General information           Offer           Departments, laboratories, task groups         Publications          Contact
  PROPULSION DEPARTMENT

TURBOCOMPRESSOR LABORATORY

Fans and compressors testing (primarily mapping) powered by electric drive (2.25 MW) with speed control.
Power demand can be reduced by 50% by throttling flow at inlet (min. absolute pressure 0.5 bar).
Speed ranges: 16564 rpm, 32093 rpm, 44619 rpm (gearbox dependent). Data acquisition system: HP-3497A logger (256 channels) for static measurements, 300 kHz 16/32 channels PC card for dynamic measurements.
Test stand control and measurement instrumentation: basic parameters including vibration monitoring.



 
Aerodynamic Department | Avionics and System Integration Department | Propulsion Department | Landing Gear Department | Prototype Workshops | Strength and Dynamics Department | Aircraft Design Team | Materials & Structures Research Center | EDC

©Institute of Aviation