Ground Support Equipment
The test rigs are designed to test the main and reserve hydraulic systems of an airplane/helicopter under airfield conditions. They have two independent hydraulic circuits. The test rig is mobile, equipped with a set of nodes, controls and measuring instruments, it can perform refuelling of the system.
Characteristics of airplane design:
Characteristics of airplane design:
- Primary line working pressure 35 MPa
- Flow rate 125 l/min per circuit
- Working fluid Skydrol
- Power 90 kW
- Working fluid fineness 3 microns
- Voltage - 3x380V
- Air cooling
- Operating temperature range - 0 ... 50 ° C
- Pressure 8 MPa
- Flow rate 40 l/min per circuit
- Working fluid FH51
- Gas - nitrogen
- Tank 40 liters
- Charging pressure 3 MPa
The test rig can be designed according to a simplified scheme directly connected to the airplane reservoir, without refuelling.
- 2 independent pressure circuits
- Pressure 15 MPa
- Working fluid FH51
- Supply 40 l/min per circuit
- Manual ergonomic control
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