IMPROVED BLADE FLAPPING MEASUREMENT PROCESS
A rotorcraft (10) comprising a rotor blade (26a) designed to flap about a hinge point, a measurement system (200) designed to measure blade flapping, and a processing system (300) designed to alter blade flapping measurements. The processing system further comprises a correction process to alter a b...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | A rotorcraft (10) comprising a rotor blade (26a) designed to flap about a hinge point, a measurement system (200) designed to measure blade flapping, and a processing system (300) 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. |
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