摘要 |
An active noise control (ANC) system for a helicopter that is operative to effectively nullify one or more high frequency vibrations emanating from the main transmission gearbox thereof at the gearbox/airframe interface, thereby significantly reducing the interior noise levels of the helicopter, that is design optimized to minimize the number of actuators required, and that is design optimized to minimize contamination forces arising from operation of the system actuators. The ANC system includes modified transmission beams that are mechanically stiffened to function as rigid bodies with respect to the one or more of the high frequency vibrations, a plurality of actuators disposed in combination with the modified transmission beams, a plurality of sensors disposed in combination with the modified transmission beams in a collinear, spaced apart functional correlation with respective actuators, and controllers interconnecting individual actuators with respective functionally correlated sensors. |
申请人 |
UNITED TECHNOLOGIES CORP., HARTFORD, CONN., US |
发明人 |
YOERKIE, CHARLES, A., NEWINGTON, CT 06111, US;WELSH, WILLIAM, A., NORTH HAVEN, CT 06473, US;SHEEHY, THOMAS, W., HAMDEN, CT 06517, US |