Construction of the new test rig
We are building a whole new combustion test rig for a wide range of liquid and gaseous fuels, or a mixture of them. Initially, acoustic, chemiluminescence, and pollutant emissions will be analyzed in the modular system. This project is hosted by the George Jendrassik laboratory of Department of Energy Engineering, funded by the OTKA-FK 124704 grant.
Liquid fuel combustion test is successful
Today is a turning point in the research project. We managed to test all the designed operating conditions of the new test rig. However, this is only the beginning of scientific work to be performed. All the connecting subsystems work flawlessly along with the low-frequency data acquisitions system. There are still several problems to solve, however, the modular structure allows us to work on the rig efficiently.
Hybrid combustion test: done
Following the easier operation with natural gas, the system was prepared for liquid fuel combustion. As the test fuel was diesel oil, a certain extent of air preheating is necessary for smooth operation. The set temperature was only 250 °C initially, which resulted in incomplete fuel evaporation yet. However, a stable operation was achieved with the addition of ~20% natural gas. Calibration of the liquid fuel system’s sensors are under way, and a precision pressure regulator valve will replace the currently used standard variant. It is expected that the test rig will be ready for the first tests with liquid fuels by the end of this month.
First successful hot test is complete
The first hot tests were successful with natural gas as fuel. Even though the picture shows a state with 18 kW thermal power instead of the desired 30 kW, the system performed otherwise flawlessly. Just before this test, the airblast atomizer also performed well with distilled water. The most difficult part of the assembly was to ensure that the central fuel pipe stays there in the small orifice and the annular atomizing medium channel is maintained.
Data acquisition system is online
The measurement system consists of Pt100 resistance thermometers, T and K-type thermocouples, 4-20 mA pressure transducers, and flow meters with 4-20 mA and 0-5 V configurations. All these data will be recorded at 1 Hz since the system will operate in a steady state. This part is the low-frequency DAQ system which is responsible for controlling the environment to provide smooth intakes and record all the variables to facilitate repeatability.
Exhaust gas system is assembled
The flue gas system is consisting of a hood which allows ambient air entrainment. This is mandatory to ensure that the hot flue gas is below 200 °C when it enters the fan. There is a thermocouple before that, and the power can be adjusted by using a frequency converter. The system ran flawlessly at the first test.
First cold test run is completed!
During the design phase, it became evident that the combustion air fan of the system is a key component which should be selected after testing the assembly. However, preceding calculations were made, the combustion air preheater is a complex device to estimate its pressure drop. Therefore, the measurement of flow characteristics required all the burner system assembled which was completed this week. Since the fan of the old test rig was big enough to surely provide the demanded flow rate, it was used to determine the design requirements of the new fan. The effect of air preheating greatly affect the pressure drop, so the combustion air temperature was increased from ambient to 400 °C in 100 °C steps. The task of the upcoming weeks will be the assembly of the flue gas system and the preparation of the burner for hot tests.
Front panel of the power electronic box is getting ready
The previous test rig required too many manual adjustments at several places by the end which required automation and simplification. We are in the middle of the electric design, and only one thing is sure. There will be numerous lamps and buttons. 🙂 The above image is just the beginning.
3D model of the burner is complete
The burner design is ready; now it is submitted for production. It features three inlet ports. The central one is for liquid fuels; the concentric one is for atomizing air. Even though the efficiency of plain-jet airblast atomizer is low, it is convenient for laboratory use. The third intake is responsible for setting the swirl number by injecting air through several side holes. Also, these holes may serve for gaseous fuel injection.
Framework is assembled
We have received the framework of the new test rig and it is now fully assembled. The core part is the burner which is under design. Until the manufacturing completes, the pneumatic and fuels systems will be prepared.
Liquid supply tank
Delivering a constant mass flow rate is quite challenging. Only volumetric pumps exist in the ~1 g/s range which generates oscillations. One solution is choking the flow, however, a more convenient way to use a pressurized tank. A needle valve performs raw adjusting while the gauge pressure does fine tuning. This simple system performed excellently through several test sessions.