Invention Grant
US08820086B2 Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal 有权
具有集成流量限制器和歧管密封件的燃气轮机燃烧器整流器组件

Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal
Abstract:
An endcover assembly for a turbine combustor adapted to support one or more combustor nozzles includes a substantially flat plate having one side which in use, faces a combustion chamber and an opposite side which, in use, faces away from the combustion chamber. At least one fuel passage extends through the substantially flat plate. A fuel manifold porting block is secured to the opposite side of the flat plate with at least one port aligned with the at least one passage. A fuel restrictor insert formed with multiple flow orifices is located between the flat plate and the fuel manifold porting block in alignment with the at least one fuel passage and the at least one port.
Information query
Patent Agency Ranking
0/0