This report briefly presents the design and development aspects of the test rig to evaluateudthe performance of high speed alternators with power rating of 5 kW at rated speed of 55000 rpm.udMajor part of the report covers detailed mechanical design of the drive turbine and the other rigudsystems. The test rig is designed and developed at Propulsion Division, NAL-CSIR to map the electricaludcharacteristics of the AC alternator to be used in a Small Turbo Fan Engine (STFE) which is beinguddeveloped by Gas Turbine Research Establishment. An air turbine drive was designed to develop 20 kWudpower at 53000 rpm to drive the alternator. A parabolic solid disc configuration is arrived at to keep theudstress minimum. Cyclic symmetry stress analysis is carried out on the sector model (1/27th) carved outudfrom the blisk. The air turbine shaft is designed to be inserted in to the bore of the alternator hallowudshaft and is to be fastened at the other end with a lock nut. The rotor-dynamic analysis is carried out forudthe rotor in overhang configuration with bearing support stiffness ranging from 17.5 to 175 MN/m andudcritical speeds of the rotor-bearing system is predicted. A lubrication system with an in-built reservoirudtank is designed to provide cooling to the stator core and to lubricate the alternator bearings. Special fixtures are designed to insert and extract the air-turbine shaft into and from the alternator rotor respectively to ensure that the alternator bearings are not unduly loaded during assembly and dis-assembly procedures. The rig is instrumented with pressure, temperature and flow transducers for compressed air and the lubrication oil in addition to speed and vibration pick-ups. As the rotationaludspeed of the rig is extremely high, several safety measures are considered and implemented.
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