A system for an aircraft includes a tiltable proprotor that is tiltable between a lift position for providing lift for the aircraft and a forward flight position for providing forward propulsion for the aircraft is provided. The system includes at least one actuator for adjusting a tilt angle of the tiltable proprotor; and at least one passive damper connected to the tiltable proprotor and configured to limit a rate of change of the tilt angle of the tiltable proprotor.
REDUNDANT LOAD PATH FOR POWERED LIFT TILT ACTUATOR
2024-04-11
Patent
Electronic Resource
English
Tilt-rotor unmanned aerial vehicle dual-safety redundant tilt actuator
European Patent Office | 2023
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