发明申请
US20100247304A1 EXHAUST PLENUM FOR A TURBINE ENGINE 有权
用于涡轮发动机的排气孔

EXHAUST PLENUM FOR A TURBINE ENGINE
摘要:
An exhaust system for gas turbine engine is provided that reduces turbulence and backflow within the exhaust system and, thus, increases the efficiency of the turbine engine. In various embodiments, the system includes an exhaust plenum that provides a gradual expansion of the exhaust gases. The exhaust plenum may also include one or more flow splitters that further reduce turbulence in the plenum and provide a more uniform gas flow in the plenum and other downstream exhaust components.
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