FIELD: machine building.
SUBSTANCE: invention relates to mechanical engineering and can be used in the processing of structural elements of the aircraft. Installation includes at least one processing station, which has a clamping frame extending along its longitudinal axis for accommodating the aircraft structural element and a processing unit. Clamping frame is articulated with the ability to move in height and rotation with two positioning towers located in the vertical plane. Clamping frame has the possibility of transverse displacement across the plane of the towers. Specified offset ensures that the loading of the clamping frame of the structural element of the aircraft and / or its unloading is carried out along the plane of the towers and passes laterally past at least one tower.
EFFECT: result is a simplified loading of the clamping frame with the structural elements of the aircraft and its unloading.
19 cl, 4 dwg
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