A device for producing electrical power has a thermoelectric device coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air. A system control is coupled to the ram air and the bleed air to control a temperature of the bleed air and to control a temperature gradient of the thermoelectric device.
THERMOELECTRIC GENERATOR ON AN AIRCRAFT BLEED SYSTEM
THERMOELEKTRISCHER GENERATOR AUF DEM ZAPFLUFTSYSTEM EINES FLUGZEUGS
GÉNÉRATEUR THERMOÉLECTRIQUE SUR UN SYSTÈME DE PRÉLÈVEMENT D'AIR À BORD D'UN AVION
2016-08-24
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft bleed system and method of controlling an aircraft bleed system
European Patent Office | 2015
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