TH 150 MINI GAS TURBINE POWER PLANT

ThermodynamicsGas turbines

TH 150 MINI GAS TURBINE POWER PLANT

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The unit is an educational two-shaft gas turbine power plant with a radial flow compressor and axial flow turbines, gear box, generator, and electrical loads as in the modern gas turbine power plant.

The first stage is a hot gas generator. Inlet air through an orifice flow measuring device is compressed by a single stage radial flow compressor. The turbine is motor started and runs on Jet A fuel. Fuel is injected by a fuel pump and ignited in the combustion chamber providing hot gas for a single stage axial flow turbine which in turn drives the compressor. The hot gas is discharged axially to a larger power turbine on the second shaft and exhausts to atmosphere. A fan is provided for cooling the gear box.

The power turbine output shaft is connected to the gear box. An alternator is connected to the gear box by a direct coupling. the electrical output is converted by an inverter to 220 VAC and the electrical power output is connected to a lamp load.

An Electronic Control Unit (ECU) controls the basic turbine operation. Additional instruments are provided for monitoring and controlling the plant operation and performance.

A touch screen computer with an interface unit and software are provided for speed and electrical load control, data display and analysis, and to assist the ECU.

Safety features include safety guard, gas generator over speed shutdown, power turbine over speed protection, power turbine entry over temperature shut down and emergency switch. The unit is floor standing with removable supports.

Instruction manual is also included.

  • Understanding the thermodynamic process.

  • Input power, output power and plant efficiency.

  • Mechanical power of gas turbine (optional)

  • Gas generator  engine construction.
  
- Diffuser: High strength aluminium 
- Combustion chamber: Stainless steel 
- Bearings: Ceramic ball bearing 
- Turbine wheel: Vacuum cast inconel 
- Compressor: High grade aluminium alloy 
  • Gas generator
  
- Running fuel: Jet A or kerosene with jet oil 
  • Power turbine construction.
  
- Turbine wheel: Vacuum cast inconel 
- Interstage guide vane: Stainless steel 
  • Gear box.
  
- Type: Planetary 
- Lubrication: Jet A 
  • Alternator
: Approx. 1.5 kW power 
  • Inverter
  
- Voltage conversion: 12 VDC to 220 VAC 
  • Lamp load
: 600W with individual lamp switch. 
  • Gear box and generator connection
: Direct coupling 
  • Output power
: Electrical approx. 400 W 
 : Mechanical approx. 700 W (required TH150-001) 
  • Accessories
: Engine cooling fan 
 : Gear box cooling fan 
 : Engine exhaust duct 
 : 2 ear muffs 
 : Jet oil 
 : arometer 
  • Sensors
  
- Temperatures: Ambient air, diffuser exit, gas generator turbine entry, power turbine entry and exit. 
- Pressures: Diffuser exit, power turbine entry and exit. 
- Speeds: Gas generator and gear box output shaft. 
- Voltage and current.  
- Fuel flow rate.  
- Air flow rate: Differential pressure at inlet orifice. 
  • Computer Interface unit with software for data display, analysis and control by computer.
  • WiFi feature for data logging and real-time display remotely on smartphone (iOS and Android)
  • Power supply  :  220V 1Ph 50Hz. Other power supply is available on request.

Net (unpacked) shipping dimensions WxLxH  :  100x 125x 110 cm

Net weight  :  Approx. 165 kg

  • TH150-001
Dynamometer for measurement of approximate mechanical power
 - Modification of alternator to dynamometer for torque measurement
 - Torque sensor with signal converter
 - Additional software for torque and power readings.
  • TH150-002
Silencer unit with stand
  • TH150-014
Dynamometer water cooling unit with pump instead of outside water supply.
 - Capacity: 2 RT
SIMILAR PRODUCTS

MT 560 TWO-SHAFT GAS TURBINE, Computer Interface

MT 560 TWO-SHAFT GAS TURBINE, Computer Interface

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Video

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The turbine is a small two-shaft gas turbine engine with a radial flow compressor and axial flow turbines as in the modern gas turbine power plant.

The first shaft is a hot gas generator. Inlet air through an orifice flow measuring device is compressed by a single stage radial flow compressor. The turbine is motor started and runs on Jet A fuel. Fuel is injected by a fuel pump and ignited in the combustion chamber providing hot gas for a single stage axial flow turbine which inturn drives the compressor. The hot gas is discharged axially to a larger power turbine on the second shaft and exhausts to atmosphere. A fan is provided for cooling the gear box.

Speed of the power turbine is reduced by the gear box. A water brake absorber is connected to the gear box for power measurement. The brake requires outside water supply. Load is manually controlled.

An Electronic Control Unit (ECU) controls the basic turbine operation. Additional instruments are provided for monitoring and controlling turbine performance.

A touch screen computer with an interface unit and software are provided for speed control, data display and analysis, and to assist the ECU.

Safety features include safety guard, gas generator over speed shutdown, power turbine over speed protection and power turbine entry over temperature shut down. The unit is floor standing with removeable supports.

Instruction manual is also included.

  • Understanding the thermodynamic process

  • Torque vs speed.

  • Power input and output and engine efficiency

  • Gas generator construction
    
- Diffuser: High strength aluminium.   
- Combustion chamber: Inconel   
- Bearings: Ceramic bearing   
- Turbine wheel: Vacuum cast Inconel   
- Compressor: High grade aluminium alloy   
  • Gas generator
    
- Starting and running fuel: Jet A or kerosene with jet oil.    
  • Power turbine
    
- Turbine wheel: Vacuum cast inconel   
- Interstage guide vane: Stainless steel   
  • Gear box
    
- Type: Planetary   
- Lubrication: Jet A   
  • Dynamometer
    
- Type: Water brake absorber (HD160S)   
- Maximum power: Approx. 5 kW   
  • Gear box and dynamometer connection.
: Direct coupling   
  • Output power
    
- Mechanical: Approx. 700 W   
  • Sensors
    
- Temperatures : Inlet air, diffuser exit, gas generator turbine entry, power turbine entry and exit   
- Pressures : Diffuser exit, power turbine entry and exit   
- Speeds : Gas generator and gear box output shaft   
- Dynamometer torque    
- Fuel flow rate    
- Air flow rate: Differential pressure at inlet orifice.   
  • Accessories
: Engine cooling fan   
 : Gear box cooling fan   
 : Engine exhaust duct   
 : 2 Ear muffs   
 : Jet oil   
 : Barometer   
  • Computer Interface unit with software for data display, analysis and control by computer
  • WiFi feature for data logging and real-time display remotely on smartphone (iOS and Android)
  • Power supply : 220V, 1 Ph, 50Hz. Other power supply is available on request.
  • Net (unassembled) Shipping Dimensions WxLxH:

    100 x 125 x 110 cm

  • Net Weight: Approx. 165 kg
  • MT560-002
Silencer unit with stand
  • MT560-014
Dynamometer water cooling unit with pump instead of outside water supply.
- Capacity: 2 RT
SIMILAR PRODUCTS

MT 553 TURBO JET ENGINE, 200N Thrust, Computer Interface

MT 553 TURBO JET ENGINE, 200N Thrust, Computer Interface

Enquiry

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The engine is a small turbo jet engine and modified for educational purposes. The unit has a radial flow compressor and an axial flow turbine as in the modern jet plane.

Inlet air through an orifice flow measuring device is compressed by a single stage radial flow compressor. The turbine is air started and runs on jet A fuel. The turbine unit is complete with control and monitoring instruments including engine data terminal and automatic start unit. The turbine runs on ceramic bearings. Lubrication is provided by jet oil in the fuel, and no separate lubrication system is required. A fan is provided for engine cooling.

An Electronic Control Unit (ECU) controls the basic turbine operation. Additional instruments are provided for monitoring and controlling the engine performance.

A touch screen computer with an interface unit, and software are provided for speed control, data display analysis, and to assist the ECU.

An engine cover and over speed shutdown are provided.

Instruction manual is also included.

  • Understanding the thermodynamic process

  • Static thrust vs turbine speed

  • Power input and output and propulsive efficiency

  • Engine construction
    
- Diffuser: High strength aluminium   
- Combustion chamber: Inconel   
- Bearings: Ceramic bearing   
- Turbine: Vacuum cast inconel   
- Compressor: High grade aluminium alloy   
  • Engine performance specifications.
    
- Maximum static thrust: Up to 220 N at approx 108,000 rpm   
- Starting and running fuel: Jet A or Kerosene with jet oil   
  • Sensors
    
- Temperatures: Inlet air, diffuser exit, turbine guide vane entry, turbine exit and nozzle exit   
- Pressures: Diffuser exit and turbine exit.   
- Thrust    
- Speed    
- Fuel flow rate    
- Air flow rate: Differential pressure at inlet orifice.   
  • Accessories
: Engine cooling fan   
 : Jet oil, 1 L   
 : 2 Ear muffs   
 : Barometer   
 
  • Computer interface unit with software for data display, analysis and control by computer

   
 
  • WiFi feature for data logging and real-time display remotely on smartphone (iOS and Android)
   
  • Power supply
: 220V, 1 Ph, 50Hz. Other power supply is available on request   
  • Net (unassembled) Shipping Dimensions WxLxH:

    Approx 85 x 115 x 100 cm

  • Net Weight: Approx. 100 kg
  • MT551-001
Kerosene oil (Thailand market only)
  • MT553-002
Silencer unit with stand
SIMILAR PRODUCTS

MT 551 TURBO JET ENGINE, 70N Thrust, Computer Interface

MT 551 TURBO JET ENGINE, 70N Thrust, Computer Interface

Enquiry

Video

Download

The engine is a small turbo jet engine and modified for educational purposes. The unit has a radial flow compressor and an axial flow turbine as in modern jet plane.

Inlet air through an orifice flow measuring device is compressed by a single stage radial flow compressor. The turbine is motor started and runs on fuel. Fuel is injected and ignited in the combustion chamber providing hot gas for a single stage axial flow turbine which inturn drives the compressor. The gas is exhausted through a nozzle at high velocity providing a thrust. The turbine runs on ceramic bearings. Lubrication is provided by jet oil in the fuel, and no separate lubrication system is required. A fan is provided for engine cooling.

An Electronic Control Unit (ECU) controls the basic turbine operation. Additional instruments are provided for monitoring and controlling engine operation and performance.

A touch screen computer with an interface unit, and software are provided for speed control, data display and analysis, and to assist the ECU.

An engine cover and over speed shutdown are provided.

Instruction manual is also included.

  • Understanding the thermodynamic process

  • Static thrust vs turbine speed

  • Power input and output and propulsive efficiency

 

  • Engine construction
    
- Diffuser: High strength aluminium   
- Combustion chamber: Inconel   
- Bearings: Angular contact ceramic bearing   
- Turbine: Vacuum cast Inconel   
- Compressor: High grade aluminium alloy   
  • Engine performance specifications.
    
- Maximum static thrust: Up to 70 N at approx. 150,000 rpm   
- Starting and running fuel: Jet A or Kerosene with jet oil   
  • Sensors
    
- Temperatures: Inlet air, diffuser exit, turbine guide vane entry and exit and nozzle exit.   
- Pressures: Diffuser exit and turbine exit.   
- Thrust    
- Speed    
- Fuel flow rate    
- Air flow rate: Differential pressure at inlet orifice.   
  • Accessories
: Engine cooling fan   
 : 2 Ear muffs   
 : Jet oil   
 : Barometer   
 
  • Computer interface unit with software for data display and analysis by computer
   
 
  • WiFi feature for data logging and real-time display remotely on smartphone (iOS and Android)
   
  • Power supply
: 220V, 1 Ph, 50Hz. Other power supply is available on request   
  • Net (unassembled) Shipping Dimensions WxLxH:

    Approx. 76 x 82 x 87 cm

  • Net Weight: Approx. 70 kg

  • Also available:

    MT 552 TURBO JET ENGINE, 160N Thrust at 120,000 rpm. Similar to MT 551 but larger engine.
  • MT551-001
Kerosene oil (Thailand market only)
  • MT551-002          
Silencer unit with stand
  
  
  
  
  
SIMILAR PRODUCTS