Helicopter rotors have traditionally been equipped with passive dampers for aeromechanical stability. These passive systems have fixed characteristics, and add to mechanical complexity and high maintenance cost. Furthermore, they are unable to change to compensate for an unexpected loading trends as typically encountered by a rotary wing vehicle. Semi-active control strategies are dissipative in nature, inherently stable, and require a little energy to operate. Hence, they appear to be particularly promising in addressing a number of the challenges facing active control strategies, in that the devices are low power, fail-safe, and reliable. In this study, author investigates friction based semi-active approach for ground resonance stability augmentation and proposes novel strategies for the adaptive, selective and individual damping control. The effectiveness of these control strategies is validated on a comprehensive multibody system model of an army helicopter. The analytical study is supplemented with a novel design of a semi-active lead lag damper and various aspects of its design in application to commercial rotors are discussed.
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Dr. Sandeep Agarwal is a Rotor Dynamics Engineer at the Boeing Company. Prior to that, he worked at the Center of Excellence in Rotorcraft Technology at Georgia Institute of Technology. His primary interests include Rotor dynamics, Aeroelasticity, Structural Morphing and Structural Optimization. He has authored several technical publications.
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Kartoniert / Broschiert. Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Agarwal SandeepDr. Sandeep Agarwal is a Rotor Dynamics Engineer at the BoeingnCompany. Prior to that, he worked at the Center ofnExcellence in Rotorcraft Technology at Georgia Institute ofnTechnology. His primary interests include Ro. N° de réf. du vendeur 4964243
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Taschenbuch. Etat : Neu. Aeromechanical Stability Augmentation Through Semi-Active Control | Semi-Active Friction based Damping for Rotorcraft Ground Resonance Stability | Sandeep Agarwal | Taschenbuch | Englisch | VDM Verlag Dr. Müller | EAN 9783639175325 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 101522117
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Helicopter rotors have traditionally been equippedwith passive dampers for aeromechanical stability. These passive systems have fixed characteristics, andadd to mechanical complexity and high maintenancecost. Furthermore, they are unable to change tocompensate for an unexpected loading trends astypically encountered by a rotary wing vehicle. Semi-active control strategies are dissipative innature, inherently stable, and require a littleenergy to operate. Hence, they appear to beparticularly promising in addressing anumber of the challenges facing active controlstrategies, in that the devices are low power,fail-safe, and reliable. In this study, authorinvestigates friction based semi-active approach forground resonance stability augmentation and proposesnovel strategies for the adaptive, selective andindividual damping control. The effectiveness ofthese control strategies is validated on acomprehensive multibody system model of an armyhelicopter. The analytical study is supplemented witha novel design of a semi-active lead lag damper andvarious aspects of its design in application tocommercial rotors are discussed. N° de réf. du vendeur 9783639175325
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