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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: NELSON, Hunter Barton, TRANTHAM, Michael David, COVINGTON, Charles Eric, JOHNSON, Randall Lee
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
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.