A system for distributing air to a plurality of aircraft zones includes an air mixer (22) including an air inlet plenum (26) and a manifold (24). The manifold including a plurality of sections (30) fluidly coupled to the plurality of aircraft zones. At least one thermoelectric device (40) is associated with said plurality of sections of said manifold. The at least one thermoelectric device is operable to condition air within said plurality of sections to a desired temperature corresponding to the plurality of aircraft zones.
AIR DISTRIBUTION MANIFOLD WITH INTEGRAL MULTIZONE THERMOELECTRIC TEC TRIM SYSTEM
LUFTVERTEILUNGSBLOCK MIT INTEGRIERTEM MEHRZONIGEM THERMOELEKTRISCHEM TEC TRIMMSYSTEM
COLLECTEUR DE DISTRIBUTION D'AIR INTÉGRANT UN SYSTÈME THERMOÉLECTRIQUE TEC MULTIZONE
2019-07-24
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIR DISTRIBUTION MANIFOLD WITH INTEGRAL MULTIZONE TEC TRIM SYSTEM
European Patent Office | 2018
|Programmable Multizone Furnace
NTRS | 1990
|