Monday, November 11, 2013

Here are some of the architectural pictures I've captured as I travelled. These are not the original images as I've edited them by Paint.net software.

Adelaide.2011.
Marina Bay Sand, Singapore. 2013.
Perth City, view from on top of a hill. 2011.




Gamma-ray absorption technique and process computed tomography

This research is about measuring tray position in distillation column using gamma-ray absorption technique and process computed tomography. The main purpose of this experiment is to measure the tray position using gamma ray absorption and Process Computed Tomography. Cobalt-60 (Co-60) has been used as gamma source and sodium iodide (NaI) scintillator detector as the measurement device. The activity of Co-60 used in gamma-ray scanning test is 5.12mCi and 2.9mCi for gamma Tomography. The results shows that the trays position in distillation column can be determined using the gamma scanning technique and we can construct the image of the column using the Gamma Tomography method.

Gamma ray scanning often referred as ‘column scanning’ is a convenient, cost effective, fast, efficient and non-intrusive technique to examine inner details of the distillation column as it operates. This method allows engineers to study the tray or packing hydraulics inside a column at any set of online condition. It provides essential data to optimise the column’s performance, extend column run times, track the performance failing effects of fouling and solid deposition, and identify maintenance requirements well in advance of scheduled turnarounds. Based on this, repair downtime can be reduced significantly.


Full setup of Computed Gamma Tomography (CGT) around a distillation column

Components inside tomography machine controller

Trays inside a distillation column


Nanofibers Electrospining : Strontium (Sr) doped zirconia (Zr)

In exploring nanotechnology, researchers have found that zirconium is an element that exhibit valuable characteristic and properties. Zirconia has a very good chemical and thermal constancy, strong, high fracture toughness, high corrosion resistivity and also low thermal conductivity. Due to this, zirconia is extensively applied in most of structural materials, in thermal coating, catalytic supports and others. Zirconia nanofiber can be manufactured through electrospinning process by first producing the polymer solution of zirconia. By combining the right proportion of a polymer, zirconia, ethanol and distilled water the sol-gel (precursor solution to be spun) of zirconia can be produced. 

The aim of this project is to investigate the crystal structure of zirconia nanofiber when it is being doped with strontium with different amount and different temperature of calcination process. The fibre diameter, grain size, crystal type and porosity of the fibre formed will be observed.

Precursor solution on an electric stirrer
Electrospinning is one of the techniques used to produce nanofibers. This versatile technique enables the production of nanofibers from natural polymer, polymer alloy or synthetic polymer. There are three main components for electrospinning process: a spinneret (metal nozzle), a high voltage power supply and a collector. The high voltage power supply is connected to the spinneret and the collector was grounded. Before connecting the components, the solution to be spun is loaded in the syringe and the syringe is connected to a metallic needle (as spinneret). The syringe also will be connected to the syringe pump to let an even feeding rate of the solution.   

Before electrospinning process, precursor solution of zirconia was made. The polymer used in the precursor solution is polyvinyl pyrrolidone (PVP) as it is very soluble in water and ethanol. For the zirconia, zirconyl oxychloride octahydrate (ZrOCl2.8H2O) was used to make the precursor solution whereas the dopant used is strontium carbonate (SrCO3).  


Fibers collected on the drum.

After the solution is ready, it can be prepared for electrospinning process. The solution was loaded into a 10ml syringe and the apparatus was setup as shown in Figure 24. A 20cc needle tip was used in this experiment and it is attached to the syringe before loading the solution. Then the syringe was secured on the syringe pump platform. Before the high voltage power supply was turned on, the earth wire is connected to drum winder while the live wire is connected to the needle tip. To collect the fibers produced easier, the drum winder was wrapped with aluminium foil. As all connection was secured, the drum winder was turned on and the rotational speed was set between 300rpm and 350rpm. The voltage supplied to the needle tip was 22kV and flow rate of the syringe was 0.75ml per hour. The spinning process was completed after 4-5 hours and the collected fibers were stored in a sample container. They were placed in a moisture reducing compartment for overnight.


Crucible containing sample in the furnace and ready to be calcinated

To remove the polymer in the fibers, the samples were calcinated. Each sample was placed in a ceramic crucible and they a placed in the furnace as shown in Figure 25. The calcination temperatures chosen for this experiment is 450°C, 650°C, 800°C and 1000°C. The furnace has a heating rate of 3°C per minute. After the furnace has reached the specific temperature, the temperature point was held for another two hours before it was cooled down.
All fibers collected are stored in sample bottles.


Stubs with samples ready for coating process

Followed after calcination process, the samples were separated for SEM and XRD analysis. For the SEM analysis, the sample was prepared by coating them with platinum layer. Firstly, only a small amount of each sample was needed to place them onto a stub. The stub was sticked with a carbon tape and sample was put onto it.

SEM image of zirconia nanofibers at 20,000x magnification


SEM image of zirconia nanofibers at 5,000x magnification




Composite dome


Composite materials have variety of application due to their advantages over using singular materials such as impact resistance, strength, corrosion resistance and good performance-to-weight ratio. In this laboratory, glass-fibre epoxy composite is constructed using glass fibre sheets and e-proxy resin through prepreg lay-up technique. The prepregs consist of 4 layers of glass fibre, which are partially cured with epoxy resin. E-glass is the most widely used type of glass fibre; it consists of silicon dioxide and metallic oxide and produced by drawing molten glass through a small orifice. The most common applications of glass-fibre epoxy composite are fishing rods, storage tanks and aircraft parts (i.e. fuselage) due to its excellent tensile strength, light weight and low cost.

This laboratory has two objectives. Firstly to construct a single circular E-glass epoxy composite dome that consists 4 layers of E-glass fabric and epoxy resin using a vacuuming process. These 4 layers of glass have different fibre arrangements (biaxial plain weave and tri-axial fibre) and within the composite are aligned to provide maximised strength in several directions. The aim is to create as high a quality composite part as possible. The second objective is to take a note on each step of process, accurately recording data such as the weight of each E-glass layer and the amount of resin consumed by each individual layer of fibre sheet.
The final product produced will be analysed for faults and compared to what would be expected in the industry or what could theoretically be better done.
Measuring and cutting the fibers

The direction of the fiber was marked and placed carefully on the dome mould.
During construction, great care is taken to ensure the individual fibres are not damaged. This is done by radially working the roller on the fibre sheets and avoiding over working any particular section. If too many fibres are damaged, then when the part is put under load the fibres could pull out resulting in failure closer to the failure point of the matrix meaning the fibres have not improved the part as desired.

Resin was applied on the fibers.
An important step in the manufacture of composites is to ensure the matrix material incorporates all the fibres. This is so all forces applied to the composite are properly transferred to all of the fibres. In the lab, it was attempted to ensure this occurs by saturating each fibre layer with resin before applying to the mould. This amount of saturation is determined when the fibre sheet becomes more transparent; but this can be hard to judge and does not absolutely ensure saturation. If there are sections of poorly saturated fibre in the final part than there may be fibres that are not bearing load when the part is put under force, reducing the total strength of the part.

The removal of air bubbles before vacuuming process.

Air was pumped out by vacuum pump.


As the process of preparing each sheet took a considerable amount of time, the resin reservoir progressively hardened and became increasingly difficult to spread. This may lead to issues such as voids of resin where saturation has not occurred but probably has a more pronounced impact on how each layer adheres to each other. If a lamina is not correctly bonded to its surrounding lamina then the matrix material between them could fail under load and the laminate could come apart. Avoiding this issue was attempted by working quickly, but it was still needed to mix additional resin as the first batch hardened before completion of the layering process.

Weight constant


Portion number

Cup (g)

Resin base (g)

Resin hardener (g)

Total resin (g)

1

10.9

242.7

47.1

289.8

2

19.5

57.3

12.8

70.1

Table 1: Weight constant used in the experiment

Weight data


Layer no.

Type

Dry weight of plastic sheet (g)

Dry weight of

Fiber (g)

Remaining resin

Weight (g)

1

Tri-axial

17.6

75.3

9.1

2

Biaxial

21.1

70.8

14.2

3

Tri-axial

17.6

80.6

16.1

4

Biaxial

23.1

78.6

26.7

Table 2: The weight data obtained from the experiment