A deployment mechanism for use on an aerial vehicle adapted for vertical takeoff and landing using deployable thrust producing elements for takeoff and landing. The deployment mechanism may use linear actuation of a linkage assembly to deploy thrust producing rotor assemblies from a vertical thrust hove configuration to a horizontal thrust forward flight configuration. The aerial vehicle may include left side rotor assemblies and right side rotor assemblies which may be deployed by deployment mechanisms.
Rotor Deployment Mechanism For Vertical Take-Off And Landing Aircraft
2025-01-30
Patent
Electronic Resource
English
Rotor deployment mechanism for vertical take-off and landing aircraft
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