Devices
Ground frequency tests of aircrafts
- PULSE FFT analyser of dynamic response
- ACCELEROMETER piezoelectric acceleration sensor (14g, 71g, 500g, single-axis, three-axis)
- DYNAMOMETER piezoelectric force sensor (1000 N)
- DRIVERS Energizing electromagnetic vibratory driver for driving construction (0.1Hz to 1kHz)
- RECOVERY BAGS to release the aircraft from the base frame (3pc)
Strength tests of aircraft
- HYDRAULIC CYLINDERS: 25 kN, 50 kN
- DYNAMOMETERS: Strain gauge force sensors GTM series K 25kN, 50kN, 200kN
- GENERATOR BOXES: Inova EU 3000, 3x HBMSpider 8
- CONTROL SYSTEM: Inova EU 3000
- POSITION SENSOR: 15pcs
Experimental aerodynamics
- WIND TUNNEL - 150kW power, measuring space 0,7x0,7m speed 70 m/s
- PNEUMATIC MEASUREMENT - multi-port probes, pressure scanners
- POWER MEASUREMENT - force-measuring units built in measured models
- HOT WIRE ANEMOMETRY - CTA four-channel high-speed data logger
- CALIBRATION OF AERODYNAMIC PROBES - speed and directional calibration
- INTERNAL FLOW - air source for measurement of the flow to 15kW
Measurement turn powertrains
- Software - own measuring program in NI Labview
- Temperatures - T type thermocouple wires
- Media Flow – Flow measurement
- Pressures - the control unit or commercial pressure gauge
- Pull - strain gauge force transducers
Troubleshooting by analytical or numerical procedures
- NASTRAN software for FEM for numerical analysis of internal tension structure, deformation, aeroelasticity or geometry optimization
- FLUENT software for CFD aerodynamic analysis of flow and pressure field
- UN-NX, CATIA software for engineering design and 3D modeling of parts, assemblies and entire aircraft