W DOC AIRBUS | AMM A320F

AIR SUPPLY BOOST SYSTEM - DESCRIPTION AND OPERATION


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1. General
The air supply boost-system gives pressure to the potable water system if no bleed air pressure is available. It makes sure that the potable water system works at the correct pressure.
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2. Component Location
FIN FUNCTIONAL
DESIGNATION
PANEL ZONE ACCESS
DOOR
ATA REF
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8MD COMPRESSOR 162DW 171 38-42-00
10MD SWITCH,PRESSURE 161DW 171 38-42-16
3000MM TANK-POTABLE WATER 161DW 171 38-11-41
4205MM VALVE-CHECK 161DW 171 38-41-41
4206MM VALVE,NON RETURN 171 25-10-00
4210MM FILTER-AIR 161DW 171 38-41-42
4212MM FILTER,AIR 171 25-10-00
4215MM SHUTTLE VALVE-AIR 171 38-41-44
4200MM VALVE-PRESSURE REDUCING 161DW 171 38-41-43
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3. System Description
The air supply boost-system supplies compressed air to potable water tank 3000MM. The system operates independently from the bleed air system of the aircraft and the ground-air pressure supply.
The normal pressure of the potable water system is between 25 psi (1.7237 bar) and 28 psi (1.9305 bar).
The system has:
  • Compressor 8MD
  • Pressure switch 10MD
  • Air filter 4212MM
  • Check valve 4206MM.
The check valve is installed on the down stream of the air filter. It makes sure that the pressure flows only in the direction of the potable water tank.
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4. Power Supply
The electric motor that drives the compressor is supplied with 115VAC at 400HZ from 3-phase AC BUS 2. This is switched to the motor through relay 9MD, that is powered from 28VDC GND/FLIGHT BUS.
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5. Interface
Limit switch 5MA at service panel 171AL is connected between 28VDC GND/FLIGHT BUS and pressure switch 10MD. When service panel 171AL is open, relay 9MD is de-energized and stops the electric motor of compressor 8MD. A bayonet-type electrical connector connects 115VAC supply to compressor 8MD.
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6. Component Description
A. The Air Compressor FIN: 8-MD
F Air Compressor ** ON A/C NOT FOR ALL
(1) The compressor is a reciprocating piston type which is electrically driven.
The compressor supplies 3801.6 in.3 (62297.20 cm3) per minute of clean compressed air at 30 psi (2.0684 bar) to the water tank.
The compressor can work continuously to give this pressure and volume of air.
The compressor has:
  • an electric motor,
  • a housing,
  • a crankshaft,
  • bearings,
  • inlet and outlet valves,
  • an inlet filter,
  • a piston rod,
  • a piston cup,
  • a relief valve.
(2) The electric motor is fan cooled and has its own housing. The motor operates at 12000 rpm. A thermal-overload protection circuit stops the motor if it becomes too hot. The thermal-overload protection circuit starts the motor again when the temperature of the motor decreases to the normal temperature.
(3) A driven pulley is connected to a crank shaft which connects to and moves a piston and piston cup in the cylinder. The piston cup is filled with teflon material and is self-lubricating. This is necessary to keep the compressed air output clean.
B. The Pressure Switch 10MD.
Pressure switch 10MD senses the pressure in the potable water tank and sets the electric motor (of the compressor) on and off. At 27.5 psi (1.8961 bar), the pressure switch disconnects the 28VDC line from the relay. This stops the electric motor. When the pressure in the potable water tank is 25.5 psi (1.7582 bar), the pressure switch connects the 28VDC line. This causes the relay to start the electric motor of the compressor to pressurize the system.
C. The Relay 9MD.
Relay 9MD is installed below the aircraft floor at FR 65. It is a 28VDC operated switch that connects and disconnects 115VAC BUS 2 to the electric motor. 28VDC electrical power that operates the relay, is supplied from the GND/FLIGHT BUS. This is supplied through limit switch 5MA of the maintenance door and pressure switch 10MD.
D. Air Filter(s)
(1) Air filter 4212MM:
The air filter stops the ingress of impurities into the system from the air around the compressor.
E. Check valve 4206MM:
The check valve makes sure that the compressed air flows only in the direction of the potable water tank.
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7. Operation
The usual cycle of the compressor increases the pressure in the potable water tank to 28 psi (1.9305 bar). At this pressure, pressure micro switch 10MD stops the power supply to relay 9MD.
If the air pressure in the potable water system decreases less than 25.5 psi (1.7582 bar):
  • Pressure micro switch 10MD energizes relay 9MD.
  • The compressor starts and the pressure in the potable water system increases for one more cycle.
If the air pressure in the system increases more than 27.5 psi (1.8961 bar):
  • Pressure micro switch 10MD de-energizes relay 9MD.
  • The compressor stops.
[Rev.10 from 2021] 2026.04.01 12:37:03 UTC