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A method for adjusting a pivotally mounted rotor blade of a wind energy converter includes controlling a first drive and a second drive to collectively turn the rotor blade into an operating position; detecting whether a failure of the first drive has occurred; activating, when the failure of the fi

A method for adjusting a pivotally mounted rotor blade of a wind energy converter includes controlling a first drive and a second drive to collectively turn the rotor blade into an operating position; detecting whether a failure of the first drive has occurred; activating, when the failure of the first drive has occurred, a first activatable lockout connected to the rotor blade, which prevents turning of the rotor blade into the operating position while allowing turning of the rotor blade into a feathered position; and controlling, when the failure of the first drive has occurred, the second drive to turn the rotor blade into the feathered position.

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1. A device for adjustment of a pivotally mounted rotor blade of a wind energy converter, the device comprising: a first drive and a second drive that cooperate to turn the rotor blade between an operating position and a feathered position; a first activatable lockout connected to the rotor blade, w

1. A device for adjustment of a pivotally mounted rotor blade of a wind energy converter, the device comprising: a first drive and a second drive that cooperate to turn the rotor blade between an operating position and a feathered position; a first activatable lockout connected to the rotor blade, which in an activated state prevents turning of the rotor blade into the operating position, but allows turning of the rotor blade into the feathered position; a detector for detecting a failure of the first drive; and a controller that controls the second drive to turn the rotor blade into the feathered position when the detector has detected the failure of the first drive. 2. The device of claim 1, wherein the controller is configured to activate the first activatable lockout when the detector has detected the failure of the first drive. 3. The device of claim 1, wherein at least one of the first and second drives comprises an electric motor, the device further comprising a first lockout activator, which activates the first activatable lockout in case of loss of electric power. 4. The device of claim 1, wherein the first activatable lockout comprises a backstop, which prevents turning of the rotor blade into the operating position. 5. The device of claim 4, further comprising a second activatable lockout, which in an activated state prevents turning of the rotor blade into the operating position but allows turning of the rotor blade into a feathered position, the second activatable lockout being configured to prevent the turning of the rotor blade by locking a drive axis of the second drive. 6. The device of claim 1, wherein the first activatable lockout is configured to prevent the turning of the rotor blade by locking a drive axis of the first drive. 7. The device of claim 1, wherein the first and second drives are configured to act on the rotor blade at different points of action. 8. The device of claim 1, wherein the first and second drives include respective first and second pinions meshing with a circular gear coupled to the rotor blade. 9. The device of claim 8, wherein the first and second pinions are positioned, with respect to a central axis of the circular gear, at a mutual angular distance of less than 90°. 10. The device of claim 8, wherein the circular gear comprises an angular zone of surface-hardened gear teeth, the angular zone encompassing less than 180° of the circular gear. 11. The device of claim 1, wherein a plurality of drives is provided to collectively supply a required torque for turning the rotor blade at any angular position of the rotor hub during operation of the wind energy converter, and wherein drives remaining after a failure of one of the plurality of drives collectively supply less than the required torque. 12. The device of claim 11, wherein each of the plurality of drives is configured to supply an equal individual torque. 13. A wind energy converter, comprising: a rotor hub; a rotor blade pivotally mounted on the rotor hub; a device for adjustment of the rotor blade, the device including a first drive and a second drive that cooperate to turn the rotor blade between an operating position and a feathered position; a first activatable lockout connected to the rotor blade, which in an activated state prevents turning of the rotor blade into the operating position, but allows turning of the rotor blade into the feathered position; a detector for detecting a failure of the first drive; and a controller that controls the second drive to turn the rotor blade into the feathered position when the detector has detected the failure of the first drive. 14. The wind energy converter of claim 13, wherein the rotor blade is mounted on the rotor hub for rotation around a pivotal axis, the rotor blade comprising a center of gravity positioned off the pivotal axis. 15. A method for adjusting a pivotally mounted rotor blade of a wind energy converter, the method comprising: controlling a first drive and a second drive to collectively turn the rotor blade into an operating position; detecting whether a failure of the first drive has occurred; activating, when the failure of the first drive has occurred, a first activatable lockout connected to the rotor blade, which prevents turning of the rotor blade into the operating position while allowing turning of the rotor blade into a feathered position; and controlling, when the failure of the first drive has occurred, the second drive to turn the rotor blade into the feathered position. 16. The method of claim 15, further comprising decoupling the first drive from the rotor blade when the failure of the first drive has occurred. 17. The method of claim 16, wherein the first activatable lockout is coupled to a drive axis of the first drive, the method further comprising activating, when the failure of the second drive has occurred, a second activatable lockout, which in the activated state prevents turning of the rotor blade into the operating position but allows turning of the rotor blade into a feathered position, the second activatable lockout being coupled to a drive axis of the second drive. 18. The method of claim 16, further comprising controlling the first drive to turn the rotor blade into the feathered position, when the failure of the second drive has occurred. 19. The method of claim 15, comprising controlling the first and second drives to exert mutually counteracting torques on the rotor blade.