Invention Grant
US09228499B2 System for secondary fuel injection in a gas turbine engine 有权
燃气涡轮发动机二次燃料喷射系统

System for secondary fuel injection in a gas turbine engine
Abstract:
Embodiments of the present disclosure provide a turbine combustor having a primary fuel injection system, a first wall portion disposed about a primary combustion zone downstream from the primary fuel injection system, and a second wall portion disposed downstream from the first wall portion. The turbine combustor also has a secondary fuel injection system disposed between the first wall portion and the second wall portion, where the secondary fuel injection system is removable form the first and second wall portions.
Public/Granted literature
Information query
Patent Agency Ranking
0/0