发明授权
US07603863B2 Secondary fuel injection from stage one nozzle 有权
二级燃油喷射从一级喷嘴

Secondary fuel injection from stage one nozzle
摘要:
A secondary combustion system for a stage one turbine nozzle. The secondary combustion system may include a supply tube extending into the stage one nozzle, a number of injectors extending from the supply tube to an outer surface of the stage one nozzle, and an air gap surrounding each of the number of injectors.
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