نتایج جستجو برای: blade pitch angle control

تعداد نتایج: 1472145  

Journal: :AIAA Journal 2021

As wind turbine diameters continue to increase, the cyclic loading experienced by blade due shear and yaw misalignment increases dramatically hindering development of larger more efficient turbines. Based on current literature, controlling a section trailing edge was found reduce loading. To quantify load control capability flap (TEF), an experimental rig designed evaluate TEF 3.5-m-diam operat...

Journal: :IOP Conference Series: Materials Science and Engineering 2020

Journal: :J. Systems & Control Engineering 2012
Alexander Stotsky Bo Egardt

This paper describes an easy-to-implement, proactive control strategy for wind turbines, incorporating constraints on blade loads. The control strategy is aimed for rejecting wind gusts and is based on upwind speed measurements and a new statistical wind gust detection mechanism. The control action comprises simultaneous driveline and collective pitch control with constraints on flapwise bendin...

Journal: :Journal of Korean Institute of Intelligent Systems 2013

Journal: :Journal of International Council on Electrical Engineering 2017

Hadi Karrabi, Meysam Sajjadi Mostafa Baghani

The Axial compressor is an integrated part of a gas turbine. The central part of compressors is its blades. Blade aerodynamic has a significant effect on compressor performance. Because of the adverse pressure gradient in the compressor, any deviation in the blade profile has a significant influence on the flow field as well as the compressor performance. During the manufacturing and operation ...

2010
Jinwei Shen Pierangelo Masarati Jeremy Bain Todd Hodges

This paper presents the development of a multibody dynamics model of a VTOL teetering rotor. The developed model includes a teetering hub, containing a flexure and torque tube, rotor blades, pitch links, and swashplate system. A non-teetering rotor configuration, which modified the baseline teetering rotor by removing the teetering hinge, is also developed, and its aeromechanics characteristics...

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