Invention Grant
US09228488B2 High pressure turbine inlet duct and engine 有权
高压涡轮机入口管道和发动机

High pressure turbine inlet duct and engine
Abstract:
A duct for connection between an exhaust manifold and a high-pressure turbine inlet include a cylindrical duct body defining a longitudinal axis. A frustoconical outlet nozzle connected at one end of the duct body and extending at about eighty-five degrees from the longitudinal axis. The duct further includes an inlet bell connected at the other end of the duct body and extending at about fifty degrees from the longitudinal axis.
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