Invention Grant
US08806871B2 Fuel nozzle 有权
燃油喷嘴

Fuel nozzle
Abstract:
A fuel nozzle for a gas turbine engine is disclosed, the fuel nozzle comprising at least one unitary component made using a rapid manufacturing process. In one aspect, the rapid manufacturing process is a laser sintering process. Unitary components disclosed include a conduit, swirler, distributor, venturi and a centerbody.
Public/Granted literature
Information query
Patent Agency Ranking
0/0