초록 ▼

In an individual rotor blade control device for a helicopter main rotor with a rotor shaft that can be driven by a main drive, with an even number of rotor blades that are arranged on the periphery of a rotor hub, with primary control mechanisms for collective and sinusoidal, cyclic rotor blade adju

In an individual rotor blade control device for a helicopter main rotor with a rotor shaft that can be driven by a main drive, with an even number of rotor blades that are arranged on the periphery of a rotor hub, with primary control mechanisms for collective and sinusoidal, cyclic rotor blade adjustment, which include a transfer element for the control movements from a non-rotating system to a rotating system and with actuators that are individually allocated to the rotor blades, wherein the actuator control movement is superimposed onto the control movement of the primary control mechanisms and each actuator is equipped with a safety device in order to bring the actuator into its final position and keep it there, if necessary, it is suggested that the setting angle change of one half of the rotor blades have an opposed direction due to the securing of the actuators in their final positions, like the setting angle change of the other half of rotor blades, and that the rotor blades of each half be distributed on the periphery in such a way that no pitching moments that could affect the rotor are generated.

대표청구항 ▼

1. An individual rotor blade control device for a helicopter main rotor (2) having a rotor shaft (4) driven by a main drive, with an even number of at least four rotor blades (8, 10, 12, 14, 16, 18) evenly distributed on the periphery of a rotor hub (6), comprising a primary control means (20) for c

1. An individual rotor blade control device for a helicopter main rotor (2) having a rotor shaft (4) driven by a main drive, with an even number of at least four rotor blades (8, 10, 12, 14, 16, 18) evenly distributed on the periphery of a rotor hub (6), comprising a primary control means (20) for collective and sinusoidal, cyclic rotor blade adjustment, which includes a transfer element for the control movements from a non-rotating system to a rotating system and actuators (36, 38, 40, 42, 44, 46) individually allocated one to each rotor blade (8, 10, 12, 14, 16, 18), wherein actuator control movement is superimposed onto the control movement of the primary control means (20) and each actuator is equipped with a safety device (54, 56) to bring the actuator into its final position and keep it there, if necessary, wherein half the rotor blades (8, 12, 16) are assigned to a first group of rotor blades and half the rotor blades (10, 14, 18) are assigned to a second group of rotor blades, the actuators when secured in their final positions provide angle changes of the first group of rotor blades (8, 12, 16) opposite in direction to the blade angle changes of the second group of rotor blades (10, 14, 18), and that each said group of rotor blades consists of at least two sub-groups (8, 12, 16; 10, 14, 18) evenly distributed on the periphery, with adjacent sub-groups being allocated to different said groups. 2. The rotor blade control device of claim 1, wherein the sub-groups (8, 12, 16; 10, 14, 18), respectively, comprises only one rotor blade so that the setting angle changes of adjacent rotor blades have opposed directions due to the securing of the actuators in their final positions. 3. The rotor blade control device of claim 1, wherein each of the actuators (36 through 46) is a linear actuator with two sub-assemblies that can move in relation to one another, wherein each sub-assembly contains a connecting point (48, 50) and the connecting points have a minimum distance in a first final position and a maximum distance from each other in a second final position. 4. The rotor blade control device according to claim 3, wherein to the rotor blades (8, 12, 16) of the first group actuators (36, 40, 44) are allocated, which can be held in the first final position, and that to the rotor blades (10, 14, 18) of the second group actuators (38, 42, 46) are allocated, which can be held in the second final position. 5. The rotor blade control device of claim 3, wherein the safety device is equipped with a pre-stressed element (56), which can be expanded parallel to the adjusting direction of the actuator, arranged between the two sub-assemblies of the actuator that can move in relation to one another and serves the purpose of bringing the sub-assemblies into a final position and holding them there. 6. The rotor blade control device of claim 5, wherein the prestressed element is a spring (56).