Systems and methods are disclosed herein for an aircraft seat with a decoupled linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature from the linear actuator in response to loss of power to the linear actuator.
Decoupled aircraft seat actuator
2016-03-22
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |