Control rod for adjusting a rotor blade of a helicopter
The invention relates to a control rod for the adjusting of a helicopter rotor blade, wherein the control rod can be adjusted in longitudinal direction, comprising: at least one contact area element, at least one limit stop element, which is designed to limit the adjustability of the control rod in longitudinal direction to a specifiable adjusting range in interrelation with the at least one contact area element, wherein the limit stop element can be transferred from a first position to a second position, wherein the at least one stop element limits the adjustability of the control rod in the first position and enables the adjustability of the control rod beyond the specifiable adjusting range in the second position.
1. A control rod for adjusting a helicopter rotor blade, wherein the control rod is adjustable along a longitudinal axis of the control rod, the control rod comprising:
at least one contact area element; and
at least one limit stop element having a fixed state and a movable state relative to a housing;
in the fixed state, a bolt is inserted through the housing and into a hole in the at least one limit stop element to fix the at least one limit stop element to the housing and the at least one limit stop element cooperates with the at least one contact area element to limit adjustability of the control rod along the longitudinal axis of the control rod to a specifiable adjusting range;
in the movable state, the bolt is removed from the hole in the at least one limit stop element to allow the at least one limit stop element to rotate around the longitudinal axis from a first position to a second position to adjust the specifiable adjusting range.
2. The control rod of claim 1 , further comprising:
a first support element coaxially arranged around the longitudinal axis of the control rod and configured to be rotatable around the longitudinal axis of the control rod;
wherein the at least one contact area element comprises at least one protrusion that extends along the longitudinal axis of the control rod and is interrupted in a circumferential direction; and
wherein the at least one limit stop element is coaxially arranged around the longitudinal axis of the control rod;
wherein the at least one limit stop element comprises a second protrusion that extends along the longitudinal axis of the control rod.
3. The control rod of claim 2 , wherein the control rod is electrically adjustable along the longitudinal axis via an actuator.
4. The control rod of claim 1 , wherein the control rod is electrically adjustable along the longitudinal axis via an actuator.
5. The control rod of claim 4 , wherein the actuator for the adjusting of the control rod comprises a spindle drive comprising a spindle and a spindle nut;
wherein the spindle is drivable via a gear stage of a planetary gear,
wherein the planetary gear is driven by an electric motor; and
wherein the spindle for the adjusting of the control rod moves the spindle nut along the longitudinal axis.
6. The control rod of claim 5 , wherein the at least one contact area element is connected to a gear wheel of the gear stage to prevent rotation of the contact area element relative to the gear wheel.
7. The control rod of claim 6 , wherein the actuator can be operated as a function of setpoint values, actual positions, and sensor signals.
8. The control rod of claim 5 , wherein the at least one contact area element is made in an integral manner with a gear wheel of the gear stage.
9. The control rod of claim 8 , wherein the actuator can be operated as a function of setpoint values, actual positions, and sensor signals.
10. The control rod of claim 5 , wherein the actuator can be operated as a function of setpoint values, actual positions, and sensor signals.
11. The control rod of claim 4 , wherein the actuator can be operated as a function of setpoint values, actual positions, and sensor signals.
12. The control rod of claim 1 , wherein the bolt further comprises at least one of a threaded bolt and a screw.