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01 FUEL SYSTEM PRESENTATION.ppt

  • Количество слайдов: 36

FUEL MENU System Presentation 1/35 FUEL MENU System Presentation 1/35

The A 320 fuel system is very much like a conventional jet aircraft fuel The A 320 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 2/35

FUEL MENU System Presentation 3/35 FUEL MENU System Presentation 3/35

FUEL MENU System Presentation 4/35 FUEL MENU System Presentation 4/35

FUEL MENU System Presentation 5/35 FUEL MENU System Presentation 5/35

The center tank is located in the fuselage. The inner tanks are located in 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 6/35

The total usable fuel quantity is approximately 19000 kg (standard density). 19000 kg FUEL The total usable fuel quantity is approximately 19000 kg (standard density). 19000 kg FUEL MENU System Presentation 7/35

FUEL PUMPS FUEL MENU System Presentation 8/35 FUEL PUMPS FUEL MENU System Presentation 8/35

Two fuel pumps are installed in the center tank. And two fuel pumps are Two fuel pumps are installed in the center tank. And two fuel pumps are installed in each inner tank. FUEL PUMPS FUEL MENU System Presentation 9/35

Two transfer valves allow fuel to transfer from the outer tanks to the inner Two transfer valves allow fuel to transfer from the outer tanks to the inner tanks. TRANSFER VALVE FUEL TRANSFER VALVE MENU System Presentation 10/35

ENG 1 FUEL ENG 2 MENU System Presentation 11/35 ENG 1 FUEL ENG 2 MENU System Presentation 11/35

ENG 1 ENG 2 ENGINE LP VALVE Each inner tank feeds its respective engine. ENG 1 ENG 2 ENGINE LP VALVE Each inner tank feeds its respective engine. Two engine Low Pressure valves are installed to cut off fuel to the engines. FUEL MENU System Presentation 12/35

ENG 1 FUEL ENG 2 MENU System Presentation 13/35 ENG 1 FUEL ENG 2 MENU System Presentation 13/35

ENG 1 ENG 2 The center tank also feeds the engines. XFEED VALVE LEFT ENG 1 ENG 2 The center tank also feeds the engines. XFEED VALVE LEFT FUEL CTR MENU A cross feed valve is fitted to connect or isolate the left and right sides. RIGHT System Presentation 14/35

ENG 1 ENG 2 APU LEFT FUEL CTR MENU RIGHT System Presentation 15/35 ENG 1 ENG 2 APU LEFT FUEL CTR MENU RIGHT System Presentation 15/35

ENG 1 ENG 2 APU LP VALVE LEFT CTR RIGHT The fuel system also ENG 1 ENG 2 APU LP VALVE LEFT CTR RIGHT The fuel system also feeds the APU. A Low Pressure valve is fitted to cut off fuel to the APU. FUEL MENU System Presentation 16/35

ENG 1 ENG 2 APU LEFT CTR RIGHT This represents the basic fuel system. ENG 1 ENG 2 APU LEFT CTR RIGHT 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 17/35

ENG 1 ENG 2 APU LEFT CTR RIGHT You can see that all the ENG 1 ENG 2 APU LEFT CTR RIGHT 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 18/35

 • The center tank in the fuselage, • the inner tanks in the • The center tank in the fuselage, • the inner tanks in the wings, • the outer tanks in the wings, FUEL MENU System Presentation 19/35

 • the fuel pumps, • the transfer valves, FUEL MENU System Presentation 20/35 • the fuel pumps, • the transfer valves, FUEL MENU System Presentation 20/35

 • the engine LP valves, • the crossfeed valve, • the APU LP • the engine LP valves, • the crossfeed valve, • the APU LP valve. FUEL MENU System Presentation 21/35

For the purpose of clarity, we have left out some indications. Click on ECAM For the purpose of clarity, we have left out some indications. Click on ECAM page display them. FUEL MENU System Presentation the to 22/35

These indications are : - Outer tank fuel quantity, FUEL MENU System Presentation 23/35 These indications are : - Outer tank fuel quantity, FUEL MENU System Presentation 23/35

These indications are : - Outer tank fuel quantity, - inner tank fuel quantity, These indications are : - Outer tank fuel quantity, - inner tank fuel quantity, FUEL MENU System Presentation 24/35

These indications are : - Outer tank fuel quantity, - inner tank fuel quantity, These indications are : - Outer tank fuel quantity, - inner tank fuel quantity, - center tank fuel quantity, FUEL MENU System Presentation 25/35

- Fuel On Board (FOB), FUEL MENU System Presentation 26/35 - Fuel On Board (FOB), FUEL MENU System Presentation 26/35

- Fuel On Board (FOB), - Fuel used quantity, FUEL MENU System Presentation 27/35 - Fuel On Board (FOB), - Fuel used quantity, FUEL MENU System Presentation 27/35

- Fuel On Board (FOB), - Fuel used quantity, - Outer tank temperature, FUEL - Fuel On Board (FOB), - Fuel used quantity, - Outer tank temperature, FUEL MENU System Presentation 28/35

- Fuel On Board (FOB), - Fuel used quantity, - Outer tank temperature, - - Fuel On Board (FOB), - Fuel used quantity, - Outer tank temperature, - Inner tank temperature. FUEL MENU System Presentation 29/35

The FUEL panel is located on the overhead panel. FUEL MENU System Presentation 30/35 The FUEL panel is located on the overhead panel. FUEL MENU System Presentation 30/35

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. FUEL MENU System Presentation 31/35

Each center tank pump is controlled by its respective pb sw. FUEL MENU System Each center tank pump is controlled by its respective pb sw. FUEL MENU System Presentation 32/35

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. This will be explained in detail in the normal and abnormal operation modules. FUEL MENU System Presentation 33/35

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. FUEL MENU System Presentation 34/35

Once again, you will operate all these controls and see the associated indications in Once again, you will operate all these controls and see the associated indications in the normal and abnormal operation modules. Module completed FUEL MENU System Presentation 35/35 NEXT

LIST OF SUBJECTS SYSTEM INTRODUCTION FUEL ECAM PAGE FUEL PANEL LOCATION FUEL CONTROLS AND LIST OF SUBJECTS SYSTEM INTRODUCTION FUEL ECAM PAGE FUEL PANEL LOCATION FUEL CONTROLS AND INDICATIONS AUDIO RETURN FUEL GLOSSARY FCOM EXIT MENU System Presentation 36/35