An airflow disruptor (34, 134, 234) for a gas turbine engine bleed air exhaust port (28) employs a disruptor plate (36) rotatably mounted upstream from an exhaust port (28) of an exhaust duct (26). An actuator is coupled to the disruptor plate (36) and adapted to rotate the disruptor plate (36) into an external airflow (29) responsive to temperature of exhaust flow (31) in the exhaust port (28) whereby the external airflow (29) is turbulated upstream of the exhaust port (28).
ANTI-ICE SYSTEM EXHAUST AIR DISRUPTOR
ANTI-EIS-SYSTEM-ABLUFTDISRUPTOR
DÉSINTÉGRATEUR D'AIR D'ÉCHAPPEMENT DE SYSTÈME ANTIGIVRE
2023-07-05
Patent
Elektronische Ressource
Englisch
Online Contents | 2017
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