An integrated LP shaft generator for the More Electric aircraft
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- Author(s): A.J. Mitcham; N. Grum Source: IEE Colloquium on All Electric Aircraft, January 1998 page 8
- Conference: IEE Colloquium on All Electric Aircraft
The engine power management and control architecture should enable power transfer to and from the airframe, and within the engine system, from the LP to the HP system. The paper considers some of the design aspects of the LP shaft generator and the selection of preferred generator technology (permanent magnet generator, switched reluctance generator, induction generator). (9 pages)
Inspec keywords: aerospace engines; permanent magnet generators; power supplies to apparatus; reluctance generators; electric vehicles; electric drives; asynchronous generators; power control; electric propulsion; aerospace propulsion
Subjects: Aerospace control; Asynchronous machines; Electric actuators and final control equipment; Small and special purpose electric machines; Synchronous machines; Power convertors and power supplies to apparatus; Power and energy control; Aerospace propulsion; Drives; Aerospace and avionic power supplies
