Methods and systems for balancing helicopter rotor blades are disclosed. In some examples, density data of a rotor blade may be acquired by scanning the rotor blade. In some examples, surface contour data of a rotor blade may be acquired by scanning the rotor blade. In some examples, simulations may be performed to predict flight data associated with a modeled rotor blade. In some examples, a database may be referenced to predict a desired weight balance and/or a desired aerodynamic balance of a rotor blade.
Methods and systems for helicopter rotor blade balancing
2015-12-22
Patent
Electronic Resource
English
Methods and systems for helicopter rotor blade balancing
European Patent Office | 2019
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