India mechanical laboratory needed for aerospace testing: Hydraulic System (Aircraft landing gear actuation systems)
HYDRAULIC SYSTEM: (Landing Gear Actuation System)
Hydraulic Reservoir: 30 liter capacity
Hydraulic Fluid: SERVO SYSTEM 68
Strainer (Initial filter)
1/2 hp Motor
Gear Pump: DOWTY make, 16 lpm, 180 bar max.
Selector valve: Two Way direction Control Valve
Pressure Gauge: 75 psi
Double acting Actuation Cylinder: Stoke length 300mm
Return Filter: 25 micron
Limit Switches with indicator Light
End effectors (landing gear Actuation System)
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