Methods and apparatus to vary an air intake of aircraft engines are disclosed. An example nacelle assembly includes a fan cowl and an inlet cowl movably coupled to the fan cowl. The inlet cowl defines a primary flow path and an auxiliary flow path of an intake of the aircraft engine. The inlet cowl moves relative to the fan cowl between an open position to allow airflow via an auxiliary flow path and a closed position to prevent airflow through the auxiliary flow path.
METHODS AND APPARATUS TO VARY AN AIR INTAKE OF AIRCRAFT ENGINES
2017-06-08
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Methods and apparatus to vary an air intake of aircraft engines
European Patent Office | 2019
|INTAKE SYSTEMS for AIRCRAFT ENGINES
SAE Technical Papers | 1943
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