Placement and sizing of piezo actuators is normally based on control effectiveness. However, retrofitting of piezoelectric actuators alters the inherent stiffness/mass properties of the parent structure. In rotating structures, the additional mass due to piezo patches contributes to the centrifugal stiffening force. The parent structure is originally designed to have a certain natural frequency spectrum in relation to the disturbance excitation. In the event of failure of the active system, the dynamics of the structure with piezos (now rendered passive) will therefore become significant. Thus it will be helpful to determine locations for mounting piezo patches based on minimal natural frequency change yet with good control authority. In th...
An equation is derived to model the piezoelectric actuators incorporation with flexible structures. ...
"Damping of vibrations is often required to improve both the performances and the integrity of engin...
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...
This paper presents numerical analyses and a physical experiment on efficiency of different shapes a...
Sizing and placement of piezoelectric sensors and actuators (S/As) for active vibration control of f...
Active vibration control has been used to suppress and bring the structure back to its equilibrium s...
This technical note presents the optimal position and orientation of a piezoelectric patch actuator ...
The effectiveness of the overall smart structure depends to a great extent on the number and distrib...
The work has been supported by the Czech Science Foundation Project Mechatronic structures with heav...
The purpose of present investigations is development of optimisation methodology for an active vibra...
Piezoceramic Patches are commonly used as actuator devices in smart structures if the induced force...
The piezoelectric stack is employed as an actuator and a sensor in a variety of technical applicatio...
Piezoelectric actuators provide high frequency, force, and stiffness capabilities along with reasona...
An equation is derived to model the piezoelectric actuators incorporation with flexible structures. ...
ABSTRACT: Future technologies in microsensing, microactuation, active changes in shapes of aerofoils...
An equation is derived to model the piezoelectric actuators incorporation with flexible structures. ...
"Damping of vibrations is often required to improve both the performances and the integrity of engin...
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...
This paper presents numerical analyses and a physical experiment on efficiency of different shapes a...
Sizing and placement of piezoelectric sensors and actuators (S/As) for active vibration control of f...
Active vibration control has been used to suppress and bring the structure back to its equilibrium s...
This technical note presents the optimal position and orientation of a piezoelectric patch actuator ...
The effectiveness of the overall smart structure depends to a great extent on the number and distrib...
The work has been supported by the Czech Science Foundation Project Mechatronic structures with heav...
The purpose of present investigations is development of optimisation methodology for an active vibra...
Piezoceramic Patches are commonly used as actuator devices in smart structures if the induced force...
The piezoelectric stack is employed as an actuator and a sensor in a variety of technical applicatio...
Piezoelectric actuators provide high frequency, force, and stiffness capabilities along with reasona...
An equation is derived to model the piezoelectric actuators incorporation with flexible structures. ...
ABSTRACT: Future technologies in microsensing, microactuation, active changes in shapes of aerofoils...
An equation is derived to model the piezoelectric actuators incorporation with flexible structures. ...
"Damping of vibrations is often required to improve both the performances and the integrity of engin...
Interest in the use of smart-structure technology for noise and vibration reduction in helicopter ap...