Design and experimental testing of an induced-shear piezoelectric actuator for rotor blade trailing edge flaps

Keyphrases

• Piezoelectric Actuator 100%
• Experimental Testing 100%
• Trailing Edge Flap 100%
• Design Testing 100%
• Tube Actuator 100%
• Rotor Blades Trailing Edge 100%
• Flap 50%
• Hinge Moment 50%
• New Actuator 33%
• Actuator 33%
• Flap Deflection 33%
• Rotational Speed 16%
• Electric Field (E-field) 16%
• Actuator Design 16%
• Finite Element Model 16%
• Applied Electric Field 16%
• Helicopter 16%
• Piezoelectric Tube 16%
• Percent Error 16%
• Blade Design 16%
• Amplification Mechanism 16%
• Rotor Speed 16%
• Analytical Modeling 16%
• Driven Element 16%
• Bender 16%
• Flap Control System 16%
• Mechanical Springs 16%

Engineering

• Trailing Edge 100%
• Flaps 100%
• Rotor Blade 100%
• Full Scale 30%
• Piezoelectric 10%
• Finite Element Modeling 10%
• Rotor Speed 10%
• Applied Electric Field 10%
• Percent Error 10%
• Blades Design 10%
• Rotation Speed 10%