Gas Turbine Jet Engine ‘TH-3133’
Experiments :
- Demonstration of the Turbo jet principle.
- Performance analysis of a Turbojet at varying power.
- Be haviour during operation of a jet engine including Start-up procedure.
- Determination of the specific thrust
- Determination of the specific fuel consumption
- Determination of lambda (fuel-air ratio)
Features
- Fully operational turbojet engine for real-time demonstration
- Mounted on a wheeled trolley for mobility and convenience
- Integrated sensors for temperature, pressure, speed, and thrust measurement
- Mimic diagram display for easy visualization of engine parameters
- Electronic thrust measurement system
- Engine Control Unit (ECU) with throttle control
- Electric starter for smooth and automatic start-up
- Optional LabVIEW-based data acquisition software
Technical Specifications
- Thrust Range: 10 – 100 N
- Maximum Thrust: 100 N (≈10 kg)
- Max Speed: 120,000 RPM
- Idle Speed: 32,000 RPM
- Fuel Type: Kerosene with jet oil
- Fuel Consumption: ~550 ml/min (at max thrust)
- Pressure Range: Up to 4 bar
- Temperature Range: Up to 1200°C
- Force Measurement: 0 – 200 N
System Components
- Single-stage centrifugal compressor
- Combustion chamber with multiple fuel injectors
- Single-stage turbine
- Tailpipe for thrust generation
- Linear thrust measurement system
- Calibrated airflow inlet system
Scope of Delivery
- 1 × Experimental Unit
- 1 × Instructional Manual
- Optional: Data Acquisition Software (LabVIEW-based)
Gas Turbine Jet Engine (TH-3133) is a high-performance educational test unit designed to demonstrate the working principles and performance analysis of a real turbojet engine. Built for engineering laboratories and training institutions, this system provides hands-on experience with jet propulsion, making complex thermodynamics concepts easy to understand.
This fully functional turbojet test stand allows users to study engine behavior under different operating conditions. It features a compact, aero-derivative jet turbine capable of producing measurable thrust, making it ideal for practical demonstrations and experiments.
The unit is mounted on a movable trolley for easy positioning and includes a complete instrumentation system to monitor critical parameters such as temperature, pressure, airflow, fuel consumption, and rotational speed. With both manual control and optional data acquisition software, users can perform detailed performance analysis and energy balance calculations.
