A rotation mechanism is provided for rotating the second sensing device.

The invention includes causing rotation of the motor in a first rotation direction if a first control signal is asserted and causing rotation of the motor in a second rotation direction if a second control signal is asserted.

The body part further includes a driving part for rotating one of the front and rear rotation parts.

An actuation system (74) is provided for rotating the assembly (26) about the axis of rotation.

The dies (32, 34) are capable of rotating together so that the patterns are in an aligned position during rotation.

The flow regulator can be rotated by turning the grille.

A motor (8) is provided for rotating the ring member (5).

In addition, the turn of the head of the spanner member enables the turn of bolts and pipes of different sizes.

The device has an axial clamp (6, 19) for clamping the axle (20), the axial clamp being provided with rotation means (25, 29) for rotating the axle (20) with respect to the rim (14).

The transfer assembly comprises a wheel (138) engaged with the frame and configured to rotate about the rotation axis.

An agitator is mounted in the bowl for rotation therein.

A first motor linked to the first valve is configured to rotate the first diverter and a second motor linked to the second valve is configured to rotate the second diverter.

A device is disclosed for controlling the attitude of a spacecraft to be rotated around a body axis of rotation.

If so, the illumination device which is rotatable will be turned to account for any rotation imparted to the aid.

The drive shaft preferably turns a sliding ratio drive transmission but may directly turn a sprocket, gear or drive wheel.