Design issues of a high-stroke, on-blade piezostack actuator for a helicopter rotor with trailing-edge flaps

Journal of Intelligent Material Systems and Structures

Volumn 11, Issue 5, 2000, Pages 328-342

  Lee, T ^a   Chopra, I ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE ELEMENT METHOD; FORCE CONTROL; HELICOPTER ROTORS; MACHINE VIBRATIONS; MATHEMATICAL MODELS; PIEZOELECTRIC MATERIALS; STIFFNESS; STRAIN;

ON-BLADE PIEZOSTACK ACTUATORS; TRAILING-EDGE FLAPS;

ACTUATORS;

EID: 0034179798     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1106/M2JN-6W7Y-WNVD-E6HW     Document Type: Article

References (17)

1. Actuation of trailing edge flap in a wing model using piezostack device
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7. Electro-mechanical characterization of piezoelectric stack actuators
8. Design of high force, high displacementa actuators for helicopter rotors
9. Design and testing of a helicopter trailing edge flap with piezoelectric stack actuators
10. Aeromechanic considerations in the design of a rotor with smart material actuated trailing edge flaps
11. Development of a piezoelectric actuator for trailing edge flap control of rotor Blades