive papers (2000 grit) and an alumina slurry to achieve a surface roughness of less than 0.1 µm (Ra).

X-ray Tests
X-ray diffraction (XRD) measurements were performed by using a NANO-Viewer Advance (Rigaku, Tokyo, Japan) equipped with a Cu target to identify the precipitates (or second-phase particles) formed in the matrix of different samples, including the T6, CFT4, and CFT6a samples.The cryoforged samples were solution-treated to get a CFT4 sample and followed by aging treatment to acquire a CFT6a sample.A power of 30 KV and current of 10 mA were used in this study.The sample sizes were 10 × 10 × 1 mm.

Anodization Process
Before anodization, all samples were polished to a surface roughness of approximately Ra ≤ 0.1 μm and then dipped into methanol and ultrasonically vibrated.The specimens were initially degreased by immersion in an alkaline solution (5 mass % NaOH) at 60 °C for 30 s and were then rinsed with water for 1-2 min.For the pickling process, specimens were submerged in an aqueous solution of HNO3 (30 vol.%) for 90 s at room temperature and then rinsed with water for 1-2 min.The anodization was conducted at 15 mA•cm −2 at 15 °C for 900 s in a 15 mass % sulfuric acid solution.The anodized samples were sealed in hot water at 95 °C for 1200 s [18].After anodization, scanning electron microscopy was conducted and determined that the anodic film was 12-14 μm thick.The anodized samples were sealed in hot water at 368 K for 20 min.

X-ray Tests
X-ray diffraction (XRD) measurements were performed by using a NANO-Viewer Advance (Rigaku, Tokyo, Japan) equipped with a Cu target to identify the precipitates (or second-phase particles) formed in the matrix of different samples, including the T6, CFT4, and CFT6a samples.The cryoforged samples were solution-treated to get a CFT4 sample and followed by aging treatment to acquire a CFT6a sample.A power of 30 KV and current of 10 mA were used in this study.The sample sizes were 10 ˆ10 ˆ1 mm.

Anodization Process
Before anodization, all samples were polished to a surface roughness of approximately Ra ď 0.1 µm and then dipped into methanol and ultrasonically vibrated.The specimens were initially degreased by immersion in an alkaline solution (5 mass % NaOH) at 60 ˝C for 30 s and were then rinsed with water for 1-2 min.For the pickling process, specimens were submerged in an aqueous solution of HNO 3 (30 vol.%) for 90 s at room temperature and then rinsed with water for 1-2 min.The anodization was conducted at 15 mA¨cm ´2 at 15 ˝C for 900 s in a 15 mass % sulfuric acid solution.The anodized samples were sealed in hot water at 95 ˝C for 1200 s [18].After anodization, scanning electron microscopy was conducted and determined that the anodic film was 12-14 µm thick.The anodized samples were sealed in hot water at 368 K for 20 min.

Microstructure Observation and Tensile Properties
Table 1 shows the measured mechanical properties of different samples.The CFT6b samples, which aged for 60 min longer than did the CFT6a samples, had increased strength but reduced elongation.The CFT6a samples exhibited a similar strength but superior elongation to the CFT6b samples, and they were adopted in this study for evaluation of their corrosion resistance and fatigue strength.In addition, the CFT6a samples obtained a matrix with a uniform hardness (HV minimum deviation: 1.7).Figure 2a,b show the second-phase (SP) and/or intermetallic compounds (IMC) located at the cross-sections in the transverse direction of the T6 and CFT6a samples.Different sizes of particles were counted and are listed in Table 2.The T6 samples exhibited more coarse SP/IMC particles than the CFT6a samples did as revealed by arrows in Figure 2.During the cryogenic forge, a shear stress was generated to act on the samples' matrix, breaking down the particles.As a result, the particles became finer and dissolution was enhanced during the solution treatment.The total SP/IMC particle count decreased from 864 to 734 counts/mm 2 .

Microstructure Observation and Tensile Properties
Table 1 shows the measured mechanical properties of different samples.The CFT6b samples, which aged for 60 min longer than did the CFT6a samples, had increased strength but reduced elongation.The CFT6a samples exhibited a similar strength but superior elongation to the CFT6b samples, and they were adopted in this study for evaluation of their corrosion resistance and fatigue strength.In addition, the CFT6a samples obtained a matrix with a uniform hardness (HV minimum deviation: 1.7).2. The T6 samples exhibited more coarse SP/IMC particles than the CFT6a samples did as revealed by arrows in Figure 2.During the cryogenic forge, a shear stress was generated to act on the samples' matrix, breaking down the particles.As a result, the particles became finer and dissolution was enhanced during the solution treatment.The total SP/IMC particle count decreased from 864 to 734 counts/mm 2 .longitudinal direction of the tensile test bar samples, as illustrated in Figure 3a,b for the CFT6a and T6 samples, respectively.The CFT6a sample had a high fraction of high-angle grain boundaries (HAGBs).The matrix of the T6 sample had grains featuring mainly low-angle grain boundaries, as shown in Figure 3b.The cyclic loaded sample after being subjected to 250 MPa and fractured at 2.56 ˆ10 5 life cycles is shown in Figure 3c, revealing further increasing HAGBs compared with those in Figure 3a.This increase could have been affected by dynamic recrystallization during cyclic loading.for the CFT6a and T6 samples, respectively.The CFT6a sample had a high fraction of high-angle grain boundaries (HAGBs).The matrix of the T6 sample had grains featuring mainly low-angle grain boundaries, as shown in Figure 3b.The cyclic loaded sample after being subjected to 250 MPa and fractured at 2.56 × 10 5 life cycles is shown in Figure 3c, revealing further increasing HAGBs compared with those in Figure 3a.This increase could have been affected by dynamic recrystallization during cyclic loading.The T6 sample comprised α-Al, Q-(AlCuMgSi), Al(Mn,Fe)Si, and some Mg 2 Si phases, as shown in Figure 4.After solution treatment, the cryoforged sample was tested and indicated that SP/IMC particles were highly dissolved in its matrix, as confirmed by the CFT4 sample in Figure 4.After artificial aging, the intensity of the Q phase was notably decreased, presenting complex phases of Mg 2 Si, Q-(AlCuMgSi), and Al(Mn,Fe)Si, as well as some Cu 9 Al 4 and CuMgSi phases; see CFT6a sample.Kim et al. annealed copper wire and an aluminum pad at 150 to 300 ˝C and found a Cu 9 Al 4 phase with an X-ray spectra peak at 43.9 ˝ [19].
Metals 2016, 6, 51 6 of 13 The T6 sample comprised α-Al, Q-(AlCuMgSi), Al(Mn,Fe)Si, and some Mg2Si phases, as shown in Figure 4.After solution treatment, the cryoforged sample was tested and indicated that SP/IMC particles were highly dissolved in its matrix, as confirmed by the CFT4 sample in Figure 4.After artificial aging, the intensity of the Q phase was notably decreased, presenting complex phases of Mg2Si, Q-(AlCuMgSi), and Al(Mn,Fe)Si, as well as some Cu9Al4 and CuMgSi phases; see CFT6a sample.Kim et al. annealed copper wire and an aluminum pad at 150 to 300 °C and found a Cu9Al4 phase with an X-ray spectra peak at 43.9° [19].[20].Cu atoms tend to segregate around the metastable phase in the Al-Mg-Si alloy, move to grain boundaries during the solution treatment, and diffuse to Mg-Si nanoparticles located at or near grain boundaries to finally form type-C precipitates [21] and the Q phase [22].As a result, in this study, the T6 sample mainly contained the Q phase and Mg2Si precipitates after aging.The present XRD spectra did not detect the S-Al2CuMg phase from the T6 sample.Neither could Vieira find the S-Al2CuMg phase in his study, in which two age-hardening heat treatments of Al-10Si-4.5Cu-2Mgwere completed [23].
The CFT6a sample increased the HAGBs in its matrix to provide more potent sites for accommodating Cu atoms after the solution treatment.During quench or aging in room temperature, Cu diffused to tie up with Al forming Cu9Al4 phase.During artificial aging, a Mg-Si cluster formed in situ; this either led to the formation of CuMgSi precipitates through movement of the Cu atoms, or the Cu-Mg clusters formed first and subsequently incubated the CuMgSi precipitate in the matrix.Figure 5a,b shows the transmission electron microscopy photos of the T6 and CFT6a samples, respectively.For a given solution and aging conditions, the CFT6a sample achieved finer precipitates (less than 100 nm) than the T6 sample did.The main constituted phases likely included Al(Mn,Fe)Si in block and plate shapes, and some fine particles (less than 100 nm) likely being Cu9Al4 and CuMgSi precipitates or Cu atoms surrounding fine Mg2Si phases, as shown in Figure 5b.The α-Al(Mn,Fe)Si dispersoids could have a block-shaped or plate-shaped morphology in the size of 50-200 nm, as reported by Li et al. [24].[20].Cu atoms tend to segregate around the metastable phase in the Al-Mg-Si alloy, move to grain boundaries during the solution treatment, and diffuse to Mg-Si nanoparticles located at or near grain boundaries to finally form type-C precipitates [21] and the Q phase [22].As a result, in this study, the T6 sample mainly contained the Q phase and Mg 2 Si precipitates after aging.The present XRD spectra did not detect the S-Al 2 CuMg phase from the T6 sample.Neither could Vieira find the S-Al 2 CuMg phase in his study, in which two age-hardening heat treatments of Al-10Si-4.5Cu-2Mgwere completed [23].
The CFT6a sample increased the HAGBs in its matrix to provide more potent sites for accommodating Cu atoms after the solution treatment.During quench or aging in room temperature, Cu diffused to tie up with Al forming Cu 9 Al 4 phase.During artificial aging, a Mg-Si cluster formed in situ; this either led to the formation of CuMgSi precipitates through movement of the Cu atoms, or the Cu-Mg clusters formed first and subsequently incubated the CuMgSi precipitate in the matrix.Figure 5a,b shows the transmission electron microscopy photos of the T6 and CFT6a samples, respectively.For a given solution and aging conditions, the CFT6a sample achieved finer precipitates (less than 100 nm) than the T6 sample did.The main constituted phases likely included Al(Mn,Fe)Si in block and plate shapes, and some fine particles (less than 100 nm) likely being Cu 9 Al 4 and CuMgSi precipitates or Cu atoms surrounding fine Mg 2 Si phases, as shown in Figure 5b.The α-Al(Mn,Fe)Si dispersoids could have a block-shaped or plate-shaped morphology in the size of 50-200 nm, as reported by Li et al. [24].An electron probe X-ray microanalyzer (JXA-8200, JEOL USA, Inc., Peabody, MA, USA) was used to obtain images of Mg, Si, Mn, and Cu mappings from the matrix of the CFT6a sample.The white aggregates in Figure 6a  An electron probe X-ray microanalyzer (JXA-8200, JEOL USA, Inc., Peabody, MA, USA) was used to obtain images of Mg, Si, Mn, and Cu mappings from the matrix of the CFT6a sample.The white aggregates in Figure 6a  An electron probe X-ray microanalyzer (JXA-8200, JEOL USA, Inc., Peabody, MA, USA) was used to obtain images of Mg, Si, Mn, and Cu mappings from the matrix of the CFT6a sample.The white aggregates in Figure 6a   The Q phase, Al(Mn,Fe)Si, and Mg 2 Si (larger than 80 nm) contained in the aluminum alloy sample are non-shearable particles in the α-Al matrix [25].Therefore, the T6 samples gained high strength.By contrast, the CFT6a samples contained Al(Mn,Fe)Si, Mg 2 Si, fine CuMgSi, and Cu 9 Al 4 precipitates.The fine Mg 2 Si or CuMgSi and Cu 9 Al 4 precipitates are shearable.Figure 7 illustrates the dislocations (marked as 1-1 and 2-2) intersected with two fine precipitates.In addition, the SP/IMC particle counts (Figure 2) were lower in the matrix of the CFT6a samples.As a result, the CFT6a sample had decreased numbers of barrier sites for tangling dislocations to reduce strength but enhance elongation.
precipitates are nanoscale and were difficult to detect by mapping.In Figure 6b, the white particles shown in the matrix of the T6 samples are Al(Mn,Fe)Si and Q-AlCuMgSi phases.An Al(MnFe)Si particle attached with Cu atoms could be distinguished and are indicated by an arrow.The black spots are the Mg2Si phase.
The Q phase, Al(Mn,Fe)Si, and Mg2Si (larger than 80 nm) contained in the aluminum alloy sample are non-shearable particles in the α-Al matrix [25].Therefore, the T6 samples gained high strength.By contrast, the CFT6a samples contained Al(Mn,Fe)Si, Mg2Si, fine CuMgSi, and Cu9Al4 precipitates.The fine Mg2Si or CuMgSi and Cu9Al4 precipitates are shearable.Figure 7 illustrates the dislocations (marked as 1-1 and 2-2) intersected with two fine precipitates.In addition, the SP/IMC particle counts (Figure 2) were lower in the matrix of the CFT6a samples.As a result, the CFT6a sample had decreased numbers of barrier sites for tangling dislocations to reduce strength but enhance elongation.Table 3 compares the surface roughness of T6 and CFT6a samples before and after anodization/sealing.Compared with the samples without anodization, these anodized and sealed samples showed an approximately 8%-10% reduction in elongation.Such a decrease is likely caused by the dissolution of SP/IMC at the film/matrix interface leading to degrade surface roughness and elongation.Before anodization, the surface roughness of the T6 and CFT6a sample was approximately 0.07 (0.04) μm; after anodization and sealing, the surface roughness became 0.16 (0.03) and 0.13 (0.06) μm.

Sample
Surface Roughness (μm) T6; CFT6a 0.07 (0.04) T6-A 0.16 (0.03) CFT6a-A 0.13 (0.06) Note: the deviations are listed in parentheses.Table 3 compares the surface roughness of T6 and CFT6a samples before and after anodization/sealing.Compared with the samples without anodization, these anodized and sealed samples showed an approximately 8%-10% reduction in elongation.Such a decrease is likely caused by the dissolution of SP/IMC at the film/matrix interface leading to degrade surface roughness and elongation.Before anodization, the surface roughness of the T6 and CFT6a sample was approximately 0.07 (0.04) µm; after anodization and sealing, the surface roughness became 0.16 (0.03) and 0.13 (0.06) µm.

Fatigue and Corrosion Tests
Applying the cryoforge before the solution treatment reduced the SP/IMC particle counts and transformed the Q phase into nanoscale CuMgSi and Cu 9 Al 4 precipitates, which reduced UTS and YS but increased elongation.Figure 8 shows that both the T6 and CFT6a samples obtained fatigue strength of 180 MPa at 1 ˆ10 7 life cycles.As shown in Figure 3a,c, we found that cyclic loading functioned to shift the peak of relative frequency from the misorientation angle of 40 ˝-45 ˝to 45 ˝-50 ˝, and increase some grain boundaries at angles of 10 ˝-20 ˝.During cyclic loading, shear stress drove part of the dislocations to conduct polygonization and/or reorganization.

Fatigue and Corrosion Tests
Applying the cryoforge before the solution treatment reduced the SP/IMC particle counts and transformed the Q phase into nanoscale CuMgSi and Cu9Al4 precipitates, which reduced UTS and YS but increased elongation.Figure 8 shows that both the T6 and CFT6a samples obtained fatigue strength of 180 MPa at 1 × 10 7 life cycles.As shown in Figure 3a,c, we found that cyclic loading functioned to shift the peak of relative frequency from the misorientation angle of 40°-45° to 45°-50°, and increase some grain boundaries at angles of 10°-20°.During cyclic loading, shear stress drove part of the dislocations to conduct polygonization and/or reorganization.Figure 9a,b show the fractured surface of the T6 and CFT6a samples, both of which were subjected to 185 MPa and which performed 5.8 × 10 6 and 7.7 × 10 6 life cycles, respectively.The CFT6a sample exhibited narrower striation spacing than did the T6 samples and achieved a longer fatigue life.The T6 sample obtained fracture steps, as revealed in Figure 9a, which can be attributed to the Q phase located at or near grain boundaries that served to strengthen the grain boundaries [22,26].Increasing fine precipitates in the matrix of the CFT6a sample likely more effectively to consume the crack propagation energy and thus slightly enhanced the life cycles.Figure 9a,b show the fractured surface of the T6 and CFT6a samples, both of which were subjected to 185 MPa and which performed 5.8 ˆ10 6 and 7.7 ˆ10 6 life cycles, respectively.The CFT6a sample exhibited narrower striation spacing than did the T6 samples and achieved a longer fatigue life.The T6 sample obtained fracture steps, as revealed in Figure 9a, which can be attributed to the Q phase located at or near grain boundaries that served to strengthen the grain boundaries [22,26].Increasing fine precipitates in the matrix of the CFT6a sample likely more effectively to consume the crack propagation energy and thus slightly enhanced the life cycles.

Fatigue and Corrosion Tests
Applying the cryoforge before the solution treatment reduced the SP/IMC particle counts and transformed the Q phase into nanoscale CuMgSi and Cu9Al4 precipitates, which reduced UTS and YS but increased elongation.Figure 8 shows that both the T6 and CFT6a samples obtained fatigue strength of 180 MPa at 1 × 10 7 life cycles.As shown in Figure 3a,c, we found that cyclic loading functioned to shift the peak of relative frequency from the misorientation angle of 40°-45° to 45°-50°, and increase some grain boundaries at angles of 10°-20°.During cyclic loading, shear stress drove part of the dislocations to conduct polygonization and/or reorganization.Figure 9a,b show the fractured surface of the T6 and CFT6a samples, both of which were subjected to 185 MPa and which performed 5.8 × 10 6 and 7.7 × 10 6 life cycles, respectively.The CFT6a sample exhibited narrower striation spacing than did the T6 samples and achieved a longer fatigue life.The T6 sample obtained fracture steps, as revealed in Figure 9a, which can be attributed to the Q phase located at or near grain boundaries that served to strengthen the grain boundaries [22,26].Increasing fine precipitates in the matrix of the CFT6a sample likely more effectively to consume the crack propagation energy and thus slightly enhanced the life cycles.The SP/IMC particles were small to be less than 17 µm.Anodization did not yield the deteriorated effect of reducing fatigue strength.The two anodized and sealed samples (T6-A and CFT6a-A) showed similar fatigue strength (185-190 MPa) at 1 ˆ10 7 life cycles as did those without anodization and sealing (180 MPa).
The polarization curves for all the samples with and without sealed anodic aluminum oxide (AAO) films are shown in Figure 10.The corrosion behavior of the samples was affected by the constituent phases of each.The T6 samples contained AlCuMgSi, Al(FeMn)Si, and Mg 2 Si phases, whereas the CFT6a samples acquired mainly Al(FeMn)Si and Mg 2 Si phases as well as some CuMgSi and Cu 9 Al 4 precipitates.Mg 2 Si is anodic relative to the aluminum matrix, but Al(FeMn)Si and AlCuMgSi are cathodic.The Cu-Al precipitates are more vulnerable to attack during the immersion test, compared with the Q phase [23].The CFT6a samples exhibited slightly inferior E corr (´1.0 V) and I corr (4.7 ˆ10 ´6 A/cm 2 ) than the T6 sample did (´0.93V and 2.6 ˆ10 ´6 A/cm 2 , respectively).The SP/IMC particles were small to be less than 17 μm.Anodization did not yield the deteriorated effect of reducing fatigue strength.The two anodized and sealed samples (T6-A and CFT6a-A) showed similar fatigue strength (185-190 MPa) at 1 × 10 7 life cycles as did those without anodization and sealing (180 MPa).
The polarization curves for all the samples with and without sealed anodic aluminum oxide (AAO) films are shown in Figure 10.The corrosion behavior of the samples was affected by the constituent phases of each.The T6 samples contained AlCuMgSi, Al(FeMn)Si, and Mg2Si phases, whereas the CFT6a samples acquired mainly Al(FeMn)Si and Mg2Si phases as well as some CuMgSi and Cu9Al4 precipitates.Mg2Si is anodic relative to the aluminum matrix, but Al(FeMn)Si and AlCuMgSi are cathodic.The Cu-Al precipitates are more vulnerable to attack during the immersion test, compared with the Q phase [23].The CFT6a samples exhibited slightly inferior Ecorr (−1.0 V) and Icorr (4.7 × 10 −6 A/cm 2 ) than the T6 sample did (−0.93V and 2.6 × 10 −6 A/cm 2 , respectively).After anodization and sealing, the anodized films on the aluminum alloy samples contained mainly amorphous alumina and a few hydrated alumina [27].These AAO films could significantly enhance the corrosion resistance of the aluminum alloys [28].Therefore, the anodized films deposited on the T6 and CFT6 samples improved Ecorr from (−0.9 to −1.0 V) to (−0.64 to −0.76 V).
Affected by a greater number of coarse SP/IMC (Table 2) and/or a higher particle population, the anodized and sealed film on the T6 sample was entrapped with particles along with air pockets, as shown in Figure 11a.By contrast, the film on the CFT6a sample is relatively sound with few trapped particles; see Figure 11b.The trapped particles could function as corrosion channels to accelerate chloride attacks.Therefore, the anodized and sealed T6 sample obtained a higher current density (Icorr of 3.6 × 10 −5 A/cm 2 ) than did the anodized and sealed CFT6a sample (Icorr of 3.8 × 10 −6 A/cm 2 ).
The dissolution of SP/IMC at the film-matrix interface drove aluminum and magnesium ions to move toward electrolytes leaving the Si particles remaining in the film, as shown in Figure 11c [27].Consequently, the anodized and sealed T6 sample obtained inferior corrosion current density to the bare T6 sample (3.6 × 10 −5 A/cm 2 vs. 2.6 × 10 −6 A/cm 2 ).Decreasing SP/IMC particle size and counts also reduced the size and counts of the Si particles that remained in the anodized film to undergo a minor change in corrosion current density (4.7 × 10 −6 vs. 3.86 × 10 −6 A/cm 2 ) in the bare CFT6a and anodized/sealed CFT6a samples.After anodization and sealing, the anodized films on the aluminum alloy samples contained mainly amorphous alumina and a few hydrated alumina [27].These AAO films could significantly enhance the corrosion resistance of the aluminum alloys [28].Therefore, the anodized films deposited on the T6 and CFT6 samples improved E corr from (´0.9 to ´1.0 V) to (´0.64 to ´0.76 V).
Affected by a greater number of coarse SP/IMC (Table 2) and/or a higher particle population, the anodized and sealed film on the T6 sample was entrapped with particles along with air pockets, as shown in Figure 11a.By contrast, the film on the CFT6a sample is relatively sound with few trapped particles; see Figure 11b.The trapped particles could function as corrosion channels to accelerate chloride attacks.Therefore, the anodized and sealed T6 sample obtained a higher current density (I corr of 3.6 ˆ10 ´5 A/cm 2 ) than did the anodized and sealed CFT6a sample (I corr of 3.8 ˆ10 ´6 A/cm 2 ).
The dissolution of SP/IMC at the film-matrix interface drove aluminum and magnesium ions to move toward electrolytes leaving the Si particles remaining in the film, as shown in Figure 11c [27].Consequently, the anodized and sealed T6 sample obtained inferior corrosion current density to the bare T6 sample (3.6 ˆ10 ´5 A/cm 2 vs. 2.6 ˆ10 ´6 A/cm 2 ).Decreasing SP/IMC particle size and counts also reduced the size and counts of the Si particles that remained in the anodized film to undergo a minor change in corrosion current density (4.7 ˆ10 ´6 vs. 3.86 ˆ10 ´6 A/cm 2 ) in the bare CFT6a and anodized/sealed CFT6a samples.

Conclusions
Adding cryoforging to the process changed the microstructure and mechanical properties of the AA6066-T6 alloy samples; specifically, it decreased SP/IMC particle counts and reduced the Q phase but increased fine CuMgSi and Cu9Al4 precipitates in the matrix of the CFT6a sample.As a result, the tensile property of elongation was increased by approximately 34% comparing with T6 sample.The anodized and sealed AAO film on the CFT6a sample improved its corrosion resistance but decreased its elongation by approximately 10% (from 14.2% to 12.7%).

Conclusions
Adding cryoforging to the process changed the microstructure and mechanical properties of the AA6066-T6 alloy samples; specifically, it decreased SP/IMC particle counts and reduced the Q phase but increased fine CuMgSi and Cu 9 Al 4 precipitates in the matrix of the CFT6a sample.As a result, the tensile property of elongation was increased by approximately 34% comparing with T6 sample.The anodized and sealed AAO film on the CFT6a sample improved its corrosion resistance but decreased its elongation by approximately 10% (from 14.2% to 12.7%).

Figure
Figure 2a,b show the second-phase (SP) and/or intermetallic compounds (IMC) located at the cross-sections in the transverse direction of the T6 and CFT6a samples.Different sizes of particles were counted and are listed in Table2.The T6 samples exhibited more coarse SP/IMC particles than the CFT6a samples did as revealed by arrows in Figure2.During the cryogenic forge, a shear stress was generated to act on the samples' matrix, breaking down the particles.As a result, the particles became finer and dissolution was enhanced during the solution treatment.The total SP/IMC particle count decreased from 864 to 734 counts/mm 2 .

Figure 2 .
Figure 2. Optical micrographs show second-phase particles located in the matrix of (a) T6; (b) CFT6a sample; non-etched cross-section in transverse direction.

Table 2 .
The SP and/or IMC particles measured from T6 and CFT6a samples; maximum particle size and count population were included.backscattered diffraction (SUPRA ULTRA 55 field emission scanning electron microscope, ZEISS, Jena, Germany) was performed to measure the misorientation angles of grain boundaries in the longitudinal direction of the tensile test bar samples, as illustrated in Figure3a,b

Figure 2 .
Figure 2. Optical micrographs show second-phase particles located in the matrix of (a) T6; (b) CFT6a sample; non-etched cross-section in transverse direction.

Figure 3 .
Figure 3. Inverse pole figure maps obtained from EBSD data and measured misorientation angle of grain boundaries from (a) CFT6a tensile tested sample; (b) T6 tensile tested sample; and (c) CFT6a sample after subjected to 250 MPa and fractured at 2.56 × 10 5 life cycles.

Figure 3 .
Figure 3. Inverse pole figure maps obtained from EBSD data and measured misorientation angle of grain boundaries from (a) CFT6a tensile tested sample; (b) T6 tensile tested sample; and (c) CFT6a sample after subjected to 250 MPa and fractured at 2.56 ˆ10 5 life cycles.

Figure 4 .
Figure 4. XRD patterns of 6066 alloy samples; including solution and aging T6 sample; cryoforged samples after solution treatment CFT4 and aging CFT6a, respectively.

Figure 4 .
Figure 4. XRD patterns of 6066 alloy samples; including solution and aging T6 sample; cryoforged samples after solution treatment CFT4 and aging CFT6a, respectively.

Figure 5 .Figure 6 .
Figure 5. TEM photo show the plate-shape and lump-shape precipitate in the matrix of (a) T6 sample, and (b) CFT6a sample.

Figure 5 .
Figure 5. TEM photo show the plate-shape and lump-shape precipitate in the matrix of (a) T6 sample, and (b) CFT6a sample.

13 Figure 5 .Figure 6 .
Figure 5. TEM photo show the plate-shape and lump-shape precipitate in the matrix of (a) T6 sample, and (b) CFT6a sample.
are the Al(Mn,Fe)Si and Q phase, and the black lumps are Mg2Si particles.The arrows indicate the locations of Q-phase precipitates.The CuMgSi and Cu9Al4

Figure 6 .
Figure 6.SEM photo and alloying elements mappings obtained from (a) T6 sample and (b) CFT6a sample.

Figure 7 .
Figure 7. TEM photo shows the intersection of dislocation 1-1 and 2-2 with two fine precipitates in the matrix of CFT6a sample, respectively.

Figure 7 .
Figure 7. TEM photo shows the intersection of dislocation 1-1 and 2-2 with two fine precipitates in the matrix of CFT6a sample, respectively.

Figure 10 .
Figure 10.Polarization curves obtained from immersion tests of T6 and CFT6a samples with/without anodization/sealing treatment.

Figure 10 .
Figure 10.Polarization curves obtained from immersion tests of T6 and CFT6a samples with/without anodization/sealing treatment.
Note: the deviations are listed in parentheses.

Table 2 .
The SP and/or IMC particles measured from T6 and CFT6a samples; maximum particle size and count population were included.

Table 3 .
Measured surface roughness of different samples before and after anodization.

Table 3 .
Measured surface roughness of different samples before and after anodization.