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A device for opening or closing an aircraft door includes an electric motor; a connector to connect the motor, and a driver. The driver includes a screw and nut system having a screw rotationally driven by the motor. The driver is configured to drive continuously and in sequence the connector with t

A device for opening or closing an aircraft door includes an electric motor; a connector to connect the motor, and a driver. The driver includes a screw and nut system having a screw rotationally driven by the motor. The driver is configured to drive continuously and in sequence the connector with the door in a translational movement along one preset direction and then in rotational movement.

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1. A device for opening or closing an aircraft door, the device comprising: an electric motor,means for connection with the door, andmeans for driving comprising a screw and nut system having a screw rotationally driven by the motor where said drive means are suited for driving continuously and in s

1. A device for opening or closing an aircraft door, the device comprising: an electric motor,means for connection with the door, andmeans for driving comprising a screw and nut system having a screw rotationally driven by the motor where said drive means are suited for driving continuously and in sequence the means for connection with the door in a translational movement along one preset direction and then in rotational movement, wherein the electric motor is fixed on a support and is coupled to a screw so as to be able to rotationally drive the screw, a nut for the screw and nut system engaging with said screw, where the screw drives the pivoting arm in translation, and the drive means additionally comprises: a coupling system with a first coupling part rigidly connected to the screw and a second coupling part complementary to the first coupling part and mobile relative the first coupling part between at least one coupled position in which the first coupling part drives the second coupling part and at least one decoupled position in which the two coupling parts are independent of each other, and a reduction gear with an entry shaft, rigidly connected to the second coupling part and an exit ring gear rotationally driven by the entry shaft with a reduction ratio, where the exit ring gear is connected with the pivoting arm so as to be able to rotationally drive the pivoting arm. 2. A device according to claim 1, wherein the means for connection with the door comprises a pivoting arm. 3. A device according to claim 1, wherein the screw and nut system is a screw and nut system with rolling elements. 4. A device according to claim 1, wherein the coupling system is a claw clutch. 5. A device according to claim 1, comprising a structure fixed relative to the support for the motor and means of guiding between the pivoting arm and the fixed structure. 6. A device according to claim 5, wherein the means of guiding comprises a groove and a finger having a shape adapted to slide in said groove. 7. A device according to claim 1, comprising a structure fixed relative to the support of the motor having a groove parallel to the screw of the screw/nut system and a finger which can slide in said groove and fixed on the exit ring gear. 8. A device according to claim 1, comprising disengageable means of locking. 9. An aircraft door comprising the device according to claim 1. 10. A device for opening or closing an aircraft door, the device comprising: an electric motor,means for connection with the door,disengageable means of locking andmeans for driving comprising a screw and nut system having a screw rotationally driven by the motor where said drive means are suited for driving continuously and in sequence the means for connection with the door in a translational movement along one preset direction and then in rotational movement, wherein the electric motor comprises a motor shaft and wherein the disengageable means of locking acts on said motor shaft. 11. A device according to claim 10, wherein the disengageable means of locking comprises a first coupling disk rigidly connected to the motor shaft, a second coupling disk rotationally locked and arranged opposite the first coupling disk, means of elastic pre-stressing acting on the second coupling disk in a manner to allow coupling between the first coupling disk and the second coupling disk, and a coil acting on the second coupling disk against the means of elastic pre-stressing when the coil is powered with an electric current.