A rotor blade for a rotary wing aircraft and a tip for the rotor blade. The rotor blade includes a blade root, a blade tip and a blade body that extends from the blade root to the blade tip. The blade tip includes: a continuously swept leading edge, a compound trailing edge, and a continuous anhedral.
Rotor blade tip design for improved hover and cruise performance
2021-01-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
ROTOR BLADE TIP DESIGN FOR IMPROVED HOVER AND CRUISE PERFORMANCE
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