Jet Engine Gas Turbine Manufacturer,Supplier and Exporter in India
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Product Code : SCL-CELE-13932
This laboratory trainer is a compact, robust system designed
to demonstrate the operation and analyze the performance characteristics of an Axial
Flow Gas Turbine engine.
- Engine
Type: Axial Flow Gas Turbine (Single stage radial compressor,
combustion chamber, axial flow turbine).
- Maximum
Performance:
- Maximum
Thrust: 167 Newtons.
- Maximum
Speed: 120,000 revolutions per minute.
- Idle
Speed: 50,000 revolutions per minute.
- Operating
Temperature: Exhaust Gas Temperature is approximately 600
degrees Celsius.
- Fuel:
Operates on standard aviation fuels: Jet A / Jet A1 / low sulphur
paraffin.
- Lubrication:
Requires specific oil mixtures (e.g., 5 percent Mobil JetOil,
Aeroshell 500/550, or Exxon 2380).
Instrumentation and Data Acquisition
The unit features an advanced, computer-controlled data
acquisition system for real-time monitoring and analysis.
- Control
Interface: The engine is controlled via software with a
user-friendly graphical interface.
- Data
Acquisition Device: A high-accuracy 16 channel device is
included (16 Bit, 250 Kilo Samples per second, USB-Based, Make National
Instruments).
- Software: LabVIEW
based Data Acquisition Software is used for performance analysis and
data logging.
- Instrumentation: Full
instrumentation is provided to measure:
- RPM
(Engine Speed)
- Thrust
- Temperature and Pressure
at each stage of the jet engine.
- Air
flow rate
Experiments and Analysis Capabilities
The set-up is ideal for fundamental and applied thermodynamic
and aerospace engineering experiments:
- Operation
Study: Familiarization with and study of the operation of the Axial
Flow Gas Turbine.
- Performance
Metrics:
- Determination
of the specific thrust.
- Determination
of the efficiency of the turbine.
- Recording
the turbine characteristic curves (e.g., thrust versus
RPM).
- Combustion
Analysis: Determination of fuel consumption and the air
and fuel ratio.
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