Laboratory of Turbine Drives

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Description

The laboratory stand is equipped with an automatic measurement system, the system includes measurements of the most important parameters of the gas turbine operation. The measurement is performed on the temperature downstream of the combustion chamber at 32 measuring points, the temperature downstream of the compressor turbine at 16 measuring points, and the temperature downstream of the drive turbine at 32 measuring points. The air mass flow in front of the compressor, the pressure behind the compressor, the compressor turbine and the drive turbine are measured. Precise description http://www.polishcimeeac.pl/Papers1/2016/004.pdf

Examples of research articles:
Publications

10.1515/pomr-2017-0139; 10.2478/pomr-2020-0050

Type of infrastructure:
large research equipment
Strategic infrastructure:
No
Accessibility
scientific research
commercial activities