An electrical power system for an aircraft including a turbine engine coupled to the aircraft and providing propulsive thrust and emitting heat during operation to define a high temperature source, a cryogenic fuel system located within the aircraft and providing fuel for the turbine and emitting heat at a lower temperature than the heat from the turbine engine to define a low temperature source and an electrical power generator located on the aircraft and having a thermodynamic generator using the temperature difference to generate electrical power and a method for producing electric power.
SYSTEM AND METHOD FOR AVIATION ELECTRIC POWER PRODUCTION
SYSTEM UND VERFAHREN ZUR ERZEUGUNG ELEKTRISCHER ENERGIE AUS DER LUFT
SYSTÈME ET PROCÉDÉ POUR LA PRODUCTION D'ÉNERGIE ÉLECTRIQUE D'AVION
2015-11-04
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
System and method for aviation electric power production
European Patent Office | 2018
|System and method for aviation electric power production
European Patent Office | 2015
|Electric energy conversion circuit of aviation electric propulsion power system
European Patent Office | 2021
|