The present invention relates to a conditioning system (100) for an aircraft. More particularly, the present invention relates to an auxiliary power system (20) with a new fuel feed architecture including a fuel tank (6). In addition, the present invention also refers to an aircraft comprising said conditioning system and a method for conditioning fuel of an auxiliary power system (20).
FUEL CONDITIONING SYSTEM FOR AN AIRCRAFT
KRAFTSTOFFKONDITIONIERUNGSSYSTEM FÜR EIN FLUGZEUG
SYSTÈME DE CONDITIONNEMENT DE CARBURANT POUR UN AÉRONEF
2024-08-21
Patent
Electronic Resource
English
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