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What aircraft systems will need to use hydraulics?
Landing gear
Flaps and slats
Flight controls
Nosewheel steering
Wheel brakes
Windshield wipers
Role equipment (cargo doors etc)
Principle of operation
Hydraulic systems provide a means of transmission of power through an incompressible fluid via pipelines and actuators.
What are the six main components common to all hydraulic systems?
Reservoir of oil, which delivers oil to the pump and receives oil from the actuators
A pump, either hand, engine or electrically driven
A selector or control valve, enabling the operator to select the direction of flow of fluid for a required service, and a return path to the reservoir
A jack to actuate the component
A filter, to keep the fluid clean
A relief valve, as a safety device to relieve excess pressure
Active systems
A pump is required to deliver a flow of fluid into the system, and some form of restriction is required to obtain pressure
This restriction is provided by moveable pistons known as jacks or actuators
Constant pressure system
Supplies fluid at a constant rate
Single or double stage gear pump
Pressure applied all the time
Large flow at a small pressure
Fast reaction time when hydraulic services are selected
Needs and ACOV
Demand system
Supplies fluid at a variable volume and controls its own pressure
High pressure built up on demand
Reaction time is much slower
Components last longer as they are not subject to constant pressure
Automatic Cut-Out-Valve (ACOV)
Returns the fluid to the reservoir when:
jacks ready their end of travel
system is not operating
High pressure systems
Weight: smaller actuators, lighter
Force delivered: able to deliver extreme forces
Ease of construction: complex
Pressure delivered: above 2,000psi
Low pressure systems
Weight: more fluid needed, heavier
Force delivered: unable to deliver extreme forces
Ease of construction: simple
Pressure delivered: below 2,000psi
Types of jacks (actuators)
Single acting - normally used as a locking device, the lock being engaged by spring pressure and released by hydraulic pressure
Double acting - because of the presence of the piston rod, the wire of the top of the piston is greater than the area under it. Consequently, more force can be applied during extension of the piston rod. Therefore, the operation which offers the greater resistance is carried out in the direction in which the piston rod extends, eg raising the landing gear
Balanced actuator - equal force can be applied to both sides of the piston, often used in applications as nosewheel steering
Sources of hydraulic pressure
Pumps may be
hand operated
Engine driven
Electric motor driven
Pneumatically driven - air turbine motor (ATM)
Ram air turbine (RAT)
Power transfer unit (PTU) - hydraulic motor driving a hydraulic pump
Hand pump
The hand pump is usually a double-acting pump (delivers oil on both strokes) in a very compact body.
Reservoirs
Stores the hydraulic fluid
Normally pressured but may be vented to atmosphere
It allows for fluid returning from the low pressure side
Holds excess fluid to compensate for leaks
Has a sight glass to check the level when
Pressurised to prevent compression
Fins help to reduce random movement
Accumulators
to store hydraulic fluid under pressure. • to dampen pressure fluctuations.
to allow for thermal expansion.
to provide an emergency supply of fluid to the system in the event of pump failure.
to prolong the period between cut-out and cut-in time of the ACOV, and so reduce the wear on the pump.
to provide the initial fluid when a selection is made, and the pump is cut-out.
Filters
Remove foreign particles from the fluid which will protect the seals and working surfaces in the components
Relief valve which allows unfiltered fluid to pass the system when the element becomes clogged
Hydraulic motors
Converts hydraulic pressure into rotary motion. The speed of a hydraulic motor is dependent on the flow rate of hydraulic fluid into it
Pressure control
Act as safety devices
Thermal relief valves: Prevents overheating, allows pressure to escape 10% tolerance
Full flow relief valves: Fitted downstream and can completely bypass the system
Flap relief: Prevents mechanical overload eg flow relief
Pressure reducing valve: Reduces pressure for devices that don’t need high pressure like 3000psi
Pressure maintaining valve: Sacrifices secondly services to keep the primary services running
Brake control valves: Control pressure in the braking system to prevent skidding
Relief valve
This type of relief valve is used as a final system protection, not as the system pressure controller
Flow control
relief valve
Restrictor valve
Pressure maintaining valve
Shuttle valve
Hydraulic fuse
Shut off valves
Non returning/check valve
Restrictor valve (choke valve)
Reduces fluid flow to slow speed of operation of a service
A one-way restrictor allows full flow in one direction and restricted flow in the other
This can either balance out the speed of operation of an unbalanced ram or allow for difference of operational speed
Pressure maintaining valve
Ensures sufficient fluid flow to the primary controls and wheel brakes
Isolates non-essential circuits if system pressure drops below a set limit
Shuttle valve
One service to be operated by two independent supplies
Guarantees an adequate supply if either system fails
Operates on differential pressure
Typically used to switch to the emergency system for landing gear or flap lowering
Hydraulic fuse
Upstream components shut off flow and prevent fluid loss
Once operated service downstream of fuse will be isolated
System upstream of the fuse should still function normally
Shut off valves
Similar to fuses in that they can shut-off services.
Isn't self regulating but is operated by an external controller. Eg a control on the flight deck.
Typically electrically operated solenoid valve.
Non return/check valve
A non return valve, or check valve only allows flow in one direction. If the pressure down stream increase to that of the supply the valve closes.
Redundancy
Cannot allow loss of hydraulic services
Multiple systems
Transfer to PTU, ATM, RAT if needed
Pressure relays
In the reservoir to warn of overheating of electrical motors
Pressure gauges
Fitted after a constant delivery pump to warm or pump failure
Pressure switches
Transmits fluid pressure to a direct reading pressure gauge
Flow indicator valve
Used to illuminate a warning lamp
Temperature indication
Electrially operated to register main and emergency system pressure