TGDEC Turbina de Gás de Dois Eixos, Controlada por Computador (PC)

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

Unit: TGDEC. Computer Controlled Two-Shaft Gas Turbine

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

Unit details

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

TGDEC/CIB. Control Interface Box: The Control Interface Box is part of the SCADA system

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

Process diagram and unit elements allocation

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

TGDEC/SOF. TGDEC Software. Main Screen

COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC
COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC
COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC
COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC
COMPUTER CONTROLLED TWO -SHAFT GAS TURBINE - TGDEC

SISTEMAS INOVADORES

The Computer Controlled Two-Shaft Gas Turbine, "TGDEC", has been designed by EDIBON to study the operation of a two-shaft gas turbine, allowing the analysis of gas generation in the high-pressure turbine and energy conversion in the low-pressure turbine, as well as the interaction between the different systems involved in the process.

Ver descrição geral

NOTÍCIAS RELACIONADAS

Descrição Geral

The Computer Controlled Two-Shaft Gas Turbine, "TGDEC", has been designed by EDIBON to practically evaluate the behavior of a two-shaft gas turbine, analyzing performance, energy balance, and the interaction between its different stages.

The unit is configured with two main shafts:

  • A first shaft corresponding to the high-pressure turbine or gas generator turbine, consisting of:
  • a radial-type compressor,
  • a tubular combustion chamber,
  • and an expansion turbine.
  • The compressor draws in atmospheric air and compresses it, increasing its pressure before entering the combustion chamber, where it mixes with the fuel and combustion takes place. The generated gases expand in the turbine, providing the energy required to drive the compressor, allowing self-sustained operation of the system.
  • A second shaft corresponding to the low-pressure turbine or power turbine, in which the combustion gases, still containing energy, expand and convert their energy into mechanical energy. This energy is transmitted to a generator, enabling electrical energy production and the analysis of the overall system performance.

The "TGDEC" unit also includes:

  • Start system: It consists of a centrifugal fan driven by an electrical motor. Air provided by this fan acts on the blades of the compressor, causing the rotation of the high pressure turbine.
  • Fuel system: The line of fuel gas consists of a ball valve to open or close the feeding, a pressure regulation valve, a safety solenoid valve and an injector. It includes a rotameter type flowmeter to measure de gas consumption.
  • Ignition system: The activation energy of the air-fuel mix will cause the flame ignition. It consists of an ignition electrode or spark plug feeded by an ignition transformer. An ionization electrode detects that the flame is ignited.
  • Lubrication system: It consists of an oil tank of 5 l. From this tank, we dispose of a gear pump to impulse the oil to the bearings of both turbine shafts. The system is completed with a filtration unit and two regulation valves to select the oil quantity to feed to each turbine.
  • Refrigeration system: It consists of a plate heat exchanger and a tubular heat exchanger through which the oil transfers its heat to the refrigeration water.

This Computer Controlled Unit is supplied with the EDIBON Computer Control System (SCADA), and includes: The unit itself + a Control Interface Box + a Data Acquisition Board + Computer Control, Data Acquisition and Data Management Software Packages, for controlling the process and all parameters involved in the process.

EXERCÍCIOS E PRÁTICAS GUIADAS

EXERCÍCIOS PRÁTICOS GUIADOS INCLUÍDOS NO MANUAL

  1. Study of a gas turbine operation.
  2. Determination of the gas turbine efficiency.
  3. Determination of the compressor operation point.
  4. Operation with power turbine.
  5. Determination of fuel consumption.
  6. Thermal efficiency.
  7. Air standard cycle.
  8. Heat balance.
  9. Work ratio.
  10. Pressure ratio.
  11. Pressure loss.
  12. Air and fuel ratio.
  13. Combustion efficiency.
  14. Recording the turbine characteristic curve.
  15. Determination of the efficiency of the compressor.
  16. Determination of the efficiency of high pressure turbine.
  17. Determination of the efficiency of output turbine (low pressure).
  18. Temperatures measurements.
  19. Effective turbine power output.
  20. Safety systems in the operation of a gas turbine.
  21. Sensors calibration

EXERCÍCIOS MAIS PRÁTICOS A SEREM FEITOS COM A UNIDADE

  1. Many students view results simultaneously. To view all results in real time in the classroom by means of a projector or an electronic whiteboard.
  2. Open Control, Multicontrol and Real Time Control. This unit allows intrinsically and/or extrinsically to change the span, gains, proportional, integral, derivative parameters, etc, in real time.
  3. The Computer Control System with SCADA and PID Control allow a real industrial simulation.
  4. This unit is totally safe as uses mechanical, electrical and electronic, and software safety devices.
  5. This unit can be used for doing applied research.
  6. This unit can be used for giving training courses to Industries even to other Technical Education Institutions.
  7. Control of the TGDEC unit process through the control interface box without the computer.
  8. Visualization of all the sensors values used in the TGDEC unit process.
  9. Several other exercises can be done and designed by the user.

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