Inventors:
Jack S. Hagelin - Woodinville WA, US
Sascha K. Ruegamer - Seattle WA, US
Tim D. Thornton - Bothell WA, US
Sean C. O'Meara - Seattle WA, US
Jeffrey R. Ellis - Snohomish WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
F16F 7/104, F16F 7/112
Abstract:
A method for damping aeroelastic modes, including limit cycle oscillations (LCO), is implemented by determining a mass for a tuned mass damper (TMD) based on an modal frequency for a mode having a potentially positive growth rate and attaching a TMD to at least one attachment point with significant motion such that a damping axis of the tuned mass damper is substantially oriented in a direction aligned with the local modal deflection.