An automatic riveting device is provided with a rivet suction attachment unit for attaching the head of a rivet by suction, a tightening unit for tightening a stringer and clip by the rivet, and a control unit. The control unit controls the rivet suction attachment unit so that the rivet suction attachment unit to which the head of the rivet is attached is moved toward an upper side support body and the shaft part of the rivet is inserted into a through hole formed in riveting position P, and controls the tightening nit so that after the rivet suction attachment unit inserts the rivet into the through hole and retreats from the riveting position P, an upper anvil and a lower anvil are brought into proximity and the stringer and clip are tightened by the rivet.

Insertable clamp (100), for the temporary assembly of at least two drilled structural parts (200a, 200b), including a main tubular body (10) extending along a longitudinal axis X and having a bearing surface (111) intended to come into contact with a first face (201a) of the structural parts, an elastic clip (30) capable of passing through drilled aligned holes, produced in said parts, the clip being translationally moveable along the longitudinal axis, driven by the rotation about said axis of a driver nut (50) provided with a tapped bore (51) cooperating with a threaded end (31) of said clip, the clip (30) comprising two branches (32) each ending by a hooking spur (33) intended to come into contact with a last face (202b) of the structural parts, said branches transversally and progressively moving apart along a spreader (40), placed between said branches and fixed in relation to the main body (10), when exposed to the recoil of the clip, the clamp further includes a compression spring (60) placed inside the main body (10) and holding the threaded end (31) partially engaged in the tapped bore (51) so that the clip (30) remains constantly aligned with the longitudinal axis.

A holding device for a test sheet includes a receiving arrangement for engagement with the test sheet, a handle arrangement connected rigidly to the receiving arrangement for a user for positioning the test sheet, and a pushbutton arrangement for producing a switching signal on the basis of an actuation by the user.

A holding device for a test sheet includes a receiving arrangement for engagement with the test sheet, a handle arrangement connected rigidly to the receiving arrangement for a user for positioning the test sheet, and a pushbutton arrangement for producing a switching signal on the basis of an actuation by the user.

A component mounting system for mounting a component to a frame member by a fastener, and includes: a machining apparatus configured to machine a hole in each of the frame member and the component along a machining axis and fasten the frame member and the component together by the fastener; a positioning unit configured to perform positioning of a mounting position present on the frame member relative to the machining axis; a robot configured to transfer the component to the mounting position present on the frame member; and a detector including a camera and a sensor, the camera being provided on the machining axis and configured to capture an image of the component transferred to the mounting position, the sensor being configured to detect a tilt of the component transferred to the mounting position.

A component mounting system for mounting a component to a frame member by a fastener, and includes: a machining apparatus configured to machine a hole in each of the frame member and the component along a machining axis and fasten the frame member and the component together by the fastener; a positioning unit configured to perform positioning of a mounting position present on the frame member relative to the machining axis; a robot configured to transfer the component to the mounting position present on the frame member; and a detector including a camera and a sensor, the camera being provided on the machining axis and configured to capture an image of the component transferred to the mounting position, the sensor being configured to detect a tilt of the component transferred to the mounting position.

A processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angular, in particular orthogonal, relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier.

A processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angular, in particular orthogonal, relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier.

The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis, and a processing unit which has a first upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angled with respect to the longitudinal direction, and wherein in at least one processing position of the upper tool of the first upper tool unit and in at least one processing position of the lower tool of the lower tool unit the first tool axis and the second tool axis are orientated coaxially relative to each other.

The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis, and a processing unit which has a first upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angled with respect to the longitudinal direction, and wherein in at least one processing position of the upper tool of the first upper tool unit and in at least one processing position of the lower tool of the lower tool unit the first tool axis and the second tool axis are orientated coaxially relative to each other.