A320燃油系统介绍

航空

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航空

FUEL MENU System Presentation 1/35
FUEL MENU
System Presentation 2/35
The A320 fuel system is very much like
a conventional jet aircraft fuel system.
It has fuel tanks located in the center
fuselage area and the wings.
FUEL MENU System Presentation 3/35
FUEL MENU System Presentation 4/35
FUEL MENU System Presentation 5/35
FUEL MENU System Presentation 6/35
The center tank is located in the fuselage.
The inner tanks are located in the wings.
and the outer tanks are located in the
wings.
FUEL MENU System Presentation 7/35
The total usable fuel quantity is
approximately 19000 kg (standard density).
1199000000 kkgg
FUEL MENU System Presentation 8/35
FFUUEELLPPUUMMPPSS
FUEL MENU
System Presentation 9/35
FFUUEELLPPUUMMPPSS FFUUEELLPPUUMMPPSS
Two fuel pumps are installed in the
center tank.
And two fuel pumps are installed in
each inner tank.
FFUUEELLPPUUMMPPSS
FUEL MENU
System Presentation 10/35
TRANSFER
VALVE
TRANSFER
VALVE
Two transfer valves allow fuel to
transfer from the outer tanks to the
inner tanks.
FUEL MENU System Presentation 11/35
EENNGG11 EENNGG22
FUEL MENU
System Presentation 12/35
EENNGG11 EENNGG22
Each inner tank feeds
its respective engine.
Two engine Low
Pressure valves are
installed to cut off fuel
to the engines.
ENGINE
LP VALVE
ENGINE
LP VALVE
FUEL MENU System Presentation 13/35
EENNGG11 EENNGG22
FUEL MENU
System Presentation 14/35
XXFFEEEEDDVVAALLVVEE
The center tank also
feeds the engines.
A cross feed valve is
fitted to connect or
isolate the left and
right sides.
EENNGG11 EENNGG22
LLEEFFTT CCTTRR RRIIGGHHTT
FUEL MENU System Presentation 15/35
AAPPUU
EENNGG11 EENNGG22
LLEEFFTT CCTTRR RRIIGGHHTT
FUEL MENU
System Presentation 16/35
AAPPUU
EENNGG11 EENNGG22
LLEEFFTT CCTTRR RRIIGGHHTT
The fuel system also
feeds the APU.
A Low Pressure valve
is fitted to cut off fuel to
the APU.
APU
LP VALVE
FUEL MENU
System Presentation 17/35
AAPPUU
EENNGG11 EENNGG22
LLEEFFTT CCTTRR RRIIGGHHTT
This represents the basic fuel system.
We will now see how this information is presented to the
pilots in the cockpit.
Click on the schematic to display
the ECAM FUEL page.
FUEL MENU
System Presentation 18/35
AAPPUU
EENNGG11 EENNGG22
LLEEFFTT CCTTRR RRIIGGHHTT
You can see that
all the components
we have talked
about are displayed
on the ECAM page.
Let’s briefly
review the basic
system using the
ECAM FUEL page.
FUEL MENU System Presentation 19/35
• The center tank in the
fuselage,
• the inner tanks in the
wings,
• the outer tanks in the
wings,
FUEL MENU System Presentation 20/35
• the fuel pumps,
• the transfer valves,
FUEL MENU System Presentation 21/35
• the engine LP valves,
• the crossfeed valve,
• the APU LP valve.
FUEL MENU
System Presentation 22/35
For the purpose
of clarity, we have
left out some
indications.
Click on the
ECAM page to
display them.
FUEL MENU System Presentation 23/35
TThheessee iinnddiiccaattiioonnss aarree ::
- Outer tank
fuel quantity,
FUEL MENU System Presentation 24/35
TThheessee iinnddiiccaattiioonnss aarree ::
- inner tank
fuel quantity,
- Outer tank
fuel quantity,
FUEL MENU
System Presentation 25/35
TThheessee iinnddiiccaattiioonnss aarree ::
- inner tank
fuel quantity,
- center tank
fuel quantity,
- Outer tank
fuel quantity,
FUEL MENU System Presentation 26/35
- Fuel On
Board (FOB),
FUEL MENU System Presentation 27/35
- Fuel On
Board (FOB),
- Fuel used
quantity,
FUEL MENU System Presentation 28/35
- Fuel used
quantity,
- Fuel On
Board (FOB),
- Outer tank
temperature,
FUEL MENU
System Presentation 29/35
- Fuel used
quantity,
- Fuel On
Board (FOB),
- Outer tank
temperature,
- Inner tank
temperature.
FUEL MENU
System Presentation 30/35
The FUEL panel is
located on the overhead
panel.
FUEL MENU
System Presentation 31/35
Each wing tank pump
is controlled by its
associated pb sw on the
FUEL panel.
FUEL MENU
System Presentation 32/35
Each center tank pump
is controlled by its
respective pb sw.
FUEL MENU
System Presentation 33/35
The MODE SEL pb sw
enables the pilot to run
the two center tank
pumps in automatic or
manual mode.
This will be explained
in detail in the normal
and abnormal operation
modules.
FUEL MENU
System Presentation 34/35
The X FEED pb sw
enables the pilot to
connect or isolate the left
and right sides of the fuel
system.
FUEL MENU System Presentation 35/35 NEXT
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Once again, you will
operate all these controls
and see the associated
indications in the normal
and abnormal operation
modules.
FUEL MENU System Presentation 36/35
LLIISSTTOOFFSSUUBBJJEECCTTSS
SSYYSSTTEEMMIINNTTRROODDUUCCTTIIOONN
FFUUEELLEECCAAMMPPAAGGEE
FUEL CONTROLS AND
INDICATIONS
FFUUEELLPPAANNEELLLLOOCCAATTIIOONN
EXIT
AUDIO GLOSSARY FCOM
RETURN

guanshyy

kkkkkkkkkkkkkkkkkkkkkkkkk

egg8770

好的 下了 学习一下呀！！！

bocome

A320燃油系统介绍

yxnedved

看看~~~~~~~~

leochxq

感谢分享~~看看先~~

tissle

好资料，学习中。。。

diguo

恩。好东西。好好学习一下吧。

ewaszym

谢谢楼主！