FLAP ANGLE MEASUREMENT SYSTEM FOR AN ACTIVE ROTOR CONTROL SYSTEM

A flap angle measurement system is disclosed for a helicopter rotor blade. The blade includes a trailing edge and a flap (18) hinged to at least a portion of the trailing edge (14) about a pivot axis. The flap angle measurement system includes a Hall effect sensor (102) mounted to the trailing edge...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	KOHLHEPP, FRED, W
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HELICOPTERS PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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