| 摘要 |
An exhaust system for gas turbine engine (12) is provided that reduces turbulence and backflow within the exhaust system and, thus, increases the efficiency of the turbine engine (12). In various embodiments, the system includes an exhaust plenum (32) that provides a gradual expansion of the exhaust gases. The exhaust plenum (32) may also include one or more flow splitters (84, 130) that further reduce turbulence in the plenum or symmetrical arrangements and provide a more uniform gas flow in the plenum and other downstream exhaust components. |
