Axial turbine test rig

The axial turbine test rig has been used successfully for decades for scientific experiments on a pilot plant scale. Thanks to its flexible design, differently scaled high-, medium- and low-pressure blading can be examined. The test rig is used for both basic research and practical development projects.

Description

Areas of application

  • Aerodynamics: Aerodynamic investigations in single and multi-stage axial turbines

  • Blading: Investigation of flexible blade types

  • Blade vibrations: Analysis of forced and aeroelastically excited blade vibrations

  • Multi-stage effects: Investigation of multistage effects and unsteady aerodynamics

  • Sound and gaps: Analysis of acoustic transport and axial gap investigations

Main research areas

  • Flow path optimization: Optimization and analysis of cross-stage transient effects

  • Low-pressure turbines: Basic investigations, e.g. wake interaction

  • Aeroelasticity: Investigation of aeroelastic issues and low-load operation

  • Numerical validation: Validation of numerical models, especially for modern high-pressure steam turbines

Technical design and operation

  • Rotor design: Axially long rotor design enables the investigation of up to seven turbine stages

  • Flexible housing: Pressurized housing in steam turbine design, flexibly adaptable to projects through retrofitting

  • Drive: Operation with compressed air, whereby the blading transfers the useful work to the rotor

  • Load machine: Precise speed control independent of mass flow, with transition between load and drag operation

Measurement technology used

  • Pressure and temperature measurement: Type K thermocouples, PT100

  • Vector probes: Steady and non-steady flow vector probes with up to 8 traverses

  • PIV and CTA: Particle Image Velocimetry and CTA probes for flow field analysis

  • Sound measurement: Loudspeaker and microphone measurement technology for analyzing sound transport

  • Comb probes: For the precise detection of inlet and outlet states

Specifications

Stagenumber/ configurations: 0,5; 1; 1,5; 2; 3; 4; 5; 7
Rotor design:


 
1 to 7-stage longitudinally grooved solid rotor
7-stage solid rotor with circumferential grooves
1-stage blisk tie rod rotor
Max. rotational speed: 10.000 1/min
Max. inlet pressure: 4 bar
Max. inlet temperature: 180 °C
Max. flow rate/ mass flow: 20 kg/s
Max. Power: 3.000 kW (electrical)
Min. hub diameter: 270 mm
Max. casing diameter: 480 mm
Weight incl. blading: 6.000 kg