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┃  .*,,.8, ,, ~L,~ A319          ┃              ┃                      ┃
┃                                ┃              ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃              ┃SEQ 105 I ┃I BEY 24  ┃
┃      A~7-~'M" A321             ┃ FUEL SYSTEM  ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━┻━━━━━┻━━━━━┛
The fuel system supplies fuel to the combustion chamber at the required flow rate,
pressure, and temperature.
The fuel flows from the tank, via the fuel
Hydromechanical Unit (HMU) and to the
pump unit and the fuel/oil heat exchanger, to the
fuel nozzles.
~ ".'.'.'.' FUEL FEED                .'.'.'.'.'.'.'.'.'.~ HYDRAULTC
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.70.40     P 2       ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l         POWERFUELNSYSTEM  ┃SEQ 005 1 ┃I REV 23  ┃
┃ aw aw ,, ~L,~ A319             ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
The HP compressor shaft drives the HP fuel pump assembly. Fuel flows through the LP
pump, then through the fuel/oil heat exchanger and the HP pump (gear pump).
The fuel then divides into a filtered flow for the servo fuel heater and the servo valves of
the HMU, and an unfiltered flow for the metering valve of the HMU.
Moving the ENG1 (ENG2) MASTER switch to OFF directly commands the closing of the LP
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(160)