AUTOMATIC DUAL ROTOR SPEED CONTROL FOR HELICOPTERS

A flight control system for a helicopter having a main rotor and a tail rotor is provided. The flight control system includes an automatic rotor speed control being configured to transition the main rotor and the tail rotor between a high speed and a low speed based upon a plurality of received info...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BARNES, GREG W, BUCKMAN, KENNETH J, HORBURY, EILEEN F, JACOBS, ERIC W
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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