CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT

CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT

Control systems (20) for a rotorcraft (1) are provided, the rotorcraft (1) including main rotor (5) and auxiliary propulsor assemblies (6). the main rotor assembly (1) including first (50) and second (51) rotors disposed to oppositely rotate relative to an airframe (2) about a same rotational axis (...

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Hauptverfasser: GEIGER, Derek, WULFF, Ole
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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creator GEIGER, Derek
WULFF, Ole
description Control systems (20) for a rotorcraft (1) are provided, the rotorcraft (1) including main rotor (5) and auxiliary propulsor assemblies (6). the main rotor assembly (1) including first (50) and second (51) rotors disposed to oppositely rotate relative to an airframe (2) about a same rotational axis (RA), and sensors (30) disposed to generate hub moment, tip clearance and lift offset data of the main rotor assembly (5).
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language eng ; fre ; ger
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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT
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