1 Introduction

Superhydrophobic surfaces have become a research focus owing to their various applications in self-cleaning [1, 2], corrosion resistance [3, 4] and anti-icing [5]. It has been proven both surface energy [6] and roughness [7, 8] are the crucial factors to obtain superhydrophobicity. Based on these two factors, coating [9, 10], chemical depositing [11] and many other approaches have been advanced to prepare artificial superhydrophobic surfaces. On account that the surface modification technics to lower surface energy are well-developed, method to construct the rough structures becomes a key issue. There are two forms of rough surfaces that can be applied to obtain superhydrophobicity, surfaces with disordered structures and ordered structures. The ordered structured arrays with designed parameters appear to be more effective in revealing the mechanism of superhydrophobic surfaces or endowing special functions [12, 13]. For example, it has been reported recently that micro arrays with specific parameters allow a reduction in contact time when water droplets impact on this kind of superhydrophobic surfaces [14, 15], which results in these surfaces with micro post arrays being promising for application prospects in anti-icing from freezing rain. Several methods to prepare superhydrophobic post arrays have been reported, including photolithography, electric spark wire cutting and laser texturing. Öner and co-workers [16] obtained superhydrophobic post arrays on silicon substrates with a variety of topographies by changing the photomasks in lithography process. Butt et al. [17] used lithography to prepare SU-8 photoresist arrays with superhydrophobicity. Liu et al. [14] prepared superhydrophobic tapered posts on copper (Cu) substrates by using wire electro discharge machining followed by chemical etching and coating thin polymer. Van et al. [18] utilized laser texturing as well as surface energy modification to fabricate superhydrophobic square posts on stainless steel substrates. However, for the aforementioned methods, the machining efficiency of wire electro discharge machining for large-area array structures is very low, in addition, it is very difficult to fabricate post arrays with diameters of several tens of micrometers. Laser texturing not only requires expensive equipment but also is difficult to efficiently fabricate post arrays with diameter of several tens of micrometers. Photolithography is a highly efficient method to prepare superhydrophobic micro arrays, but currently, it can only be applied on silicon and photoresist substrates. Considering that metals are one of the most widely used materials, an effective method to fabricate superhydrophobic array structures on engineering metals has great significance for moving superhydrophobic surfaces towards real-world applications.

Mask electrochemical machining (MECM), which combines photolithography and micro electrochemical machining, is widely used to prepare micro-pits arrays on engineering metal materials because of its low cost, easy operation process and high machining efficiency [19,20,21,22]. Here, we extended this technique into the area of fabricating superhydrophobic post arrays on aluminum (Al) substrates. The influence of machining parameters on the array structures was investigated by simulation and then verified by experiment. Based on the fabricated post array structures, the relationship between wettability and microstructural parameters was further studied.

2 Experiment

The preparation process of the superhydrophobic post arrays is shown in Figure 1. Al plate (35 mm × 35 mm × 2 mm, Dalian Al material manufacturer, China) was first polished by abrasive paper to remove surface oxide and then cleaned in an ultrasonic bath. After drying, a thin film of positive photoresist (BP212-37S, Beijing Kehua Microelectronics, China) of 1.5 μm thickness was spun on the surface with rotation speed 450 r/min for 15 s and 2000 r/min for 45 s. Then the obtained plate was prebaked at 85 °C for 45 min and subsequently exposed to a UV light source for 20 s. After that, the plate was developed in 0.5 wt.% aqueous NaOH solution for 4 min. Then, after being postbaked at 85 °C for 45 min, the Al plate with the photoresist array was prepared.

Figure 1
figure 1

Preparation process of micro post arrays

The as-prepared Al plate and Cu plate of the same size were placed face to face with a separation distance of 10 mm in the electrolyte tank. Then the Al plate was electrochemically machined as a positive electrode under ultrasonic vibration in 15.0 wt.% aqueous NaNO3 solution to generate the designed array structures. And the current load was applied by a DC electrical source which exports current constantly and can provide voltage up to 60 V. After that, the fabricated plate was ultrasonically cleaned and then immersed in 1.0 wt.% fluoroalkylsilane–ethanol solution for 2 h at room temperature (25 °C) to lower its surface energy.

Micro morphologies of the samples were observed via scanning electron microscope (SEM, JSM-6360LV, Japan) and surface profiler (XZ-230, Zygo, America). Static contact angle (CA) measurements were performed by optical contact angle meter (DSA100, Krüss, Germany) at room temperature.

3 Results and Discussions

3.1 Modeling and Analyzing of MECM Fabrications of Micro Post Arrays

In order to obtain micro post arrays with the required structures, a 2D model as shown in Figure 2(a) was built in the ANSYS platform to study the variation of the array structures on process time (t) and current density (I). Domains I ~ IV in the figure represent the Cu electrode, electrolyte, Al plate and photoresist, respectively. The distance between positive and negative electrode (G) and the thickness of the photoresist film (H) were set to 10 mm and 1.5 μm, respectively. The photoresist parameters d0 = 150 μm, w0 = 250 μm were set in accordance with the photomask we used.

Figure 2
figure 2

Simulation of the electrochemical manufacturing process

Figure 2(b)‒(d) show the electric field intensity nephograms of different stages in the MECM process (these images were vertically enlarged to enable better imaging). At the beginning, the electric field was distributed homogeneously (Figure 2(b)) because comparing with G, H was so small that the photoresists had nearly no influence on the electric field distribution. After the removal of some of the Al plate, the structural changes led to a re-distribution of the electric field, and every surface that was exposed to the electrolyte had an electric load on it (Figure 2(c)). As a result, the sidewalls of the micro structures started to be corroded. And the structures of the micro array changed both vertically and horizontally over time. Eventually, the micro posts changed to truncated cones as shown in Figure 2(d). According to that, a 3D structural model was sketched and shown in Figure 2(e). The diameter of the top surface of the post (d) and post height (h) were utilized as the critical parameters to describe the post array structures.

During the manufacturing process, ranges of domain II (electrolyte) and domain III (Al plate) changed continuously because of Al material removal. The varying velocity of the electrolyte-Al plate contact line (V) obeyed Faraday’s law,

$$\varvec{V}\, = \,\eta \omega \kappa \varvec{E}\text{,}$$
(1)

where ƞ refers to the current efficiency, ω denotes the electrochemical equivalent of Al material, \(\kappa\) represents the electric conductivity of 15.0 wt.% aqueous NaNO3 solution, E is electric field intensity of nodes and it can be solved by simulation.

For an arbitrary node Mn(xn, yn) on the contact line of electrolyte and Al plate, the coordinate of corresponding new node Mn+1(xn+1, yn+1) after a time interval ∆t could be calculated as follows:

$$x_{{{\text{n}} + 1\,}} \, = \,x_{{{\text{n}}\,}} + \,\eta \omega \kappa E_{X} \Delta t,$$
(2)
$$y_{{{\text{n}} + 1\,}} \, = \,y_{{{\text{n}}\,}} + \,\eta \omega \kappa E_{Y} \Delta t,$$
(3)

where EX and EY are the components of E along X axis and Y axis, respectively.

New boundaries of domain II and domain III were generated by connecting all the nodes computed. These boundaries were used to set up a new model from which subsequent model boundary variations could be obtained. Therefore, an iterative method to set up time series model that represents the structural geography was given. After several times of iterative calculations, correlation between t and the micro structures was revealed. The variation of electrolyte-Al plate contact line with t without considering of ƞ when a 0.6 A/cm2 current load was applied is shown in Figure 3.

Figure 3
figure 3

Profile changes of electrolyte-Al plate contact line

In the iterative calculation, variations of the node coordinates were proportional to the effective current density ƞI and the process time t. And the result of simulation indicated that a uniform structure could be obtained when we adjusted I and t to make ƞIt equal. So we established ƞIt as the independent variable, after considering the changes of I with the range changes of the processing area in a constant current mode, a polynomial fitting was carried out to establish the variation laws of d and h, which could be deduced as follows:

$$d\, = \,{d_0}\, - \,0.563\eta It\, + \,2.77e^{ - 4} \left( {\eta It} \right)^{2} ,$$
(4)
$$h\, = \,0.298\eta It\, - \,4.32e^{ - 4} \left( {\eta It} \right)^{2} .$$
(5)

Moreover, although the 15.0 wt.% aqueous NaNO3 solution used in this experiment as electrolyte had a current efficiency that increased non-linearly with the growth of current density. Under our processing condition, we noticed that ƞ is approximately 47.5% when the electric current density was constant 3‒7 A/cm2. So in the subsequent manufacturing, the current density was chose within the range of 3‒7 A/cm2, and the variation laws of d and h with I and t could be expressed as follows:

$$d\, = \,{d_0}\, - \,0.267It\, + \,6.25e^{ - 5} \left( {It} \right)^{2} ,$$
(6)
$$h\, = \,0.142It\, - \,9.75e^{ - 5} \left( {It} \right)^{2} .$$
(7)

And these variation laws are illustrated in Figure 4.

Figure 4
figure 4

Variation of critical parameters with I and t

3.2 Comparison of Simulation and Fabricated Results of the Micro Post Arrays

A comparison of fabricated Al plates and simulant results was performed to verify the accuracy of the above simulation. Figure 5 shows the section profiles of micro arrays produced under current density of 4 A/cm2 for 90 s and 6 A/cm2 for 60 s, as well as simulant result when It = 360 As/cm2.

Figure 5
figure 5

Comparison of section profiles when It = 360 As/cm2

Shown in Figure 6(a), (b) are the experimental verification at various time points of d and h, respectively, when I = 6 A/cm2.

Figure 6
figure 6

Compare of d, h between simulation and experiment

It can be observed from Figure 5 that there was only a difference in the sidewall profiles among the three lines.

Because current density was reckoned as a constant in the simulation, for areas of low electric intensity in Figure 2(c), (d), current efficiency ƞ was applied inaccurately owing to the non-liner property of electrolyte. Therefore, a deviation of sidewall profile occurred consequently because these low intensity areas were always at the bottom and sidewalls of the posts.

But for the top surface and the areas far from the post centers, electric intensities tended to be close to the loads applied, so ƞ was used correctly, and the key parameters d and h were predicted precisely as shown in Figure 6. Thus, d and h of the post arrays can be accurately controlled by adjusting I and t according to Eqs. (6), (7).

Shown in Figure 7 are SEM images of the fabricated Al plate with expected d and h when I = 6 A/cm2 and t = 100 s, the anticipative micro post arrays were obtained on Al substrates.

Figure 7
figure 7

Fabricated structures when I = 6 A/cm2 and t = 100 s

3.3 Analysis of Wettability of the Post Arrays

According to the observation of solid-liquid contact interfaces on as-prepared Al plates, two typical modes shown in Figure 8(a) were observed. These two modes were in accordance with the Cassie–Baxter model [8] and Wenzel model [9] as shown in Figure 8(b), respectively.

Figure 8
figure 8

Observed and theoretical contact mode

And after further measuring of static water CAs of fabricated Al plates, we found that the superhydrophobic surfaces where the CA was larger than 150° were in the contact mode of Cassie while the non-superhydrophobic surfaces were not. So static CAs of fabricated superhydrophobic surfaces can be explained by Cassie equation [8] as follows:

$$\text{cos}\theta^{\text{*}} \, = \,\varphi \text{s (cos}\theta_\text{0}\; + \,\text{1)}\, - \,\text{1,}$$
(8)

where \(\theta^{\text{*}}\) is the theoretical CA of Cassie model, \(\theta_\text{0}\) denotes the instinct CA of Al after modification, \(\varphi \text{s}\) refers to the fraction of solid-liquid interface in the composite interface.

Apparent CAs (θA) of Al plates of different post height and solid fraction were compared with θ* and shown in Figure 9. These Al plates were fabricated by MECM with different photomasks that had a diverse center-to-center distance w0 in the range of 160‒200 μm. And according to the Cassie theory, Al plates with different d and w0 would have the same CA if they had the same solid fraction \({\varphi_s}\).

Figure 9
figure 9

Theoretical and measured CAs of fabricated arrays

The reason that structures positioned in the gray area of Figure 9 don’t show superhydrophobicity can be explained as follows:

  1. (1)

    For a post array with certain diameter, the post height has to exceed a threshold to prevent the water droplet from collapsing into the microstructures [23,24,25]. Arrays of 20 μm post height were non-superhydrophobic as they failed to suspend the water droplet on the posts as depicted in the Cassie model.

  2. (2)

    The capillary pressure Pc of a fabricated micro array can be calculated as follows [26]:

    $$P_{\text{c}} \, = \,-\,\frac{{\text{4}d}}{{w_\text{0}^{\text{2}} }}\gamma {\text{ cos}\theta_\text{0}},$$
    (9)

    where γ refers to the surface tension coefficient of water. When \(\varphi_\text{s}\) was extremely small, capillary pressure provided by the micro array was low and the water droplet could not be suspended either. Therefore, if the center-to-center distance w0 is much larger than d, these arrays were not superhydrophobic regardless of the post height.

  3. (3)

    When the value of \(\varphi_\text{s}\) was large enough, the micro arrays were not superhydrophobic according to Eq. (8). A difference in the contact mode, as shown in Figure 8 resulted in a deviation between apparent CAs and theoretical CAs in this experiment.

For superhydrophobic surfaces shown in the golden area of Figure 9, \(\theta_\text{A}\) could be accurately predicted because they matched well with \(\theta^{\text{*}}\). For a micro cylindrical array, the solid fraction can be deduced as follows:

$$\varphi \text{s }\, = \,\text{ }\frac{{\pi d^{\text{2}} }}{{\text{4}w_\text{0}^{\text{2}} }}$$
(10)

Combining Eq. (10) with Eq. (8), the correlation between \(\theta_\text{A}\) and microstructure of the micro post array can be given as,

$$\text{cos}\theta_\text{A}\, = \,\frac{{\pi d^{\text{2}} }}{{\text{4}w_\text{0}^{\text{2}} }}\left( {\text{cos}\theta_\text{0}\, + \,\text{1}} \right)\, - \, 1$$
(11)

Thus, according to Eqs. (6) and (11), microstructures as well as apparent CAs of the superhydrophobic post arrays can be precisely controlled by adjusting I and t in the MECM process.

4 Conclusions

  1. (1)

    A facile method, combining photolithography, electrochemical machining with surface energy modification, was developed to fabricate superhydrophobic micro post arrays on aluminum substrates.

  2. (2)

    According to the simulant and experimental results, after a center-to-center distance is determined, the key structural parameters d and h of the post arrays can be precisely controlled by adjusting I and t in the MECM.

  3. (3)

    The correlation of array structure and apparent water contact angle for Al plates fabricated through the proposed method coincided with the Cassie-Baxter model. Thus, the structures and water CAs of superhydrophobic micro post arrays fabricated through this method are both controllable.