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Fuel Feed System: Function

Kenzie Evans Aeronautical Engineering English

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Fuel Feed System: Function

  1. Two methods of Pressure Controlled Fuel Feed

    • High Pressure Pumps
      • Also called override and jettison pumps
      • Deliver twice as much pressure as standard boost pumps
        • Forces discharge check valves on standard pumps to close
          • Prevents fuel flow from standard pumps
    • Sequence Valves
      • Installed at the pump outlets of standard boost pumps
        • Reduce output pressure
          • Allows some fuel back into the tank
  2. Electrical Fuel Feed Management

    • Performed automatically
    • Controlled in accordance with flight phases
    • Taxiing phase, centre tank feeds engines
      • Other pumps on standby
    • Take-off phase
      • Occurs when flaps are extended for take-off
      • Engines supplied individually
        • Two boost pumps from each main tanks 2 and 3 (engines 2 and 3 respectively)
        • Double capacity centre tank boost pumps for engines 1 and 4
    • Cruise phase
      • After take-off when flaps have been retracted
      • Centre tanks and stabilizer tank are emptied first
      • Inner main tanks used next
      • All engines now supplied by double capacity override and jettison pumps in main tanks 2 and 3
  3. Fuel Scavange

    • Reduces amount of non-usable fuel in the tanks
    • Most commonly used method uses jet pumps
    • Boost pumps supply jet pumps with pressure they need for operation
    • Scavenged fuel is pumped to the main inner tank
    • Another method uses electrically driven scavenge pump
      • Controlled automatically as fuel level drops below certain threshold
      • Pump fuel into a main tank
  4. Fuel Recirculation

    • Ensures proper cooling of engine oil and integrated drive generator oil
    • Fuel from tank is pumped through engine oil cooler which heats the fuel and cools the engine oil
    • Fuel then passes through the high pressure gear driven engine pump to the burners on the engine
    • Some fuel is diverted and passes through a bypass valve
      • Proceeds to the Integrated Drive Generator (IDG) cooler
        • Fuel is heated further and then recirculated and mixed with new fuel ready to repeat the process
    • Works well until engine runs at lower speed and there is a high electrical load on the IDG
      • As engine runs slower, the cooling becomes critical as there may not be enough fuel for cooling
    • Solenoid activates on the fuel return valve
      • Return valve opens and returns fuel to the tank
        • Cool fuel is mixed to cool down the hot fuel
  5. Fuel Boost Pumps

    • Generally impeller type
    • Impeller forces fuel from the inlet to the pump outlet by centrifugal force
    • Boost pump can be removed from canister without draining fuel
      • Special removal valve shuts off the fuel inlet as the pump is pulled out

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Aeronautical Engineering (M11 Mind Maps) Mind Map on Fuel Feed System: Function, created by Kenzie Evans on 04/10/2017.
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Kenzie Evans
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