An inset configured for use in a rotor blade is provided including a body having a shape generally complementary to a hole formed in the rotor blade. An opening extends between a first surface and a second surface of the body. The opening is configured to provide a fluid flow path between an interior and an exterior of the rotor blade.
AIRCRAFT ROTOR BLADE INSERT
2020-08-06
Patent
Electronic Resource
English
BLADE INSERT FOR A WIND TURBINE ROTOR BLADE AND RELATED METHODS
European Patent Office | 2021
|BLADE INSERT FOR A WIND TURBINE ROTOR BLADE AND RELATED METHODS
European Patent Office | 2020
|