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.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Download (147Kb) |
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 |
Actions (login required)
| View Item |
