An aircraft actuator assembly includes a failsafe holding device, comprising a body that extends between a lug 503 configured to hingedly connect the holding device to a actuator support body 423 and an attachment flange 501 configured to fixedly attach the holding device to a landing provided by a main body 507 of an actuator, wherein the holding device is configured to prevent movement of the actuator 507 from a normal working position relative to the actuator support body 423 in the event of structural failure of a connection body 407 of the actuator.
Holding device for an aircraft actuator
2019-01-09
Patent
Elektronische Ressource
Englisch