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Skydrol

Hydraulic Test Rig to supply flow & pressure requirements to test an aircraft Wing Tip Brake

At a glance

Fluid: Skydrol LD-4.

4kW Pump / motor set (4.5 lpm / 350 bar)

All filtration Hydac

Scope

Design & manufacture a Hydraulic Test Rig to supply the necessarily flow & pressure requirements to test an aircraft Wing Tip Brake (WTB).

The project featured

  • Fluid: Skydrol LD-4
  • 4kW Pump / motor set (4.5 lpm / 350 bar)
  • 4 x Proportional pressure control c/w close loop feedback
  • Snapmaster data acquisition system
  • All filtration Hydac

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