| 摘要 |
An exhaust assembly (52) for a gas turbine engine (40) which includes a turbine rear frame (75). The exhaust assembly comprises an engine exhaust nozzle (76) extending downstream from the turbine rear frame and an infrared suppression system (72) coupled in flow communication with said engine exhaust nozzle for channeling exhaust gases discharged from said exhaust nozzle. The suppression system comprises a flow channel (90) coupled to an access door (12), movable with the access door from a closed position to an open position wherein the access door forms a work platform. The suppression system facilitates suppressing an exhaust infrared signature of the gas turbine engine.
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