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Volumn 1 PART A, Issue , 2008, Pages 261-268
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Spin testing of pneumatic artificial muscle systems for helicopter rotor applications
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Author keywords
[No Author keywords available]
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Indexed keywords
(+ MOD 2N) OPERATION;
ACTUATION SYSTEMS;
BI DIRECTIONAL;
BLOCKED FORCE;
FLAP SYSTEMS;
HARSH ENVIRONMENTS;
HINGE MOMENT;
INTERNATIONAL DESIGNS;
MECHANICAL VIBRATIONS;
PNEUMATIC ACTUATORS;
PNEUMATIC ARTIFICIAL MUSCLES;
PNEUMATIC ARTIFICIAL MUSCLES (PAMS);
ROTOR BLADES;
SPIN TESTING;
SYSTEM PERFORMANCES;
TECHNICAL CONFERENCES;
TORSIONAL SPRINGS;
TRACK CHANGES;
VIBRATION REDUCTIONS;
ACCELERATION;
ACTUATORS;
AERODYNAMICS;
ARCHITECTURAL ACOUSTICS;
ARCHITECTURAL DESIGN;
ASSOCIATIVE STORAGE;
BISMUTH;
COMPUTER NETWORKS;
COMPUTERS;
CONTROL SYSTEMS;
ENGINEERING;
EQUIPMENT TESTING;
FLUID MECHANICS;
GAS DYNAMICS;
HELICOPTERS;
LATTICE VIBRATIONS;
LOADING;
LOADS (FORCES);
MILITARY HELICOPTERS;
MULTITASKING;
MUSCLE;
PHOTOACOUSTIC EFFECT;
PNEUMATIC DRIVES;
PNEUMATICS;
PULSE AMPLITUDE MODULATION;
ROTORS (WINDINGS);
SOFTWARE TESTING;
TECHNOLOGY;
TESTING;
TISSUE;
TURBOMACHINE BLADES;
VIBRATION CONTROL;
VIBRATIONS (MECHANICAL);
VIBRATORS;
HELICOPTER ROTORS;
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EID: 44849087723
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1115/DETC2007-35653 Document Type: Conference Paper |
Times cited : (2)
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References (8)
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