Vibration Suppression of a Helicopter Using Pendulum Absorbers : First Elastic Mode of a Blade

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概要

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• Centrifugal pendulum vibration absorbers are widely used as a vibration suppression device for helicopters. The vibration characteristics of this absorber have been investigated by utilizing linear anti-resonance theory. However, it has been noted that nonlinear characteristics appear when pendulums swing at large amplitudes. The authors investigated vibration suppression characteristics of pendulum absorbers considering nonlinear characteristics of pendulums. In the first report, we investigated a two-degree-of-freedom (2DOF) system composed of a rigid blade and a pendulum. In this system, the blade was excited by a harmonic deflection motion of the shaft. In the second report, we investigated a three-degree-of-freedom system composed of a fuselage, a rigid blade and a pendulum. In this third study, the model has 3DOF and is composed of a blade, a pendulum and a rotor mount. The blade is assumed to be flexible and only the first elastic mode is considered. An aerodynamic excitation force is applied to the blade. The vibration suppression characteristics of this system are investigated theoretically and experimentally.

著者

• Ishida Yukio

  Nagoya University

• NAGASAKA Imao

  Chubu Institute of Technology

• KOYAMA Takayuki

  Mitsubishi Hevy Industry Co. Ltd.

• FUJIMATSU Naoki

  Makita Co. Ltd.

関連論文

• On the Internal Resonance in a Nonlinear Two-Degree-of-Freedom System : Forced Vibrations near the Higher Resonance Point When the Natural Frequencies Are in the Ratio 1:2
• Ultra-Subharmonic Oscillations in a Nonlinear Vibratory System
• Nonstationary vibrations of a rotating shaft with nonlinear spring characteristics during acceleration through critical speeds.
• On the Internal Resonance in a Nonlinear Two-degree-of-freedom System : When the Natural Frequencies Are in the Ratio 2 : 3
• Foreword
• Vibration Suppression of a Helicopter Using Pendulum Absorbers : First Elastic Mode of a Blade
• Vibration Suppression of a Helicopter Fuselage by Pendulum Absorbers : Rigid-Body Blades with Aerodynamic Excitation Force
• Preface

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