ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM

摘要

An electronically-synchronized flap system for a fixed-wing aircraft including a first wing including a first flap panel, the first flap panel being connected with a first in-board actuator and a first out-board actuator, and a second wing including a second flap panel, the second flap panel being connected with a second in-board actuator and a second out-board actuator. In an embodiment, the system can further include an electronic control unit (ECU) configured to control the first and second in-board and out-board actuators to electronically synchronize the positions of the first and second flap panels.