| Grant number: | 13/15264-3 |
| Support Opportunities: | Scholarships in Brazil - Doctorate |
| Start date: | September 01, 2013 |
| End date: | September 27, 2018 |
| Field of knowledge: | Engineering - Aerospace Engineering - Aerospace Structures |
| Principal Investigator: | Carlos de Marqui Junior |
| Grantee: | Marcel Araujo Clementino |
| Host Institution: | Escola de Engenharia de São Carlos (EESC). Universidade de São Paulo (USP). São Carlos , SP, Brazil |
| Associated scholarship(s): | 15/04804-2 - Design and experimental verification of a semi-active pitch link for helicopter vibration attenuation, BE.EP.DR |
Abstract Piezoelectric materials have been used for vibration control in different engineering problems. In general, the piezoelectric vibration controllers are classified as active or passive systems. In the first case, the reverse piezoelectric effect is used and an external power source is required. In the second case, mechanical energy is converted to electrical energy based on the direct piezoelectric effect. The piezoelectric material is connected to simple electrical circuits (that uses passive elements) in order to dissipate energy. More recently, switching circuits have been used for the nonlinear treatment of the electrical output of piezoelectric materials resulting in semi-passive and semi-active controllers. Different switching circuits have been presented in the literature of piezoelectric vibration control. In some cases, the behavior of the switching controller is similar to mechanical systems used in helicopters for vibration control. One of these mechanical systems is the active pitch link presented by a Canadian research group. This system uses the combination of springs in order to control the stiffness of the pitch link. Although a remarkable control performance has been achieved with the active pitch link, some drawbacks (i.e. external voltage is required and mechanical failures) are point out by the authors. The main goal of the present project is the design and experimental verification of a self-powered piezoelectric semi-active pitch link using autonomous switching circuits. This solid-state configuration would address the issues presented by the mechanical active pitch link as well as present a good performance in vibration attenuation. | |
| News published in Agência FAPESP Newsletter about the scholarship: | |
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Filed patent(s) as a result of this research project
SISTEMA DE HASTE DE COMANDO DE PASSO DE HELICÓPTERO BR 10 2018 000434 4 - Universidade de São Paulo (USP). . Carlos De Marqui Junior; Marcel Araújo Clementino; Tarcísio Marinelli Pereira Silva; Fred Nitzsche - January 2018, 01