PROCESS AND INSTALLATION FOR REDUCING THE SHOCKING OF THE AIRCRAFT VANE BY MEANS OF ACTIVE GOVERNORS

摘要

TO REDUCE THE SHAKING CAUSED BY TAKE-OFFS ON AN AIRCRAFT BLADE 11A, 11B, A PARAMETER REPRESENTATIVE OF THE TREMBENT (DYNAMIC CONSTRAINT IN THE CANOPY) IS MEASURED, BY ACTING A RUDDER 10 FOLLOWING A REGIONAL LAW LOCATED OF THE CANOPY, ALTERNATE SOLICITATIONS OF WHICH AMPLITUDE AND PHASE ARE AUTOMATICALLY DETERMINED TO DAMAGE ONE OR MORE MODES OF VIBRATION OF THE CANOPY.