Bending Elasticity In Rotors .
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
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