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GENERATOR CONSTANT SPEED DRIVE SYSTEM - DESCRIPTION/OPERATION |
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Schematic diagram of the Constand Speed Drive System. Click on picture for a larger version |
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| Photo showing the components of the Constant Speed Drive unit. | |||||||
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General
Each engine driven generator is driven through a variable ratio transmission.
The transmission supplies the torque to drive the generator at a constant speed
from the variable speed accessory drive pad located on the airplane engine.
Accordingly, the purpose of the constant speed drive may be stated as the
conversion of the varying speed of the jet engine to a constant speed, so that
the generator it drives will produce current at 400Hz within narrow limits.
Constant speed drive consists essentially of a hydraulic transmission with
mechanical controls governing the output rotation speed. The transmission is
capable of either adding to or subtracting from the speed received from the
gearbox in order to provide constant output speed to keep the generator on
frequency. Mechanical (flyweight) governor action keeps the generator output
close to 400Hz. Constant Speed Drive Functional Description At
the lower input speeds, the variable displacement unit acts as a hydraulic pump
to supply flow to the fixed unit which is added to the input speed through the
differential. At the straight through input speed, torque is transmitted
directly through the differential unit and the fixed unit is not rotating. The
variable displacement unit wobbler will be slightly offset from the zero angle
so that some pumping will be accomplished and leakage loses made up. At input
speed above straight through, the variable angle wobbler is set to allow
negative displacement of the variable CSD Mechanical Differential and Hydraulic UnitsThe
differential is a folded type with planet gears in the center and input and
output ring gears on the outside. The planet gears rotate about their own axes
and also revolve about the centerline of the planet gear carrier. The planet
gear carrier is driven by drive input. The variable displacement hydraulic unit
is also driven by the transmission input. The fixed displacement hydraulic unit
is hydraulically coupled to the variable displacement unit and is connected to
the differential through the input ring gear. The output ring gear of the
differential is connected to the transmission output. Constant speed of the
output ring gear is maintained by either adding to or subtracting from the speed
of the planet gears by controlling the direction of rotation and speed of the
input ring gear. The gear and pumps are driven by a constant speed output gear.
(a) Overdrive
(b) Straight through Drive (c) Underdrive
Speed Governor
This magnetically produced torque then works in conjunction with the centrifugal
torque to position the valve stem. The magnetic trim provides a means of
introducing electrical trimming signals to the transmission with out any
additional parts above those already in the governor.
During normal operation the governor accepts oil under pressure, which is
distributed through the flyweight-operated valve to a pressure actuated speed
switch, keeping its electrical contacts open. Charge oil pressure through the governor stem valve allows free
passage of oil to the wobbler control cylinder.
If the output speed falls below the prescribed limit, spring force becomes
greater than centrifugal force on the flyweights, resulting in the displacement
of the stem valve to cause drainage of oil from the pressure (speed) switch
through the governor housing to the sump. Release of pressure on the speed
switch results in completion of the electrical circuit which sends an
under-speed signal to the generator control unit. If the CSD output speed exceeds the prescribed limit, centrifugal force on the flyweights causes the displacement of the governor stem valve whereby charge pressure is cut off from the speed switch and is ported through the governor stem valve to the sump. The drop in pressure in the switch allows the contacts to close, causing the generator circuit breaker to trip. Also the oil from the control cylinder is allowed to drain to the sump. Since charge oil is always present on the side of the control cylinder piston which has the smaller cross sectional area, removing pressure from the side with the larger area causes the piston to actuate in such a direction that the variable displacement unit wobbler moves through the vertical position and comes to rest against a stop pin.
Therefore, if the output speed of the CSD exceeds prescribed limits,
the action to the governor also causes the transmission assembly to assume
minimum speed ratio. The CSD will continue to be at minimum speed ratio as long
as charge pressure is available to keep the control cylinder from resetting to
its normal operating position. Normally, sufficient charge pressure will be
available during flight to prevent the wobbler control cylinder from resetting.
A reset is affected automatically when all input speed to the CSD ceases.
From the above it is evident that the governor performs two protective
functions. First, centrifugal force causes the governor to assume its over-speed
position and second, as the input speed drops the governor valve spring puts it
in the under-speed position. A third protective function is performed by the
fail-safe spring should the governor drive mechanism fail. When this happens and
the governor stops rotating, the fail-safe spring takes over for the motionless
flyweights and moves the valve sleeve against a stop, equivalent to a maximum
under-speed position for the governor. This then provides the desired
under-speed response to a mechanical failure in the governor gears. Hydraulic system
The scavenge pump is located in the hydraulic circuit between the transmission
sump and the external oil cooler. The scavenge pump picks up lube oil and
internal leakage and pumps it through the external oil cooler into the all
attitude reservoir.
Scavenge oil pumped through the cooler returns to the transmission reservoir via
the swirl chamber. This return oil, which is highly aerated, enters the swirl
chamber at high velocity through a tangential inlet, causing a swirling action,
which creates a vortex within the swirl chamber. Air entrained in the entering
oil, having a lower density than the oil, moves to the center of the vortex and
escapes to the case. The oil, relieved of its entrained air, moves along the
wall of the swirl chamber and out into the reservoir.
As described above, return oil is always de-aerated and ported to the reservoir,
regardless of transmission attitude. The inlet suction port is located in
approximately the center of volume of the reservoir, and the volume of oil
contained within the reservoir is such that, regardless of transmission
attitude, the inlet port will always be surrounded by oil. Static pressure in
the reservoir is approximately the same as case pressure. The charge relief valve regulates the operating pressure of the charge oil system. The valve accomplishes this function by metering the discharge of oil from the charge oil system to maintain the preset charge pressure. The charge pump draws oil from the reservoir and delivers a constant volume of oil to the charge relief valve cylinder. The piston in the relief valve cylinder is moved back by oil pressure compressing the spring.
Oil is bled to the sump as
determined by spring pressure against charge pressure acting on the piston. The
oil under charge pressure is used for control in the governor and control valve
and to replenish the oil used in the multiple piston hydraulic units through the
stationary port plate. When charge pressure reaches a determined value, the
electrical contacts on the charge pressure switch open, interrupting a circuit
to extinguish a CSD oil pressure indicator light on the cockpit instrument panel.
The filters are used to filter the oil in the hydraulic system. The charge
filter, functionally located in the charge pressure line is equipped with a
bypass around the filter element to ensure a flow of oil in case the element
becomes clogged. The other filter is in the scavenge line between the scavenge
pump and the reservoir.
Case pressurization is required when the constant speed drive is operated at
higher altitudes, or at higher than ambient temperature. This pressurization is
maintained by use of a vacuum break check valve. During normal operation, when
case pressure is equal to or above atmospheric pressure, the vacuum break check
valve remains closed. In this way, atmospheric air that is entrapped at low
altitudes is retained within the transmission case until the constant speed
drive develops a negative case pressure, or vacuum. During this condition the
vacuum break check valve opens and allows atmospheric air to enter the case
replenishing the air supply. As vacuum is relieved and case pressure equalises,
the vacuum break check valve closes.
A temperature and pressure sensitive valve, or thermal bypass valve, located in
the transmission allows oil to bypass the cooler until it reaches a temperature
of 100 degree F. at this temperature the valve closes and the oil is directed
through the cooler. The valve will also open at a preset pressure, to allow oil
to bypass, if the cooler should become damaged or clogged. Generator Drive Disconnect
Generator Drive Cooling An oil temperature rise indicating system shows abnormal operation of the CSD, whereby the opportunity is afforded to allow corrective action, such as disconnecting the CSD, before total failure occurs. Temperature bulbs, mounted in the scavenge filter downstream from the scavenge pump and in the integral tank, sense the temperature of the operating oil before and after it is subjected to cooling. The oil IN temperature bulb in the tank and the oil OUT bulb in the scavenge line are connected to form a bridge circuit with a CSD OIL TEMP indicator in the cockpit's instrument panel. The difference in temperatures sensed by the two bulbs is indicated by a meter movement on two ranges of the indicator. In the event that the oil cooler becomes clogged or damaged a cooler bypass valve opens at a preset value and directs return oil around the cooler. References : Boeing Aircraft Maintenance Manuals Airbus Aircraft Maintenance Manuals
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