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
2025-07-30
Patent
Electronic Resource
French