Research Facilities
Equipment Capabilities
<p>1.Pressure test to assess hydraulic external/internal leakage <br /> 2. Pressure test procedure on fuel systemcomponents <br /> 3.Demonstraion of Hydraulic filter system</p>
Specifications
1. Hydraulic System: (Landing Gear Actuation System)<br /> <font>Includes: Hydraulic Reservoir (tank), Hydraulic<br /> Fluid 30liters, Strainer, 1 hp Motor, Gear Pump,<br /> Selector valve with Pressure controller, double<br /> acting Actuation Cylinder, Return Filter, End<br /> effectors (landing gear Actuation System). Electrical<br /> Panel Board.<br /> 2. Filter clogging: High wing tanks, gravity feed system cum<br /> pressure feed pumps for each tank, carbon filters, RO hoses with<br /> T & L unions, pressure adjuster, Atomizer with 0.5mm hole</font>
Purpose
Lab and Research
Laboratory
Aircraft System Lab