Dresden
Technology Portal

 
Your access to research infrastructure and know-how
de|en
After more than 10 years of service, the Dresden Technology Portal will cease operations in the near future.
We will provide a link to the successor service once it goes live.
Please do not update any equipment entries here anymore. Use the new portal from now on.

Equipment of Chair for Turbomachinery and Flight Propulsion

Technische Universität Dresden
Filter:

institutions: this unit(10), daughter units(0),

tags:Infrastruktur(10)

Sort:

10 results

 

Control valve for steam turbines

Facility: Chair for Turbomachinery and Flight Propulsion

Scaled control valve for the experimental investigation of the valve's unsteady operating behaviour.

 

High resolution photogrammetry camera

Manufacturer: GOM GmbH
Model: ATOS Plus
Facility: Chair for Turbomachinery and Flight Propulsion

"The photogrammetry camera delivers up to 29 megapixel resolution capturing high accuracy reference points." [www.gom.com]

 

High resolution, optical 3d-digitizer

Manufacturer: GOM GmbH
Model: ATOS Triple Scan
Facility: Chair for Turbomachinery and Flight Propulsion

"ATOS Triple Scan is a high resolution, optical digitizer that delivers rapid and precise three-dimensional measuring data for the optimization of design processes..." [www.gom.com]

 

ATOS ScanBox

Manufacturer: GOM GmbH
Model: 5108
Facility: Chair for Turbomachinery and Flight Propulsion

ATOS ScanBox - A comprehensive system for automated scan using fringe projection.

 

Deflector Wind Tunnel (UGWK)

Facility: Chair for Turbomachinery and Flight Propulsion

Deflector Wind Tunnel is a continuously operating open wind tunnel in suction mode (Eiffel channel).

 

Plate film cooling channel (PFKK)

Facility: Chair for Turbomachinery and Flight Propulsion

Plate film cooling channel - A rectangular channel for the investigation of film cooling, and internal heat transfer in the cooled turbine blades.

 

Transonic Turbines Cascade Wind Tunnel (TTGWK)

Facility: Chair for Turbomachinery and Flight Propulsion

Transonic Turbines Cascade Wind Tunnel for the investigation of transonic turbine cascades at very low aspect ratios.

 

Low Speed Research Compressor (LSRC)

Facility: Chair for Turbomachinery and Flight Propulsion

The Low Speed Research Compressor is a scaled, low-speed 1- to 4-stage compressor model. It is used for the investigation of flow structures at the stability limit of compressors.

 

Cascade Wind Tunnel (GWK)

Facility: Chair for Turbomachinery and Flight Propulsion

The Cascade Wind Tunnel is a continuously operating, open wind tunnel. It's used for the investigation of turbine or compressor bladings.

1