Beta
25401

OPTIMAL DESIGN OF PIEZO-ACTUATORS IN A LAYERED COMPOSITE STRUCTURE

Article

Last updated: 24 Dec 2024

Subjects

-

Tags

-

Abstract

Optimization of the location and thickness of twin collinear piezoelectric actuators embedded in a layered composite structure is analytically studied. An expression for the effective moment induced by the actuators is derived using a static analysis assuming perfect bonding between layers (i. e, zero bonding thickness). The optimal actuator position and thickness which maximizes piezo-actuator/ substructure coupling is investigated for an aluminium substructure with lead zirconate titanate (PZT) actuators. Results of this study show that the optimal location for thin actuators is on the surface of the composite. However, for thicker actuator the optimum location is shown to be within the composite structure. An
analysis actuator thickness shows that the optimal actuator thickness depends on the actuator position. An explanation of this behavior is presented.

DOI

10.21608/asat.1997.25401

Authors

First Name

M.

Last Name

El-NOMROSSY

MiddleName

M.

Affiliation

Department of Aeronautics, MTC., Cairo, Egypt.

Email

-

City

-

Orcid

-

First Name

A.

Last Name

ISTAFANOS

MiddleName

A.

Affiliation

Department of Aeronautics, MTC., Cairo, Egypt.

Email

-

City

-

Orcid

-

Volume

7

Article Issue

ASAT Conf. 13-15 May 1997

Related Issue

4645

Issue Date

1997-05-01

Receive Date

2019-01-20

Publish Date

1997-05-01

Page Start

203

Page End

215

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25401.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25401

Order

15

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

OPTIMAL DESIGN OF PIEZO-ACTUATORS IN A LAYERED COMPOSITE STRUCTURE

Details

Type

Article

Created At

22 Jan 2023