A propulsion assembly for an aircraft, which has a propulsion system with a combustion chamber surrounded by a casing, a supply pipe that conveys dihydrogen to the combustion chamber through the casing via injectors, and a housing fastened to the casing in a sealed manner around the latter, wherein the supply pipe has a downstream part housed inside the housing and wherein the injectors are also housed inside the housing.
ENSEMBLE PROPULSIF POUR AÉRONEF
PROPULSION ASSEMBLY FOR AIRCRAFT
ANTRIEBSEINHEIT FÜR EIN FLUGZEUG
30.07.2025
Patent
Elektronische Ressource
Französisch