A strake for a turbine engine nacelle may comprise a forward portion (261) coupled to a turbine engine nacelle inlet, and an aft portion (262) coupled to a turbine engine nacelle fan cowl, wherein the aft portion is configured to move between a first position and a second position, and the aft portion engages the forward portion in response to the aft portion moving to the second position to secure the fan cowl with respect to the inlet.
AERODYNAMIC NACELLE STRAKES AS AXIAL LOCATOR
AERODYNAMISCHE GONDELSTREBEN ALS AXIALPOSITIONIERER
VIRURES DE NACELLE AÉRODYNAMIQUE EN TANT QUE LOCALISATEUR AXIAL
2023-02-08
Patent
Electronic Resource
English
Aerodynamic control using forebody strakes
NTRS | 1991
|Aerodynamic control using forebody strakes
AIAA | 1991
|