发明申请
US20130283804A1 TRANSITION DUCT WITH LATE INJECTION IN TURBINE SYSTEM 有权
在涡轮机系统中具有最初注入的过渡管

TRANSITION DUCT WITH LATE INJECTION IN TURBINE SYSTEM
摘要:
A system for supplying an injection fluid to a combustor is disclosed. The system includes a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The passage defines a combustion chamber. The system further includes a tube providing fluid communication for the injection fluid to flow through the transition duct and into the combustion chamber.
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