Invention Grant
US08127546B2 Turbine engine fuel injector with helmholtz resonators 有权
具有亥姆霍兹共振器的涡轮发动机燃油喷射器

Turbine engine fuel injector with helmholtz resonators
Abstract:
An end cap for a fuel injector of a turbine engine is disclosed. The end cap includes an annular first surface including a plurality of perforations. The annular first surface is exposed to a combustion chamber of the turbine engine. The end cap is coupled to an end face of the fuel injector to define an enclosed cavity. The enclosed cavity and the plurality of perforations form an array of Helmholtz resonators.
Public/Granted literature
Information query
Patent Agency Ranking
0/0