Anti-ice system exhaust air disruptor

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Anti-ice system exhaust air disruptor

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MACKIN STEVE G / MILLER KIMBERLY A

An airflow disruptor for a gas turbine engine bleed air exhaust port employs a disruptor plate rotatably mounted upstream from an exhaust port of an exhaust duct. An actuator is coupled to the disruptor plate and adapted to rotate the disruptor plate into an external airflow responsive to temperature of exhaust flow in the exhaust port whereby the external airflow is turbulated upstream of the exhaust port.

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Document information

Title :

Anti-ice system exhaust air disruptor

Contributors:

MACKIN STEVE G (author) / MILLER KIMBERLY A (author)

Publication date :

2021-08-10

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES