Design and manufacturing of a model-scale active twist rotor prototype blade

Journal of Intelligent Material Systems and Structures

Volumn 19, Issue 12, 2008, Pages 1443-1456

  Shin, Sang Joon ^a   Cesnik, Carlos E S ^b   Wilkie, W Keats ^c   Wilbur, Matthew L ^d  

^a Seoul National University   (South Korea)

^b UNIVERSITY OF MICHIGAN   (United States)

^c CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Active twist rotor; Blade integral actuation; Helicopter vibration control; Piezoelectric composite actuator

Indexed keywords

ACTUATORS; DESIGN; HELICOPTERS; LATTICE VIBRATIONS; MANUFACTURE; PIEZOELECTRIC ACTUATORS; PIEZOELECTRICITY; TURBOMACHINE BLADES;

ACTIVE TWIST ROTOR; ACTIVE TWIST ROTORS; ACTUATION TESTS; BLADE INTEGRAL ACTUATION; DESIGN GOALS; DESIGN REQUIREMENTS; HELICOPTER VIBRATION CONTROL; MANUFACTURING PROCESSES; PIEZOELECTRIC COMPOSITE ACTUATOR; PIEZOELECTRIC FIBER COMPOSITES; ROTOR BLADES; STRAIN ACTUATIONS; STRUCTURAL CHARACTERISTICS; VIBRATION REDUCTIONS;

HELICOPTER ROTORS;

EID: 57049172000     PISSN: 1045389X     EISSN: 15308138     Source Type: Journal    
DOI: 10.1177/1045389X07088051     Document Type: Article

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