A heat exchange system for an aircraft includes an aircraft controller (106) for controlling an operation of an aircraft, a thermoelectric device (104) having a low temperature side (120) and a high temperature side (122). Heat is transferred away from the inlet line to the outlet line through the thermoelectric device when a predetermined condition is met.
AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE
FLUGZEUGWÄRMETAUSCHERSYSTEM EINSCHLIESSLICH EINER THERMOELEKTRISCHEN VORRICHTUNG
SYSTÈME D'ÉCHANGE DE CHALEUR D'AÉRONEF COMPRENANT UN DISPOSITIF THERMOÉLECTRIQUE
2019-05-15
Patent
Electronic Resource
English
AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE
European Patent Office | 2018
|Aircraft heat exchange system including a thermoelectric device
European Patent Office | 2019
|Aircraft heat exchange system including a thermoelectric device
European Patent Office | 2018
|AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE
European Patent Office | 2017
|AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE
European Patent Office | 2017
|