An aircraft fuselage assembling jig is a horizontal-type jig on which an aircraft fuselage panel is placed in a laid-down state, and includes: a base with a plurality of frame indexes for positioning both ends of a plurality of aircraft fuselage frames; a plurality of header plates, each of which protrudes from the base to extend along the panel, the header plates being arranged in parallel in an axial direction of the panel; a plurality of electric cylinders radially provided on each plate, the electric cylinders moving respective receiving members in a radial direction of the panel, the receiving members contacting a skin included in the panel; and air lifting devices provided on the respective receiving members and that, when supplied with air pressure, lift the skin from receiving surfaces of the respective receiving members and support the aircraft fuselage panel such that the aircraft fuselage panel is slidable.

A system and method for drilling a hole in a vehicle structure and installing a fastener in the hole. A drill plate having openings and associated machine-readable elements is positioned on the structure. A drill gun is positioned in a particular opening and reads hole information from the associated element, and a computer determines whether the drill gun is properly set-up to drill the hole. A fastener insertion gun is positioned in the particular opening and reads fastener information from the element, and the computer determines whether the hole has been drilled and, if so, whether the fastener insertion gun is properly set-up to insert the fastener. A fastener delivery subsystem stores, tracks, and delivers fasteners to the fastener insertion gun. A system computer monitors the drilling of every hole, the insertion of every fastener, and the overall operation of the fastener delivery subsystem.

Systems and methods are provided for inspecting installation of a fastener. One method includes monitoring hydraulic pressure of a tool that is installing the fastener, detecting that the hydraulic pressure has dropped by more than a threshold amount within a period of time, determining that a pintail of the fastener has snapped in response to the detecting, and reducing the hydraulic pressure in response to the determining.

Systems and methods are provided for inspecting installation of a fastener. One method includes monitoring hydraulic pressure of a tool that is installing the fastener, detecting that the hydraulic pressure has dropped by more than a threshold amount within a period of time, determining that a pintail of the fastener has snapped in response to the detecting, and reducing the hydraulic pressure in response to the determining.

A system and method for drilling a hole in a vehicle structure and installing a fastener in the hole. A drill plate having openings and associated machine-readable elements is positioned on the structure. A drill gun is positioned in a particular opening and reads hole information from the associated element, and a computer determines whether the drill gun is properly set-up to drill the hole. A fastener insertion gun is positioned in the particular opening and reads fastener information from the element, and the computer determines whether the hole has been drilled and, if so, whether the fastener insertion gun is properly set-up to insert the fastener. A fastener delivery subsystem stores, tracks, and delivers fasteners to the fastener insertion gun. A system computer monitors the drilling of every hole, the insertion of every fastener, and the overall operation of the fastener delivery subsystem.

The present disclosure relates to riveting apparatuses, riveting devices, and methods for their use. An example riveting apparatus includes a pneumatically operated riveting tool having a working end for squeezing a rivet. The riveting apparatus includes a support bracket connected to the riveting tool proximate the working end, the support bracket having arms projecting on each side of the riveting tool. The riveting apparatus also includes a pair of spaced-apart edge rollers coupled to the support arms. The edge rollers are configured to rollably engage an edge of a work-piece so as to support the weight of the riveting tool and enable movable adjustment of the working end relative to the work-piece. The riveting apparatus includes a handle rotatably mounted to the riveting tool to enable axial rotation of the handle, the handle having an actuatable switch configured to selectively operate the riveting tool.

A multi-task device includes an element for securing the device to a motorized handler; an element for securing the device to a structure that is to be worked; at least two functional modules, each including at least one mobile member able to allow a given task to be accomplished; and a single drive and control assembly for driving and controlling the functional modules. The drive and control assembly includes: a single drive spindle; a drive capable of driving the movement of the spindle; a measurement element measuring at least one physical parameter indicative of at least one characteristic of operation of the functional modules; and a controller controlling the drive and the measurement element. The device further includes a coupling gear able to connect the single drive spindle, for the purposes of transmitting movement, alternatively to the at least one mobile member of the functional modules.

An apparatus for threading a tool unit onto an elongate structural element. The apparatus has a holding arrangement for holding it on a feed device, a tool unit to be threaded onto the elongate structural element. The tool unit has a tool axis and a vibration unit connected to the tool unit and configured to generate a periodic force in at least one first spatial direction that runs transversely with respect to the tool axis. First and second coupling components, held elastically on one another, are provided. The first coupling component is connected to the holding arrangement, the second coupling component is connected to the tool unit. The vibration unit is operated, during a feed movement of the holding arrangement for threading the tool unit onto the elongate structural element, to add an additional, periodically varying transverse component to a feed force acting on the tool unit.

There is provided an automated rivet apparatus for installing a semi-tubular fastener rivet. The apparatus includes a numerical control (NC) drilling and riveting machine and a controller. The NC drilling and riveting machine includes a lower head having a lower pressure bushing, a lower drill spindle, and a lower anvil to apply an upset force to a tail portion of the semi-tubular fastener rivet. The NC drilling and riveting machine further includes an upper head having an upper pressure bushing, an upper drill spindle, and an upper anvil that holds the semi-tubular fastener rivet to insert the semi-tubular fastener rivet in a rivet-receiving hole. The lower drill spindle countersinks the rivet-receiving hole from a lower side of a workpiece. The controller directs movement of a nose of the lower anvil to apply the upset force and form a predetermined flare contour in the tail portion within a lower countersink.

Embodiments provide a mobile robot platform for processing an aircraft structural component with a robot, with a platform which can be moved on a floor in a horizontal movement direction, and with a height adjustment unit, arranged on the platform, the robot being arranged in a vertically adjustable fashion on the height adjustment unit and in at least one processing mode of the mobile robot platform the height adjustment unit is arranged in a non-pivoting fashion with respect to the platform, the robot having robot kinematics for positioning an end effector, and the robot kinematics having a first robot joint with a first robot limb, which is mounted ahead of the first robot joint, and with a second robot limb, which is mounted after the first robot joint, and a second robot joint ahead of which the second robot limb is mounted and after which a third robot limb is mounted.