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The Challenge:
Developing a flexible, rugged and cost effective automated test system for testing the performance of the Starter-Generator at various load conditions.
The Solution:
Developing a flexible, rugged, cost effective automated “Starter Generator Test System” using NI cRIO and LabVIEW.
Introduction:
Briefly, Starter generator rotates the turbine engine fast enough, so the fuel can be ignited and takes over as a generator providing DC power to the electrical system after start in the aircraft.
There are two types; shunt start and series start. The shunt type can usually be identified by having two large terminals and two small terminals located on the terminal block marked A, B, D and E. For starting, terminals B and E supply current to the armature and stator windings. At the same time, voltage is applied to the shunt field terminals A and D from the Generator Control Unit.
Three large terminals on the terminal block marked as C+, B and E- can identify series start type units. Shunt field terminals A and D are located on either side of the larger terminals. Terminals C+ and E- supply current to the armature and stator windings during the start cycle and the starter generator works the same as a DC electric motor. The shunt windings are not used in this mode. Following the starter operation, the Generator Control Unit regulates shunt field current with voltage supplied from generator residual voltage and maintains a nominal system voltage of 28 volts DC.
The Starter Generator is tested in two different modes namely Generator mode and Starter mode to check its performance at various load conditions. Both the modes have a common Control desk & Data Acquisition System (DAS) to control, monitor and store the required parameters.
Generator Mode:
In this mode the equipment used is “Inverter duty AC motor, AC drive, Step up Gear Box, Torque Sensor, Spline Shaft &Cooling blower”. The AC motor and Step up Gear Box were mounted on a Mild Steel base plate. This entire setup was grouted on to a foundation / stress relieved Mild Steel structure. The Gearbox output spline shaft is coupled to the Generator.
In generator mode of operation, the generator is driven by an AC motor connected to a 1:10 Step up gear box. The generator was flange mounted on to a Hollow shaft Torque sensor. The torque sensor was mounted on the step up gearbox. The AC Motor speed is varied through a closed loop Flux Vector drive.
The generator was loaded at various speeds in steps using the resistive load bank in steps and a momentary load for 0.3 seconds at the beginning of each step of loading. The following Figure 1, Figure 2 shows the generator mode test rig and generator mode schematic diagram of starter generator test system.
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