The disclosure is towards an inlet cowl for a turbine engine including a surface defining an inlet with a flow path and a method towards controlling the airflow in the flow path. The inlet cowl further includes an inlet lip and inner and outer barrels. The inlet lip confronts the inner barrel at a junction defining a gap.
INLET COWL FOR A TURBINE ENGINE
2018-04-12
Patent
Elektronische Ressource
Englisch