A turbofan engine includes a fan variable area nozzle includes having a first fan nacelle section and a second fan nacelle section movably mounted relative the first fan nacelle section. The second fan nacelle section axially slides aftward relative to the fixed first fan nacelle section to change the effective area of the fan nozzle exit area.
GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE
2017-03-16
Patent
Electronic Resource
English
GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE
European Patent Office | 2021
|GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE
European Patent Office | 2018
|GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE
European Patent Office | 2018
|Gas turbine engine with axial movable fan variable area nozzle
European Patent Office | 2022
|Gas turbine engine with axial movable fan variable area nozzle
European Patent Office | 2021
|