Aircraft Nose Wheel Steering System general description and operation | A320 Nose Wheel Steering System description and operation
Aircraft Nose Wheel Steering Systems
Most aircraft
include a nose wheel steering system that allows the pilot to control the nose
wheel from the flight deck. As a result, the aircraft can be guided while
operating from the ground. Some straightforward aircraft have castering nose
wheel systems. Differential braking is used to guide such aircraft when they
are taxiing.
Nose wheel Steering System General
Small Aircraft Steering System
The majority of small
aircraft may steer by means of a straightforward mechanical linkage system
attached to the rudder pedals. On the bottom strut cylinder, pedal horns are
attached to push-pull tubes. The strut piston axle and wheel assembly turn to
the left or right as a result of the pedals being depressed.
Large Aircraft Nose Steering System
Large aircraft
use a power source for nose wheel steering because of their mass and the need
for positive control. Most power is hydraulic. Large aircraft nose steering
systems come in a wide variety of configurations. The majority have comparable
traits and elements. A small wheel, tiller, or joystick, normally positioned on
the left side wall, is used on the flight deck to control the steering. On some
aircraft, the system can be turned on and off. A steering control unit receives
the controller input movement by mechanical, electrical, or hydraulic
connections.
A hydraulic
metering or control valve serves as the control unit. In order to spin the
lower strut, it sends hydraulic fluid under pressure to one or two actuators
built with different linkages. The fluid in the actuators and system is always
under pressure thanks to an accumulator and relief valve, or equivalent pressurizing equipment. The steering actuating cylinders can now function as
shimmy dampers thanks to this. Various gears, cables, rods, drums, and/or
bell-cranks are components of a follow-up mechanism. Once the steering angle is
attained, it resets the metering valve to its neutral position.
During takeoff
and landing, several systems feature an input subsystem from the rudder pedals
for minor degrees of turns done while controlling the aircraft at high speed.
All systems often have safety valves to release pressure in the event of a
hydraulic breakdown, allowing the nose wheel to swivel.
Through a shaft,
the steering drum inside the flight deck control pedestal is connected to the
nose wheel steering wheel. Through the use of cables and pulleys, the control
drum of the differential assembly receives the steering signal as a result of
the rotation of this drum. The metering valve assembly receives movement from
the differential assembly through the differential link, which then moves the selector
valve to the desired position. This gives the nose gear's hydraulic power
source.
The open safety
shutoff valve directs pressure from the aircraft hydraulic system into a pipe
going to the metering valve. The metering valve then directs the pressurized fluid out of port A and into steering cylinder A through the right turn
alternating line. Since there is only one port, pressure causes the piston to
start extending. The extension of the piston gradually moves the steering
spindle to the right since its rod attaches to the nose steering spindle on the
nose gear shock strut, which pivots at point X. As the nose wheel rotates,
fluid is pushed from steering cylinder B into port B of the metering valve via
the left turn alternating line. The metering valve sends this return fluid into
a compensator, which then sends it to the return manifold for the aircraft
hydraulic system.
As said, the
nose gear rotates as a result of hydraulic pressure. The gear shouldn't be
turned too far, though. Devices that stop the gear at the chosen angle of turn
and maintain it there are part of the nose gear steering system. With the help
of follow-up linking, this is achieved. As previously mentioned, the steering
spindle rotates the nose gear as cylinder A's piston extends. Gear teeth on the
back of the spindle mesh with a gear at the base of the orifice rod. The
orifice rod rotates in the opposite direction from the nose gear and spindle. The
scissor follow-up links, which are situated at the top of the nose gear strut,
receive this rotation from the two portions of the orifice rod. The attached
follow-up drum rotates as the follow-up links return, transmitting movement to
the differential assembly by cables and pulleys. The metering valve is moved
back toward the neutral position by the differential arm and links when the
differential assembly is operating.
Compensator unit
The compensator
unit system maintains constant pressure in the steering cylinder fluid. A
spring-loaded piston and poppet are housed inside a three-port housing that
makes up this hydraulic device. The left port serves as an air vent to keep
trapped air from obstructing the piston's movement at its rear. The metering
valve return port is connected by a line to the second port, which is found at
the top of the compensator. On the right side of the compensator is where
you'll find the third port. The return manifold for the hydraulic system is
connected to this port. When the poppet valve is open, it directs the steering
system return fluid into the manifold.
When the piston
is under high enough pressure to compress the spring, the compensator poppet
opens. This system requires 100 psi. As a result, the pressure holding the
fluid in the metering valve return line is sufficient. The metering valve and
the cylinder return lines are both under the same 100 psi pressure. This keeps
the steering cylinders under pressure at all times and enables them to serve as
shimmy dampers.
Shimmy Dampers
Most nose gear has a tendency to shimmy or oscillation quickly at certain speeds, and torque connections connecting from the stationary upper cylinder of a nose wheel strut to the moving bottom cylinder or piston of the strut are insufficient to prevent this. A shimmy damper must be utilised to control this disturbance. A shimmy damper uses hydraulic dampening to control nose wheel shimmy. Although the damper can be integrated within the nose gear itself, it is often an external element linked to the upper and lower shock struts. It keeps the nose gear steering system operating normally throughout all phases of ground operation.
Steering Damper
Large aircraft
with hydraulic steering, as previously indicated, maintain pressure in the
steering cylinders to give the necessary dampening. Steering damping is the
term for this. Vane-type steering dampers are seen on several vintage transport
aircraft. However, they serve to reduce vibration as well as steer the nose
wheel.
Airbus A320 Nose Wheel Steering system
Description
A hydraulic
actuating cylinder steers the nose wheel. The green hydraulic system supplies
pressure to the cylinder, and electric signals from the BSCU (Brake and
Steering Control Unit) to control the Nose Steering.
The BSCU receives orders from:
- the Captain's and the First Officer's steering control wheels (command added algebraically),
- the rudder pedals,
- the autopilot.
The BSCU (Brake
and Steering Control Unit) transforms these commands into nose wheel steering
angle. That steering angle has the following limits, which depend on ground
speed of the aircraft and the origin of the orders.
The nose wheel steering system receives actuating hydraulic pressure when:
- The A/SKID & N/W STRG switch is on and,
- The towing control lever (installed on nose wheel) is in normal position and, at least one engine is running and,
- The aircraft is on ground.
The logic is
designed in such a way that the nose landing gear doors must be closed in order
for the green hydraulic system to apply pressure to the actuating cylinder.
The handwheel
can turn the nose wheel up to 75° in either direction. A lever on the towing
electrical box (installed on nose landing gear) allows ground crew to
deactivate the steering system for towing the aircraft. This then allows the
wheel to be turned 95° in either direction.
The pilots can
use a pushbutton on either steering handwheel to prevent rudder pedal input or
autopilot input from going to the BSCU. An internal cam mechanism installed returns
the nose wheel to the centered position after takeoff.
Controls and Indicators
Indication on ECAM
Page: The “STERING” LEGEND appears along with an ECAM caution if either the
nose wheel steering system or the Anti-Skid system fails.
The steering
handwheels, which are interconnected for operation from both crew, can steer
the nose wheel up to 75° in either direction.
Note: The
steering system automatically centers the nose wheel after liftoff.
Rudder PEDAL
DISC Push Button: Pressing this button on either handwheel removes control of
nose wheel steering from the rudder pedals until the button is released.
A/SKID
& N/W STRG Switch: This ON/OFF switch activates or deactivates the nose wheel
steering and anti-skid.
MEMO Display: When
the nosewheel steering selector is in the towing position, “NW STRG DISC” is
displayed in green. The legend is in amber color, if one engine is running.
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