Micro-model Design and Geometric Characteristics
The micro-model used in this study had three parts. The main part was the pore network formed by the void space between two slabs of PDMS connected by a large number of randomly distributed non-overlapping cylindrical pillars (shown as white circles in Fig. 1), having similar pore topology as in previous works (Ng et al. 1978; Reddi 1998; Tallakstad et al. 2009). The diameters of the cylinders, which represent the solid phase of the porous medium, were chosen from a random distribution, with maximum and minimum values of 80 and 20 \(\upmu \hbox {m}\), respectively. The cylinders all had the same height equal to the desired depth of the micro-model network. In order to accommodate the fibre optic piezometers (described in detail in Sect. 2.3), we needed a minimum depth of 320 \(\upmu \hbox {m}\). The network’s dimensions were 4 mm by 26 mm, and it had a porosity of 50%.
The second part of the micro-model was the inlet and outlet ports. This model had two separate inlet ports, one for each phase and one common outlet port. The two inlet ports allow for the simultaneous injection of two fluid phases from the same side, for the investigation of ganglia behaviour, similar to the works of (Avraam and Payatakes 1995, 1999). The outlet port is in the middle of the outlet area; it is not shown in Fig. 1 as it is on the other PDMS slab.
The third part of the micro-model was a set of measurement ports where the fibre optic piezometers can be inserted. In this design, we had five ports, two for each fluid at the inlet, one at the outlet and two along the micro-model. In Fig. 1, the positions of the sensors are shown as black vertical lines.
Soft Lithography
Manufacturing of PDMS micro-models was based on soft lithography (Quake and Scherer 2000; Markov et al. 2010). Soft lithography is a technique that is based on the use of elastomeric materials to produce micro- and nanoscale structures. A detailed description of the manufacturing procedure can be found in Karadimitriou et al. (2013). Here a short summary is given.
Mould Manufacturing
First, a silicon wafer was spin-coated with the liquid polymer SU8-2025 (MicroChem) according to the recipe, proposed by the supplier. The thickness of the coating was dictated by the target depth of the micro-model, i.e. 320 \(\upmu \hbox {m}\). This could not be applied in one step and had to be made in four layers. Given the viscosity of SU8-2025, each layer thickness was limited to 80 \(\upmu \hbox {m}\). First, a layer of 80 \(\upmu \hbox {m}\) was spin-coated and the wafer was soft baked at 65 and 95 \(^{\circ }\)C, for 3 and 8 min respectively. This was repeated three more times to achieve the required thickness. In order to ensure the adequate evaporation of the polymer’s solvent, after the first layer, the soft baking time was increased by 20% for every baking cycle.
The digitally generated pore network, described in Sect. 2.1 and shown in Fig. 1, was printed on a transparency. The transparent mask was placed on the soft baked photoresist coating and was exposed to UV light. The exposure times were calculated based on the recipe of SU-8 and the energy of the UV lamp for a film of 320 \(\upmu \hbox {m}\). This was followed by the post-exposure baking (hard baking) at 65 and 95 \(^{\circ }\)C, for 4 and 15 min respectively.
After exposure, the silicon wafer was developed for 30 mins with SU-8 developer (MicroChem). During this step, the unexposed photoresist was dissolved by the developer. An image of the result is shown in Fig. 2. To check whether the thickness was correct, the wafer was systematically measured with a profilometer. Afterwards, the wafer was baked at 150 \(^{\circ }\)C for 30 min. Finally, the wafer was silanized in a vacuum chamber with trichloro-(1H,1H,2H,2H-perfluorooctyl) silane. The final product was a mould bearing the negative of the image shown in Fig. 1.
Micro-model Production
The wafer was used as a mould for the fabrication of the micro-models. A mixture of 50 g of PDMS and 5 g of curing agent was prepared. The mixture was degassed in a vacuum chamber, before it was poured carefully into a petri dish containing the mould. In another petri dish, we poured enough mixture to make a solid slab for covering and sealing the micro-model. The two petri dishes were degassed in a vacuum chamber before they were cured in the oven at 68 \(^{\circ }\)C. The two cured parts were removed from the petri dishes and placed in a small chamber for the silanization step (Zhou et al. 2010). Usually, the silanization step is done after the model is sealed (Karadimitriou et al. 2013). However, in order to prevent the potential effect of this treatment on the pressure sensors, which could affect their performance, we performed the silanization process prior to the insertion of the pressure sensors and the sealing of the micro-model.
The final steps in the manufacturing of the micro-model were the insertion of the pressure sensors and the bonding of the two slabs of the micro-model. First, the sensors were placed by hand in the pre-set locations. Finally, the two slabs were bonded together with a corona discharge (Haubert et al. 2006) and then the micro-model was kept in room temperature for 24 h for the bonding to mature. Although the silanization step preceded the bonding of the micro-model, we didn’t encounter issues with sealing the micro-model.
Fibre Optic Pressure Sensors
Obviously, a pressure sensor for pore-scale measurements must have the same or smaller dimensions as the pores. Traditional pressure sensors have at least one order of magnitude larger dimensions, usually in the range of millimetres. Therefore, they cannot fit in the pore space of a micro-model. Fibre optic pressure sensors (Bao et al. 2013) can be used for measuring pressure at this scale. These are miniature fibre optic piezometers (FOP - MIV) (Smartec), which are used for fluid pressure measurements in live tissues. The sensors used in this micro-model are the FOP-M260-SHEATHED model (Fig. 3). These sensors have a diameter of 260 \(\upmu \hbox {m}\), and they are covered with a protective sleeve, which gives an overall diameter of 320 \(\upmu \hbox {m}\).
A schematic presentation of the pressure sensor is shown in Fig. 3. The sensor consists of the following parts: a cylindrical cavity formed between a flexible membrane, with a reflective inner surface, and a reference optical surface at the optical fibre end. This configuration constitutes a Fabry–Pèrot interferometer (Totsu et al. 2005). The fluid pressure acting on the membrane deforms it. This consequently changes the cavity’s length. The light, emitted from a light source travels through the optical fibre into the cavity, reflects the membrane’s surface and finally travels back though the optical fibre to the spectrometer. The measured spectrum of the light, altered by the change in cavity length, is translated into pressure.
Their measurement range is from − 40 up to 40 kPa, with a resolution of 40 Pa and accuracy of 0.6% of the full range, which makes them ideal for monitoring pressure at the pore scale. Moreover, the acquisition rate of 250 Hz is sufficient for fast monitoring of pressure changes commonly encountered in dynamic two-phase flow experiments. The sensors were tested in various ways. First, we used them to measure air pressure under controlled conditions. In another test, we placed a sensor at the bottom of a graded cylinder filled with one metre of water. The level of water was reduced by increments of 5 cm and the sensor readings were collected. We found a strictly linear variation of the sensor readings with the height of the water. Next, once the sensors were embedded in the micro-model, we saturated the micro-model with the wetting phase and subjected it to a known pressure. We then recorded sensors readings under no flow conditions. In all cases, deviations of the pressure measurements from known values were in the range of the resolution (i.e. 40 Pa). Finally, we checked pressure measurements during steady-state single-phase flow experiments at known flow rates. Experiments are described shortly. Results showed that the sensors response with flow rate was linear, as it is shown in Fig. 4.