Invention Grant
US08453458B2 Gas turbine engine variable exhaust nozzle 有权
燃气轮机发动机可变排气喷嘴

Gas turbine engine variable exhaust nozzle
Abstract:
Variation in the available mixing plane areas in an exhaust arrangement of a gas turbine engine enables alteration and configuration for better thermal cycle performance of that engine. A shaped centre fairing is associated with an exit nozzle and a bypass duct such that channels between the fairing, nozzle exit and duct can be adjusted to change the available areas. Such variation is achieved by relative axial displacement, typically of the exit nozzle using an appropriate mechanism.
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