The present invention discloses a riveting robot, comprising: a robot part provided on a chassis, and detachably coupled with a riveting tool part through a hydraulically quick change disk; a visual position identification part provided on a side of the hydraulically quick change disk and secured on the sixth axis of the front end of the robot part; an automatic rivet feeding part provided on a mounting baseplate which is secured on a chassis through a two-stage vibration damping structure; a riveter tailing material collection part used for collecting tailing materials produced during riveting; a riveting quality judgment part used for collecting riveting data, and processing and generating a riveting curve to realize judgment of the riveting quality.

A fastening device for feeding fasteners to a workpiece and for joining it, the fastening device comprising a fastening tool, a fastening device system. The fastening device including a magazine arrangement mounted on the fastening tool. The magazine arrangement having a magazine for holding a fastener, a magazine plate, and a base plate. The magazine plate includes a plate body and a closure arrangement with a closure slider adapted to move between an open position and a closed position, and a toggle mechanism adapted to move the closure slider from the closed position to the open position.

A component manufacturing method includes a step in which a robot for attachment gripping a long frame presses the frame against a tabular skin and a step in which, in a state in which the frame is pressed against the skin, a robot for riveting gripping a first rivet inserts the first rivet into a first through-hole formed in the skin and a second through-hole formed in the frame. In the step, the robot for riveting changes a position in the gripped first rivet in a direction perpendicular to an axial direction of the first rivet according to a force received by the first rivet from the skin or the frame.

The invention relates to a joining unit (10, 40) for an articulated arm robot (12, 44) for joining a component (24, 58) with a joining element (28, 60) by applying an axial force. The joining unit (10, 40) comprises a base element (14, 42) for connecting to an articulated arm robot (12, 44). The base element (12, 42) is connected to an advancing unit (13, 46), which can be moved relative to the base element (14, 42) in an axial direction in and against a setting direction. The advancing unit (13, 46) is connected to a setting device (16, 54), which can be moved together with the advancing unit (13, 46). Furthermore, a pressure piece (26, 50) mounted for movement relative to the advancing unit (13, 46) in and against the setting direction is connected to the advancing unit (13, 46) by means of a coupling unit (17, 48). The invention is distinguished in that the coupling unit (17, 48) comprises a blocking unit (18, 56), which, starting from a predefined axial blocking position, prevents motion of the pressure piece (26, 50) relative to the advancing unit (13, 46) against the setting direction so long as the advancing force is less than the set blocking force. The blocking unit comprises a release device (20, 62), by means of which the relative motion of the pressure piece (26, 50) against the setting direction is enabled.

There is provided a spherical mechanism robot assembly for accessing a confined space in a vehicle, to perform confined space operation(s) in the vehicle. The assembly includes a base structure configured for attachment to the vehicle. The assembly includes a spherical mechanism structure having a first end attached to the base structure, and having a second end. The spherical mechanism structure includes a plurality of mechanical links, joints coupling the plurality of mechanical links together, and a plurality of actuators having one or more actuators coupled at each joint of the plurality of joints. The assembly includes an end effector attached to the second end of the spherical mechanism structure. The assembly is configured such that a majority portion remains outside of the confined space, while a remaining portion of the assembly accesses and occupies the confined space in the vehicle, to perform the confined space operation(s) in the vehicle.

A method and apparatus for positioning an end effector relative to a fuselage assembly. The end effector is positioned relative to an expected reference location for a reference point on the fuselage assembly using data from a first metrology system. After positioning the end effector relative to the expected reference location, an actual reference location for the reference point on the fuselage assembly is identified using data from a second metrology system. The end effector is positioned at an operation location based on the actual reference location identified.

A method and apparatus for performing an assembly operation. A tool may be macro-positioned within an interior of a fuselage assembly. The tool may be micro-positioned relative to a particular location on a panel of the fuselage assembly. An assembly operation may be performed at the particular location on the panel using the tool.

A method for performing operations on a target workpiece including taking an operating tool unit by an industrial robot, carrying the tool unit to the workpiece, releasing the tool unit at the workpiece, moving the robot away from the tool unit, performing one or more operations on the workpiece through the tool unit while the tool unit moves with the workpiece; and retrieving the tool unit from the workpiece after the tool unit has performed the one or more operations on the workpiece. A robotic assembly for performing a method including at least one industrial robot, at least one operating tool unit, and a quick tool changer for detachably coupling the tool unit with the industrial robot including a first tool changer part arranged in the industrial robot and a second tool changer part arranged in the operating tool unit.

There is provided a spherical mechanism robot assembly for accessing a confined space in a vehicle, to perform confined space operation(s) in the vehicle. The assembly includes a base structure configured for attachment to the vehicle. The assembly includes a spherical mechanism structure having a first end attached to the base structure, and having a second end. The spherical mechanism structure includes a plurality of mechanical links, joints coupling the plurality of mechanical links together, and a plurality of actuators having one or more actuators coupled at each joint of the plurality of joints. The assembly includes an end effector attached to the second end of the spherical mechanism structure. The assembly is configured such that a majority portion remains outside of the confined space, while a remaining portion of the assembly accesses and occupies the confined space in the vehicle, to perform the confined space operation(s) in the vehicle.

A method and apparatus for building an assembly fixture for holding a fuselage assembly. A number of cradle fixtures may be driven across a floor to an assembly area. The number of cradle fixtures may be configured to form the assembly fixture.