System for reducing vibrations or stresses in a rotor blade system
In one aspect, the present disclosure provides a system for reducing vibrations or stresses in a rotor blade system. The system may include at least three rotor blades configured to be rotated about a main rotor axis, where each of the three rotor blades may be adjusted by at least one electrically-adjustable control rod of a plurality of control rods. The plurality of control rods may include a first number of control rods forming a first group, and the plurality of control rods may include a second number of control rods forming a second group. A first circuit for may activate or deactivate the first group of control rods, and a second circuit may activate or deactivate the second group of control rods.
1. method for reducing vibrations or stresses in a rotor blade system, the method comprising:
rotating a first rotor blade, a second rotor blade, and a third rotor blade about a main rotor axis;
adjusting each of the three rotor blades by at least one electrically-adjustable control rod of a plurality of control rods, wherein the plurality of control rods includes a first number of control rods forming a first group, and wherein the plurality of control rods including a second number of control rods forming a second group;
activating or deactivating the first group of control rods with a first circuit; and
activating or deactivating the second group of control rods with a second circuit,
adjusting the first group of control rods during rotation of the at least three rotor blades when the second group of control rods remains static during normal operation of the rotor blade system; and
adjusting the second group of control rods during rotation of the at least three rotor blades when the first group of control rods remains static during normal operation of the rotor blade system.
2. The method of claim 1 , wherein the system includes a fourth rotor blade, wherein the first rotor blade and the third rotor blade are situated opposite one another, wherein the second rotor blade and the fourth rotor blade are situated opposite one another, wherein the first and second rotor blades are assigned to the first group, and wherein the third and fourth rotor blades are assigned to the second group.
3. The method of claim 1 , wherein the control rods assigned to the first group are arranged consecutively in a peripheral direction of the axis.
4. The method of claim 3 , wherein the control rods assigned to the second group are arranged consecutively in the peripheral direction of the axis.
5. The method of claim 1 , wherein the system includes an even number of rotor blades, and wherein each control rods is assigned to a different group with respect to the control rods arranged consecutively in a peripheral direction.