Test Equipment For Aircraft Servo Valve
Автор: Neometrix Defence Limited
Загружено: 2024-11-06
Просмотров: 177
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...
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#servovalve #ATF #hydraulic #hydraulictechnology #neometrix #neometrixdefence #testrig #testbench #hydraulicmachines #aircraftfuelpump #testequipment #AircraftServoValve #valve
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Contact Details:
Neometrix Defence Limited
E-148, Sector-63, Noida India – 201301
Mobile No. - +91-01204500800, +91-9871243732
Contact: [email protected]
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