Development of a Piezoelectric Servo-Flap Actuator for Helicopter Rotor Control (original) (raw)

Piezoelectric Servo-Flap Actuator for Helicopter Rotor Control

Eric Prechtl

1994

View PDFchevron_right

Piezoelectric servo-flap actuation system for helicopter rotor individual blade control

Eric Prechtl

2000

View PDFchevron_right

Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps

DR.Dharmendra Kumar

View PDFchevron_right

A combined piezoelectric composite actuator and its application to wing/blade tips

Kevin Ha

2005

View PDFchevron_right

Bench-top characterization of an active rotor blade flap system incorporating C-block actuators

Andrew Moskalik

1998

View PDFchevron_right

Comparison of active and passive modes of piezoelectric patch actuators for scaled helicopter rotor blade vibration suppression

Demos T Tsahalis

View PDFchevron_right

Helicopter Rotor Blade Vibration Control on the Basis of Active/Passive Piezoelectric Damping Approach

Sergey Shevtsov

View PDFchevron_right

Pseudo-Active Control of Helicopter Blade Vibration Using Piezoelectric Actuators

Ioan G Ursu

45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, 2004

View PDFchevron_right

Fundamental Behavior of Piezoceramic Sheet Actuators

Inderjit Chopra

Journal of Intelligent Materials Systems and Structures, 2000

View PDFchevron_right

Refined Analysis of the Piezoelectric Pseudo-Active Control for Helicopter Blades Vibration

Ioan G Ursu

46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2005

View PDFchevron_right

Design and Fabrication of a Piezo Actuated Flapping Mechanism for a Micro Aerial Vehicle

Nandu Jith

View PDFchevron_right

Experimental and numerical study of a novel piezoelectric pilot stage for servovalves

Andrew R Plummer

2020

View PDFchevron_right

Research of the Piezo Actuator Location Influence on the Twist Angle of a Model Helicopter Blade Made of Polymer Composite Materials

Pavel Pisarev

IOP Conference Series: Materials Science and Engineering, 2019

View PDFchevron_right

Aeroelastic Modeling of Trailing-Edge-Flap Helicopter Rotors Including Actuator Dynamics

Inderjit Chopra

Journal of Aircraft, 2004

View PDFchevron_right

Detailed Design of an Active Rotor Blade for Reducing Helicopter Vibratory Loads

Wonjong Eun

2011

View PDFchevron_right

Active and passive vibration control of aircraft composite structures using power piezoelectric patch-like actuators

Sergey Shevtsov

Piezoceramic Materials and Devices, NOVA Science publ., 2009

View PDFchevron_right

A Novel Servovalve Pilot Stage Actuated by a Piezo-electric Ring Bender: A Numerical and Experimental Analysis

Pietro Palma

Energies

View PDFchevron_right

A Novel Servovalve Pilot Stage Actuated by a Piezo-Electric Ring Bender (Part II): Design Model and Full Simulation

Andrew R Plummer

Energies

View PDFchevron_right

Final work : Application of Piezoelectric actuators for controlled blade vibrations

DANIEL MANSO FABA

2019

View PDFchevron_right

Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices

Giovanni Bernardini

International Journal of Aerospace Engineering, 2015

View PDFchevron_right

Piezoelectric actuators 2006

Kenji Uchino

Journal of Electroceramics, 2008

View PDFchevron_right

Post-buckled precompressed (PBP) piezoelectric actuators for UAV flight control

Michel Van Tooren

Smart Structures and Materials 2006: Smart Structures and Integrated Systems, 2006

View PDFchevron_right

i: ill 4 L s_ L' Control of Helicopter Rotorblade Aerodynamics

Baba Olokonla

View PDFchevron_right

GA based optimization of flextensional piezoelectric actuator for rotorcraft active vibration control

Igor Zhilyaev, Sergey Shevtsov

View PDFchevron_right

Development of the Smart Spring for Active Vibration Control of Helicopter Blades

Viresh Wickramasinghe

Journal of Intelligent Material Systems and Structures, 2004

View PDFchevron_right

Actuator design for the active trailing edge of a helicopter rotor blade

Peter Jänker

… Forum, Kazan, Russia, 2007

View PDFchevron_right

DEFORMATION AND FORCE CHARACTERISTICS OF LAMINATED PIEZOELECTRIC ACTUATORS

Sontipee Aimmanee

2004

View PDFchevron_right

Structural response investigation of a triangular-based piezoelectric drive mechanism to hysteresis effect of the piezoelectric actuator

Tegoeh Tjahjowidodo

Mechanical Systems and Signal Processing, 2013

View PDFchevron_right

Design, Analysis, and Experiment on a Novel Stick-Slip Piezoelectric Actuator with a Lever Mechanism

mengxin sun

Micromachines, 2019

View PDFchevron_right

Wind Tunnel Testing of a Helicopter Rotor Trailing Edge Flap Actuated via Pneumatic Artificial Muscles

Benjamin Woods, Norman Wereley

Journal of Intelligent Material Systems and Structures, 2011

View PDFchevron_right

Development of a novel plane piezoelectric actuator using Hamilton's principle based model and Hertz contact theory

Abdul-Ganiyu Adisa Jimoh

Sensors and Actuators A: Physical, 2014

View PDFchevron_right

Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades

Carlos Cesnik

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003

View PDFchevron_right

New Actuators for Aircraft and Space Applications

Frank Claeyssen

2008

View PDFchevron_right

PNEUMATIC ARTIFICIAL MUSCLE DRIVEN TRAILING EDGE FLAPS FOR ACTIVE ROTORS

Benjamin Woods

View PDFchevron_right

Control of helicopter rotorblade aerodynamics

James Fabunmi

1991

View PDFchevron_right