A rotorcraft comprising a rotor blade designed to flap about a hinge point, a measurement system designed to measure blade flapping, and a processing system designed to alter blade flapping measurements. The processing system further comprises a correction process to alter a blade flapping measurement dependent on rotor RPM or rotor torque.
BLADE FLAP MEASUREMENT PROCESS
2021-12-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |