Angle Calculus-Based Thrust Force Determination on the Blades of a 10 kW Wind Turbine

Author:

Dorrego-Portela José Rafael1ORCID,Ponce-Martínez Adriana Eneida1ORCID,Pérez-Chaltell Eduardo1ORCID,Peña-Antonio Jaime1ORCID,Mateos-Mendoza Carlos Alberto2ORCID,Robles-Ocampo José Billerman3ORCID,Sevilla-Camacho Perla Yazmin3ORCID,Aviles Marcos4ORCID,Rodríguez-Reséndiz Juvenal4ORCID

Affiliation:

1. División de Estudios de Posgrado, Universidad del Istmo, Oaxaca 70760, Mexico

2. Instituto Tecnológico de Salina Cruz, Carretera a San Antonio Monterrey km 1.7, Salina Cruz 70701, Mexico

3. Cuerpo Académico de Energía y Sustentabilidad, Universidad Politécnica de Chiapas, Carretera Tuxtla Gutiérrez- Portillo Zaragoza Km 21+500, Col. Las Brisas, Suchiapa 29150, Mexico

4. Facultad de Ingeniería, Universidad Autónoma de Querétaro, Querétaro 76010, Mexico

Abstract

In this article, the behavior of the thrust force on the blades of a 10 kW wind turbine was obtained by considering the characteristic wind speed of the Isthmus of Tehuantepec. Analyzing mechanical forces is essential to efficiently and safely design the different elements that make up the wind turbine because the thrust forces are related to the location point and the blade rotation. For this reason, the thrust force generated in each of the three blades of a low-power wind turbine was analyzed. The angular position (θ) of each blade varied from 0° to 120°, the blades were segmented (r), and different wind speeds were tested, such as cutting, design, average, and maximum. The results demonstrate that the thrust force increases proportionally with increasing wind speed and height, but it behaves differently on each blade segment and each angular position. This method determines the angular position and the exact blade segment where the smallest and the most considerable thrust force occurred. Blade 1, positioned at an angular position of 90°, is the blade most affected by the thrust force on P15. When the blade rotates 180°, the thrust force decreases by 9.09 N; this represents a 66.74% decrease. In addition, this study allows the designers to know the blade deflection caused by the thrust force. This information can be used to avoid collision with the tower. The thrust forces caused blade deflections of 10% to 13% concerning the rotor radius used in this study. These results guarantee the operation of the tested generator under their working conditions.

Publisher

MDPI AG

Subject

Computer Science (miscellaneous)

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