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About: Test Equipment For Aircraft Servo Valve- This test equipment is meant for functional testing and priming of Aircraft unit with ATF at room temperature and at 120° C temperature. The Test Equipment is sub-divided into following Sub-sections :- 1- Hydraulic Circuit – The functions of the fuel system is to: • Feed the unit with fuel. • Supply constant pressure lines of 120 Kgf/cm2 & 250 kgf /cm2. • Maintain drain pressure 1.8 to 2.7 kgf/cm2. This Circuit can be further divided into: a) Tank Unit: This includes minimum 100 liters Tank & 50 liters Tank (for ATF) b) Pump Unit: – This includes Loading Section, inlet from Pump (rated 10 kgf/cm2) to Test Unit (rated 120 kgf/cm² ,30 LPM & 250 kgf/cm², 15 LPM & 50 kgf/cm², 30 LPM ) c) Test Equipment Driving Unit: This includes Test Equipment driving motor (7.5 KW) d) Drain Unit: This unit consists of Pilot operated pressure relief valve which maintains a Pressure of 1.8 to 2.7 kgf/cm2 in the drain line. e) Cooling system:-this system is consist of plate type heat exchanger, cooling media -water 2- Preservation Circuit – Includes Circuit which is used to Provide separately. This Circuit can be further divided into: a) Tank Unit: This includes minimum 50 litre Tank (for ATF) b) Pump Unit: – This includes Loading Section, inlet from Pump (rated 10 kgf/cm2) to Test Unit (rated 50 kgf/cm²,30 LPM) 3- Power Supply:- 27 V DC power supply. ELECTRICAL CONTROL PANEL: The Control Panel Consist of Switch & Indicator for Power ON/OFF , Switch & Indicator for Pump Motor M1,M2,M3 , Switch & Indicator For drive motor M4, Temperature Indicator & Controller ,Indicator For Over Temperature , Indicator For Speed of drive with control knob , Indicator for the fluid level in tanks T1 & T2 (High/Low) 27VDC (10A) power source The Control Panel for Equipment for Flushing of Aggregates, is attached. Specification: Tank : 400&150 Litre Various Types Valves: Ball Valve, Constant Pressure Valve, Pressure Relief Valve, Pilot Pressure Relief Valve, Needle valve Tank Unit: This includes minimum 50 litre Tank. Pump Unit: This includes Loading Section, inlet from Pump (rated 10 kgf/cm2) to Test Unit (rated 50 kgf/cm²,30 LPM ) Power Supply : 27 V DC power supply Working Fluid: ATF (Aviation Turbine Fluid) Maximum Working pressure of fluid: 204 kgf/cm² Working Temp: 20 to 120 deg C Fineness Of Filtration: 6 - micron Phase: 3 Voltage: 415±10% Frequency: 50±1Hz Application: This test equipment for Aircraft Servo Valve. Key Features: Hydraulic Circuit Preservation Circuit Power Supply Test Equipment Driving Unit Cooling system Web Link- Test Equipment For Aircraft Servo Valve https://neometrixgroup.com/products/t... #aircraft #indianairforce #machine #defence #defencenews #manufacturer #manufacturing #servovalve #ATF #hydraulic #hydraulictechnology #neometrix #neometrixdefence #testrig #testbench #hydraulicmachines #aircraftfuelpump #testequipment #AircraftServoValve #valve Follow us on below links for more updates: / neometrixgroup https://x.com/neometrixgroup / neometrix / neometrixdefencelimited Contact Details: Neometrix Defence Limited E-148, Sector-63, Noida India – 201301 Mobile No. - +91-01204500800, +91-9871243732 Contact: [email protected]