Gas Turbine

Gas Turbine .

Specification: Gas Turbine

• Function and behaviour during operation of a gas turbine
• Single-shaft arrangement for operation as jet engine
• Two-shaft arrangement for operation with power turbine
• Start-up fan to start the gas turbine
• Asynchronous motor with frequency converter as generator

Technical Data

• Gas generator (compressor and turbine)
• Speed range: 60000...125000min-1
• Max. pressure ratio: 1:2,2
• Max. mass flow rate (air): 0,125kg/sec
• Max. fuel consumption: 120g/min
• Fuel nozzle pressure: 2,5...4bar

Power turbine

• Speed range: 10000...40000min-1
• Mechanical power: 0...2kW
• Electrical power: 0...1,5kW
• Sound level at 1m distance: max. 80dB(A)

Operation as jet engine

• Thrust measurement: 0...50N
• Sound level at 1m distance: max. 110dB(A)

Measuring ranges

• Temperature: 6x -200...1000°C / 1x -40...1300°C
• Speed: 0...199999min-1
• Electrical power: 0...1999W
• Fuel mass flow rate: 0...10kg/h
• Fuel supply pressure: 0...25bar
• Fuel nozzle pressure: 0...4bar
• Combustion chamber pressure loss: 0...50mbar
• Pressure, turbine inlet in gas generator: 0...2,5bar
• Pressure, power turbine inlet: 0...250mbar