29. Hydraulic
Short Description
A32...
Description
A320 – HYDRAULIC
A320 – HYDRAULIC
•• OVERVIEW OVERVIEW •• SYSTEM SYSTEM DESCRIPTION ••DESCRIPTION NORMAL NORMAL OPERATION OPERATION •• ABNORMAL ABNORMAL •OPERATION QUIZ •OPERATION QUIZ
A320 – HYDRAULIC SYSTEM OVERVIEW
AIRBUS A320 – HYDRAULIC
The A320 features 3 hydraulic systems. To make things easy, let’s call them GREEN, BLUE and YELLOW. They operate continuously at 3000 psi. Transfer of fluid between systems is NOT possible. Every system has its own reservoir.
G RSVR
B RSVR
Y RSVR
Each system has its own pump or pumps, which provide hydraulic pressure to feed the different users such us landing gear, reversers, flight controls, etc. The fluid then comes back to the reservoir.
AIRBUS A320 – HYDRAULIC
USERS
PUM P
G RSVR
USERS
USERS
PUMP S
PUMPS
B RSVR
Y RSVR
The three systems feature accumulators, priority valves, shutoff valves, filters and leak measurement valves. This will be reviewed later in detail. It is also possible to transfer PRESSURE (not fluid) from the GREEN system to the YELLOW and vice versa.
AIRBUS A320 – HYDRAULIC
USERS
PUM P
G RSVR
USERS
USERS
PUMP S
PUMPS
B RSVR
Y RSVR
A320 – HYDRAULIC SYSTEM DESCRIPTION
The green pump is powered by engine 1.
AIRBUS A320 – HYDRAULIC
1
The blue system is pressurized by an electric pump. There is also a Ram Air Turbine (RAT) available to be used in abnormal operations.
ELE C
AIRBUS A320 – HYDRAULIC
1
RA T
The yellow main pump is driven by engine 2. If the engines are stopped, hydraulic power is available through an electric pump. If there is no electrical power at all, the cargo doors can be operated with a hand pump.
ELE C
AIRBUS A320 – HYDRAULIC
1
RA T
ELE C
2
The layout is easy to remember using the “1, 2, 3” rule: The GREEN system has 1 PUMP, the BLUE one has 2 PUMPS, and the YELLOW one has 3 PUMPS.
AIRBUS A320 – HYDRAULIC
1 PUMP
2 PUMPS
3 PUMPS
There is also a bidirectional Power Transfer Unit (PTU) which allows the yellow system to pressurize the green system and vice versa. It turns on if the differential pressure between the two systems exceeds 500 PSI. Note that no fluid at all is being transferred.
AIRBUS A320 – HYDRAULIC
PT U
A320 – HYDRAULIC ADDITIONAL COMPONENTS
SYSTEM ACCUMULATORS There are one accumulator per system to cope with transient demands and provide with some reserve pressure when no pump is working at all.
AIRBUS A320 – HYDRAULIC
ACC U
ACC U
ACC U
PRIORITY VALVES If the system pressure gets low, priority valves will cut off power to heavy load users such as landing gear, slats, flaps and the emergency generator.
GREEN HEAVY USERS • LANDING GEAR • SLATS & FLAPS
AIRBUS A320 – HYDRAULIC
• FLAPS
• EMER GEN • SLATS PR VAL VE
USERS
YELLOW HEAVY USERS
BLUE HEAVY USERS
PR VAL VE USERS
PR VAL VE USERS
FIRE SHUTOFF VALVES The green and yellow systems feature a shutoff valve each which can be closed by the crew during abnormal operations. This is done by pressing the ENG 1(2) FIRE pushbutton.
1 ENG PUMP
AIRBUS A320 – HYDRAULIC
SHUTO FF VALVE
2 ENG PUMP
SHUTO FF VALVE
LEAK MEASUREMENT VALVES AND FILTERS
AIRBUS A320 – HYDRAULIC
In order to measure the leakage in each system, three leak measurement valves have been set upstream of the accumulators and the primary flight controls. They can be closed through their own pushbuttons in the cockpit maintenance panel. Several filters are also installed to clean the fluid all thorough the system.
RESERVOIR PRESSURIZATION The reservoirs are pressurized with HP bleed air from engine 1. If this pressure is too low, the system takes bleed air from the crossbleed duct.
1
AIRBUS A320 – HYDRAULIC
XBLEE D DUCT
DISTRIBUTION
AIRBUS A320 – HYDRAULIC
Get familiar with the users of the three different systems. Be aware that this layout may change depending on the serial number. For example, the Nose Wheel Steering may be powered by the yellow system as well.
A320 – HYDRAULIC INDICATIONS
ECAM HYD PAGE We are progress.
in
cruise
making
good
AIRBUS A320 – HYDRAULIC
Please call the ECAM HYD PAGE now.
ECAM HYD PAGE
AIRBUS A320 – HYDRAULIC
Well done. This is the HYD page during normal operations in-flight. The three systems are working properly. Let’s take a look at the meaning of every symbol in there.
ECAM HYD PAGE
AIRBUS A320 – HYDRAULIC
As you can see on the screen, the nominal pressure of every system is indicated on the top, together with the system label. All pumps provide 3000 psi, except the RAT which works at 2500 psi (emergency only).
ECAM HYD PAGE
AIRBUS A320 – HYDRAULIC
If system pressure is above 1450 psi, the system line, the pressure indication and the triangle on top are green. The system label remains white. Otherwise all of them become amber.
ECAM HYD PAGE
AIRBUS A320 – HYDRAULIC
Moreover, the three squares (one per system) represent each of the main pumps, with the label “1” and “2” for the engine-driven pumps and “ELEC” for the blue electrical pump.
ECAM HYD PAGE
AIRBUS A320 – HYDRAULIC
[Aquí se continua con los distintos símbolos de la página con fotos sacadas del VPT]
TRIPLE INDICATOR
AIRBUS A320 – HYDRAULIC
[Aquí van una foto con el triple indicador y el significado de los indicadores]
A320 – HYDRAULIC CONTROLS
MAIN HYD PANEL
AIRBUS A320 – HYDRAULIC
The main hydraulic panel is located in the upper area of the systems overhead panel.
MAIN HYD PANEL
AIRBUS A320 – HYDRAULIC
The panel features pushbutton switches for the main pumps, the yellow electrical pump and the PTU. There is also a pushbutton for the manual extension of the RAT, guarded in red.
GREE N PUM P
BLUE PUMP (GUARDE D)
YELLO W PUMP
YELLO W ELEC PUMP
A320 – HYDRAULIC NORMAL OPERATION
COCKPIT PREPARATION
AIRBUS A320 – HYDRAULIC
As per the Airbus general rule, all white lights must be extinguished during the scan. It is mandatory to get clearance from the ground crew before applying hydraulic power, since some parts of the airplane may move and cause serious harm.
DO NOT APPLY HYDRAULIC POWER WITHOUT GROUND PERSONNEL CLEARANCE!
COCKPIT PREPARATION
AIRBUS A320 – HYDRAULIC
The accumulator pressure indication must be in the green band. If it is not, turn on the yellow electric pump to recharge the accumulator. Remember: ask for ground clearance first!
COCKPIT PREPARATION
AIRBUS A320 – HYDRAULIC
Let´s put you find the accumulator pressure low. Please get it back to the green band using the yellow elec pump.
COCKPIT PREPARATION
AIRBUS A320 – HYDRAULIC
Well done!
ENGINE START The GREEN and YELLOW pumps will start working when their corresponding engine spools up. The BLUE pump will automatically be turned on after the first engine start.
AIRBUS A320 – HYDRAULIC
The PTU will perform a self-test during engine start-up. A PTU FAULT is triggered if the second engine is started within 40 seconds after the end of the cargo doors operation.
IN-FLIGHT During the cruise scan, the ECAM HYD page should be reviewed. If you see a slight decrease in quantity, it is normal. Particularly the green system is lower than on ground because of the landing gear retraction.
AIRBUS A320 – HYDRAULIC
Fluid contraction during cold soak can also be expected.
A320 – HYDRAULIC ABNORMAL OPERATION
HYDRAULIC ABNORMALS The simple hydraulic abnormal procedures will follow this basic guideline: 1. The system will try to recover automatically the affected part by means of the PTU (if applicable).
AIRBUS A320 – HYDRAULIC
[Aquí va ECAM]
un
pantallazo
del
2. The ECAM will tell the pilot to turn off the affected PUMP and, in case of GREEN or YELLOW LOW LEVEL or OVERHEAT, switch off the PTU to prevent the overheat condition to spread.
AIRBUS A320 – HYDRAULIC
[Aquí va ECAM]
un
pantallazo
del
3. If a system is lost, then the landing distance will be affected since the spoilers, reversers and braking are hydraulically powered.
AIRBUS A320 – HYDRAULIC
[Aquí va ECAM]
un
pantallazo
del
4. If an overheat condition disappears during the approach (FAULT light extinguishes), the system may be recovered.
AIRBUS A320 – HYDRAULIC
[Aquí va ECAM]
un
pantallazo
del
EXAMPLES
AIRBUS A320 – HYDRAULIC
[Aquí van un par de ejemplos con lo que saquemos del VPT]
DOUBLE HYDRAULIC FAILURES
AIRBUS A320 – HYDRAULIC
[Aquí va material con lo que saquemos del VPT]
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