A turbo-generator system for generating propulsive electrical power for an aircraft includes an electric machine comprising: a rotor configured to be rotated by a gas-turbine of the turbo-generator system; a stator comprising: a first active section comprising first windings surrounding a first portion of the rotor, and a second active section comprising second windings surrounding a second portion of the rotor.
Fault tolerant turbo-generator system
17.09.2024
Patent
Elektronische Ressource
Englisch
Reliability Model Generator for fault-tolerant systems
AIAA | 1988
|Turbo-generator integrated gas energy recovery system
Tema Archiv | 2006
|