A system and method for improving the flight control and efficiency of an aerial vehicle. Many embodiments are directed to a rotor-shroud assembly system where a plurality of rotor blades are connected to the internal side of a shroud and are set up to pivot through the use of a pitching mechanism. The entire assembly is configured to rotate when attached to a motor.
Rotating Shroud for Rotator Blade Systems
2023-07-06
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Turbine Blade Platform, Blade Tip and Shroud Heat Transfer
British Library Conference Proceedings | 1995
|Turbine blade platform, blade tip and shroud heat transfer
Tema Archiv | 1995
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