Reduction of the vibration in a helicopter blade using piezoelectric actuators
A method to reduce vibration in a helicopter blade under a variable harmonic pressure loading using piezoelectric actuators is presented. The model of a helicopter blade is an equivalent aluminum plate. To decrease the amplitude in the resonant frequency range, piezoelectric actuators are set on the...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2006-06-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7385 |
| _version_ | 1818383988724596736 |
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| author | Sergejs Gluhihs Andrejs Kovalovs |
| author_facet | Sergejs Gluhihs Andrejs Kovalovs |
| author_sort | Sergejs Gluhihs |
| collection | DOAJ |
| description | A method to reduce vibration in a helicopter blade under a variable harmonic pressure loading using piezoelectric actuators is presented. The model of a helicopter blade is an equivalent aluminum plate. To decrease the amplitude in the resonant frequency range, piezoelectric actuators are set on the top of the plate. The results were obtained by using the ANSYS finite element code. The temperature analogy method instead of a variable pressure load is assumed for numerical analysis. The influence of piezoelectric actuators on the plate is considered. It is shown that the use of piezoelectric actuators to decrease the vibration of the plate is highly efficient. The most rational arrangements of piezoelectric actuators and the required amount of electric voltage are determined.
First Published Online: 14 Oct 2010 |
| first_indexed | 2024-12-14T03:15:07Z |
| format | Article |
| id | doaj.art-53566bbcc62d4931a9a80b607ca5b84d |
| institution | Directory Open Access Journal |
| issn | 1648-7788 1822-4180 |
| language | English |
| last_indexed | 2024-12-14T03:15:07Z |
| publishDate | 2006-06-01 |
| publisher | Vilnius Gediminas Technical University |
| record_format | Article |
| series | Aviation |
| spelling | doaj.art-53566bbcc62d4931a9a80b607ca5b84d2022-12-21T23:19:10ZengVilnius Gediminas Technical UniversityAviation1648-77881822-41802006-06-0110210.3846/16487788.2006.9635927Reduction of the vibration in a helicopter blade using piezoelectric actuatorsSergejs Gluhihs0Andrejs Kovalovs1Institute of Materials and Structures of Riga Technical University. Azenes St. 16-323, LV-1048, Riga, LatviaInstitute of Materials and Structures of Riga Technical University. Azenes St. 16-323, LV-1048, Riga, LatviaA method to reduce vibration in a helicopter blade under a variable harmonic pressure loading using piezoelectric actuators is presented. The model of a helicopter blade is an equivalent aluminum plate. To decrease the amplitude in the resonant frequency range, piezoelectric actuators are set on the top of the plate. The results were obtained by using the ANSYS finite element code. The temperature analogy method instead of a variable pressure load is assumed for numerical analysis. The influence of piezoelectric actuators on the plate is considered. It is shown that the use of piezoelectric actuators to decrease the vibration of the plate is highly efficient. The most rational arrangements of piezoelectric actuators and the required amount of electric voltage are determined. First Published Online: 14 Oct 2010https://journals.vgtu.lt/index.php/Aviation/article/view/7385ANSYSpiezoelectricplatevibrationthermal analogy |
| spellingShingle | Sergejs Gluhihs Andrejs Kovalovs Reduction of the vibration in a helicopter blade using piezoelectric actuators Aviation ANSYS piezoelectric plate vibration thermal analogy |
| title | Reduction of the vibration in a helicopter blade using piezoelectric actuators |
| title_full | Reduction of the vibration in a helicopter blade using piezoelectric actuators |
| title_fullStr | Reduction of the vibration in a helicopter blade using piezoelectric actuators |
| title_full_unstemmed | Reduction of the vibration in a helicopter blade using piezoelectric actuators |
| title_short | Reduction of the vibration in a helicopter blade using piezoelectric actuators |
| title_sort | reduction of the vibration in a helicopter blade using piezoelectric actuators |
| topic | ANSYS piezoelectric plate vibration thermal analogy |
| url | https://journals.vgtu.lt/index.php/Aviation/article/view/7385 |
| work_keys_str_mv | AT sergejsgluhihs reductionofthevibrationinahelicopterbladeusingpiezoelectricactuators AT andrejskovalovs reductionofthevibrationinahelicopterbladeusingpiezoelectricactuators |