An electrical power system for an aircraft including a turbine engine (101) coupled to the aircraft (5) and providing propulsive thrust and emitting heat during operation to define a high temperature source, a cryogenic fuel system (12) located within the aircraft and providing fuel for the turbine (101) 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
26.08.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
System and method for aviation electric power production
Europäisches Patentamt | 2018
|SYSTEM AND METHOD FOR AVIATION ELECTRIC POWER PRODUCTION
Europäisches Patentamt | 2015
|Electric energy conversion circuit of aviation electric propulsion power system
Europäisches Patentamt | 2021
|