ASTB-12 Jet Engine Lab Equipment
The ASTB-12 Jet Engine Lab Equipment is an axial flow gas turbine system designed for practical educational purpose. The system consists of a Micro Gas Turbine Engine (MGTE) integrated with sensors and a Data Acquisition System (DAQ). An Electronic Engine Controller continuously monitors the engine to ensure safe operating limits of the engine. A computer-based software is used to manage the engine for real-time data acquisition.
ASTB-12 GUI
- Complete aeronautical axial gas turbine engine
- Real-time thrust measurement software controllable throttle setting with safety limits
- Real-time fuel metering system
- Transparent safety housing for protection while the engine is visible to students
- Standard graph plotting, display parameters, and data logging features for analysis
- Microprocessor-based fully automatic ECU (Engine Control Unit)
Instruments Included (For Data Reading)
Nozzle Area
Exit Total Temperature
Fuel Flow
Shaft Speed (RPM)
Thrust
Compressor Stage
Exit pressure
Inlet Duct (Air Intake) Stage
Inlet temperature
Inlet Pressure
Turbine Stage
Intel total temperature
Inlet total pressure
Exit total temperature
Exit total pressure
Engine Specifications
Thrust: 150 N Max
EGT: 550-750°C
Starting: Automatic Starting
Sequence
Compressor Type: Single Stage
Radial
Typical Fuel: Kerosene, Jet A-1, JP-4,
JP-5, JP-8, bio-fuel and synthetic
fuel.
RPM: 33000~34000 @ Idle, 110,000
@Max
Turbine Type: Single stage
Specifications Of Lab Equipment
Length: 0.9m
Width: 0.5m
Height: 0.4m
Trolley Height: 0.8m
Overall Height: 1.2m
AC Supply: 110/220 VAC 60/50 Hz
Power Consumption: 200 W
DC Supply: 12V 10AH / 11.1V 3S
LIPO