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Fuel system презентация
Содержание
- 1. Fuel system
- 2. The A320 fuel system is very
- 6. MENU
- 7. MENU
- 8. FUEL PUMPS
- 9. FUEL PUMPS FUEL PUMPS MENU
- 10. TRANSFER VALVE TRANSFER VALVE Two transfer
- 11. ENG 2 ENG 1
- 12. Each inner tank feeds its respective
- 14. XFEED VALVE MENU
- 15. APU
- 16. CTR LEFT RIGHT The fuel system
- 17. This represents the basic fuel system.
- 18. You can see that all the
- 19. MENU
- 20. MENU
- 21. MENU
- 22. For the purpose of clarity, we
- 23. These indications are : - Outer tank fuel quantity,
- 24. These indications are : - inner
- 25. These indications are : -
- 26. - Fuel On Board (FOB),
- 27. - Fuel On Board (FOB), - Fuel used quantity,
- 28. - Fuel used quantity, -
- 29. - Fuel used quantity, -
- 30. The FUEL panel is located on
- 31. Each wing tank pump
- 32. Each center tank
- 33. The MODE SEL pb sw
- 34. The X FEED pb
- 35. MENU NEXT Module
- 36. LIST OF SUBJECTS MENU
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. MENU
Слайд 2
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.
It has fuel tanks located in the center fuselage area and the wings.
MENU
Слайд 6
MENU
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.
and the outer tanks are located in the wings.
Слайд 9FUEL PUMPS
FUEL PUMPS
MENU
Two fuel pumps are installed in the center tank.
And
two fuel pumps are installed in each inner tank.
FUEL PUMPS
Слайд 10TRANSFER
VALVE
TRANSFER
VALVE
Two transfer valves allow fuel to transfer from the outer tanks
to the inner tanks.
MENU
Слайд 12
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
MENU
Слайд 14
XFEED VALVE
MENU
The center tank also feeds the engines.
A cross feed valve
is fitted to connect or isolate the left and right sides.
CTR
LEFT
RIGHT
Слайд 16CTR
LEFT
RIGHT
The fuel system also feeds the APU.
A Low Pressure valve is
fitted to cut off fuel to the APU.
MENU
APU
LP VALVE
Слайд 17
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.
MENU
Слайд 18
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.
Let’s briefly review the basic system using the ECAM FUEL page.
MENU
Слайд 19
MENU
The center tank in the fuselage,
the inner tanks in
the wings,
the outer tanks in the wings,
the outer tanks in the wings,
Слайд 22
For the purpose of clarity, we have left out some indications.
MENU
Click
on the ECAM page to display them.
Слайд 25
These indications are :
- inner tank fuel quantity,
MENU
- center tank
fuel quantity,
- Outer tank fuel quantity,
Слайд 29
- Fuel used quantity,
- Fuel On Board (FOB),
MENU
- Outer
tank temperature,
- Inner tank temperature.
Слайд 33
The MODE SEL pb sw enables the pilot to run the
two center tank pumps in automatic or manual mode.
MENU
This will be explained in detail in the normal and abnormal operation modules.
Слайд 34
The X FEED pb sw enables the pilot to connect or
isolate the left and right sides of the fuel system.
MENU
Слайд 35MENU
NEXT
Module completed
Once again, you will operate all these controls and see
the associated indications in the normal and abnormal operation modules.
Слайд 36
LIST OF SUBJECTS
MENU
SYSTEM INTRODUCTION
FUEL ECAM PAGE
FUEL CONTROLS AND INDICATIONS
FUEL PANEL
LOCATION
EXIT
GLOSSARY
AUDIO
FCOM
RETURN
