Graz University of Technology Institute for Thermal Turbomachinery and Machine Dynamics ·...
Transcript of Graz University of Technology Institute for Thermal Turbomachinery and Machine Dynamics ·...
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Graz University of Technology
Institute for Thermal Turbomachinery
and Machine Dynamics
Facilities -Workshop
Gas Turbine Combustion
Metrology in Turbomachinery – Laser Optical
Metrology
Turbomachinery Optimisation –CFD Methods
Machine Dynamics -Acoustics
TU Graz / TTM, Inffeldgasse 25/A, 8010 Graz Univ.-Prof. Dr.-Ing. Franz Heitmeirhttp://ttm.tugraz.at
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Institute for Thermal Turbomachinery
and Machine Dynamics
The Institute specializes in research and education in the field of
compressors, gas and steam turbines and their application in modern power plants, airplanes and vehicles. The second focus is machine dynamics for all industrial applications.
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Cycle Optimisation
AcousticsMachine Dynamics
Combustion
Computational Fluid Dynamics Experimental Flow Analysis
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Facilities
• Laboratory equipped with modern conventional and laser-optical measurement techniques
• 3 MW Compressor station,
• 5 MW Air heater,
• Two-shaft transonic test turbine facility
• Single-shaft subsonic test turbine facility
• Combustion test rig operating at high temperature and pressure
Cooperation
Funding:
– EU-Projects (FP6 und FP7)
– National projects (FWF, TAKE-OFF and LuFo IV)
Projects: AIDA, DREAM, NEWAC, ALFA-BIRD, CFD-TRANS,…
Partners: MTU, Rolls-Royce, SAFRAN, VOLVO AERO, ITP, AVIO,…
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Examples of Research
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boundary layer probes
LDV, Probes or FRAP
rotateable LP stator
rotateable HP stator
Static pressure taps
∅ 2,5 mm
five hole
probe
Aggressive Intermediate
Duct Aerodynamics
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This project focus on a breakthrough in low noise and low emission engine
architectures. VITAL will achieve this breakthrough by bringing together 53 actors
from the leading European engine manufactures
European Union Project
EnVIronmenTALly
Friendly Aero Engine
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Clocking InvestigationsAustrian Science Fund
Objective of this project is a detailed investigation of the stator-rotor-stator
interaction in a transonic turbine stage. The outcome of this work is a experimental
database for unsteady, transonic flows through a high pressure turbine 1 ½ stage.
1st rotor2nd stator
with window
de-swirler
1st stator
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Combustion Diagnostics
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• Mainly direct contractory work for industry
• Conventional and laser-optical recording of
vibrations
• Recording of sound-pressure
• Component analysis using shakers (up to
20kHz and 180N) and vibration insulated
platforms (appr. 1,8x3m)
• Support for acceptance tests
• Support by Finite Element Analysis.
Acoustics and Machine Dynamics
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Cycle Optimisation - Graz Cyclefuel (natural gas,
synthetic gas)Oxygen (O2)
steam (H2O), carbon dioxid (CO2)at 1400°C and 40 bar
HTT
H2O and CO2
extraction
Condensation
C1LPT
C2
HPT
Steam (H2O)
560 °C, 180 bar
C3
Carbon dioxid (CO2)
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Dream – ValiDation of
Radical Aero Engine Sytems
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AIDA
FWF unst.
CC-Vibrations
NEWAC,
ALPHA-BIRD
VITAL
FWF
Clocking
MassiF
DREAM
BeZwiG
Hoeger-
Lift
AMICA
Aeronautical Research
Programme IV (LuFo IV)
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Thank you for your attention !