FUEL SYSTEM PRESENTATION MENUThe A 320 fuel system

The A320 fuel system is very much like a conventional jet aircraft fuel system.

MENU The center tank is located in the fuselage. The inner tanks are located

MENU The total usable fuel quantity is approximately 19000 kg (standard density). 19000 kg

FUEL PUMPS FUEL PUMPS MENU Two fuel pumps are installed in the center tank.

TRANSFER VALVE TRANSFER VALVE Two transfer valves allow fuel to transfer from the outer

Each inner tank feeds its respective engine. Two engine Low Pressure valves are installed

XFEED VALVE MENU The center tank also feeds the engines. A cross feed valve

CTR LEFT RIGHT The fuel system also feeds the APU. A Low Pressure valve

This represents the basic fuel system. We will now see how this information is

You can see that all the components we have talked about are displayed on

MENU The center tank in the fuselage, the inner tanks in the wings, the

MENU the fuel pumps, the transfer valves,

MENU the engine LP valves, the crossfeed valve, the APU LP valve.

For the purpose of clarity, we have left out some indications. MENU Click on

These indications are : - Outer tank fuel quantity,

These indications are : - inner tank fuel quantity, - Outer tank fuel quantity,

These indications are : - inner tank fuel quantity, MENU - center tank fuel

- Fuel On Board (FOB), - Fuel used quantity,

- Fuel used quantity, - Fuel On Board (FOB), - Outer tank temperature,

- Fuel used quantity, - Fuel On Board (FOB), MENU - Outer tank temperature,

The FUEL panel is located on the overhead panel. MENU

Each wing tank pump is controlled by its associated pb sw on the FUEL

Each center tank pump is controlled by its respective pb sw. MENU

The MODE SEL pb sw enables the pilot to run the two center tank

The X FEED pb sw enables the pilot to connect or isolate the left

MENU NEXT Module completed Once again, you will operate all these controls and see

LIST OF SUBJECTS MENU SYSTEM INTRODUCTION FUEL ECAM PAGE FUEL CONTROLS AND INDICATIONS FUEL

Скачать презентацию FUEL SYSTEM PRESENTATION MENUThe A 320 fuel system

01_fuel_system__presentation.ppt

Количество слайдов: 36

>FUEL SYSTEM PRESENTATION MENU FUEL SYSTEM PRESENTATION MENU

>The A320 fuel system is very much like a conventional jet aircraft fuel system. 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

>MENU The center tank is located in the fuselage. The inner tanks are located 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.

>MENU The total usable fuel quantity is approximately 19000 kg (standard density). 19000 kg MENU The total usable fuel quantity is approximately 19000 kg (standard density). 19000 kg

>FUEL PUMPS FUEL PUMPS

>FUEL PUMPS FUEL PUMPS MENU Two fuel pumps are installed in the center tank. FUEL 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

>TRANSFER VALVE TRANSFER VALVE Two transfer valves allow fuel to transfer from the outer TRANSFER VALVE TRANSFER VALVE Two transfer valves allow fuel to transfer from the outer tanks to the inner tanks. MENU

>ENG 2 ENG 1 ENG 2 ENG 1

>Each inner tank feeds its respective engine. Two engine Low Pressure valves are installed 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

>XFEED VALVE MENU The center tank also feeds the engines. A cross feed valve 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

>APU APU

>CTR LEFT RIGHT The fuel system also feeds the APU. A Low Pressure valve CTR 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

>This represents the basic fuel system. We will now see how this information is 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

>You can see that all the components we have talked about are displayed on 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. MENU

>MENU The center tank in the fuselage, the inner tanks in the wings, the MENU The center tank in the fuselage, the inner tanks in the wings, the outer tanks in the wings,

>MENU the fuel pumps, the transfer valves, MENU the fuel pumps, the transfer valves,

>MENU the engine LP valves, the crossfeed valve, the APU LP valve. MENU the engine LP valves, the crossfeed valve, the APU LP valve.

>For the purpose of clarity, we have left out some indications. MENU Click on For the purpose of clarity, we have left out some indications. MENU Click on the ECAM page to display them.

>These indications are : - Outer tank fuel quantity, These indications are : - Outer tank fuel quantity,

>These indications are : - inner tank fuel quantity, - Outer tank fuel quantity, These indications are : - inner tank fuel quantity, - Outer tank fuel quantity,

>These indications are : - inner tank fuel quantity, MENU - center tank fuel These indications are : - inner tank fuel quantity, MENU - center tank fuel quantity, - Outer tank fuel quantity,

>- Fuel On Board (FOB), - Fuel On Board (FOB),

>- Fuel On Board (FOB), - Fuel used quantity, - Fuel On Board (FOB), - Fuel used quantity,

>- Fuel used quantity, - Fuel On Board (FOB), - Outer tank temperature, - Fuel used quantity, - Fuel On Board (FOB), - Outer tank temperature,

>- Fuel used quantity, - Fuel On Board (FOB), MENU - Outer tank temperature, - Fuel used quantity, - Fuel On Board (FOB), MENU - Outer tank temperature, - Inner tank temperature.

>The FUEL panel is located on the overhead panel. MENU The FUEL panel is located on the overhead panel. MENU

>Each wing tank pump is controlled by its associated pb sw on the FUEL Each wing tank pump is controlled by its associated pb sw on the FUEL panel. MENU

>Each center tank pump is controlled by its respective pb sw. MENU Each center tank pump is controlled by its respective pb sw. MENU

>The MODE SEL pb sw enables the pilot to run the two center tank 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.

>The X FEED pb sw enables the pilot to connect or isolate the left The X FEED pb sw enables the pilot to connect or isolate the left and right sides of the fuel system. MENU

>MENU NEXT Module completed Once again, you will operate all these controls and see MENU NEXT Module completed Once again, you will operate all these controls and see the associated indications in the normal and abnormal operation modules.

>LIST OF SUBJECTS MENU SYSTEM INTRODUCTION FUEL ECAM PAGE FUEL CONTROLS AND INDICATIONS FUEL LIST OF SUBJECTS MENU SYSTEM INTRODUCTION FUEL ECAM PAGE FUEL CONTROLS AND INDICATIONS FUEL PANEL LOCATION EXIT GLOSSARY AUDIO FCOM RETURN