Development of High Speed Alternator for Gas Turbine Engine

Ramachandran, A and Ramamurthy, S and Rajeshwari Natarajan, S and Rajendran , R (2003) Development of High Speed Alternator for Gas Turbine Engine. In: 6th National Conference on Air Breathing Engines and Aerospace Propulsion, January 10-11th, IISC,Bangalore.

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    Abstract

    A high-speed alternator is deigned and experimentally evaluated for its performance with load. For testing the alternator a partial admission turbine drive is optimally designed and fabricated. The turbine drive system is analyzed for stresses and critical speed. The alternator, which consists of permanent magnet surrounded by a stator, was designed to get the required power. The alternator was tested at various speeds with load. This paper describes the salient features of the alternator and its performance characteristics.

    Item Type: Conference or Workshop Item (Lecture)
    Subjects: AERONAUTICS > Aeronautics (General)
    AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Other, Propulsion Division, Propulsion Division, Propulsion Division
    Depositing User: Dr S Ramamurthy
    Date Deposited: 13 Aug 2010 10:20
    Last Modified: 13 Aug 2010 10:20
    URI: http://nal-ir.nal.res.in/id/eprint/8946

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