Abstract: A robotic system comprises an end effector including an electromagnetic clamp, a force sensor attached to the end effector for measuring force exerted by the clamp against a work piece surface, and a plurality of normality sensors. The normality sensors are positioned about the force sensor to determine whether the clamp is normal to the surface before the force sensor makes contact with the surface.

Abstract: An aircraft fuselage barrel (10) includes a skin (12) and a shear tie (18). The shear tie (18) resides within and is integrally formed with the skin (12). The shear tie (18) is separate from and configured for frame attachment thereon. A multi-ring system (79) for fuselage barrel formation includes a mold (68) with a ring (50). The ring (50) has width (W2) approximately equal to a separation distance (D) between two adjacent fuselage frames (22) and includes a module (52) that has a circumferential length (L1) that is greater than a circumferential distance between two fuselage longerons (14). A support structure (80) is coupled to and supports the mold (68). A method of forming the aircraft fuselage barrel (10) includes constructing the support structure (80). Rings (86) of the mold (68) are attached to and over the support structure (80). The mold (68) is constructed. Material is laid-up onto the mold (68) to integrally form the one-piece fuselage barrel (10) including a Hat-configured longeron (14).

Abstract: An assembly system and method for assembling an aircraft wing box or other structure that may define an interior area accessible through at least one access opening are provided. The method includes inserting a robot having an assembly tool mounted thereto into the interior area through the at least one access opening. The assembly tool may be positioned at a fastener location, and may be clamped to the structure. A hole may be made through the structure, and a fastener may be installed in the hole.

Abstract: A method and apparatus for performing operations on a workpiece. A first frame in a frame system may be held on the workpiece by applying a vacuum to the first frame. A second frame in the frame system may be detached from the workpiece by applying a pressure to the second frame. The second frame may be moved to a location on the workpiece. The second frame may be attached to the workpiece by applying the vacuum to the second frame. An operation may be performed on the workpiece.

Abstract: A method, apparatus and computer program product are present for performing a manufacturing procedure. A component may be positioned in a work area. A plurality of groups of robots may be operated in parallel and robots of each group of robots of the plurality of groups of robots may be operated in synchronism for performing a plurality of manufacturing operations at a plurality of locations on the component.

Abstract: An assembly system and method for assembling an aircraft wing box or other structure that may define an interior area accessible through at least one access opening are provided. The method includes inserting a robot having an assembly tool mounted thereto into the interior area through the at least one access opening. The assembly tool may be positioned at a fastener location, and may be clamped to the structure. A hole may be made through the structure, and a fastener may be installed in the hole.

Abstract: A fully automated method is performed on a structure having a confined space. The structure has a location that is identifiable from within the confined space and from outside the confined space. A first robotic system moves a first end effector inside the confined space such that the first end effector is positioned over the location. A first vector corresponding to the location is generated. A second robotic system moves a second end effector outside the confined space such that the second end effector is positioned over the location. A second vector corresponding to the location is generated. The first and second vectors are used to move the first and second end effectors to a new location such that the first and second end effectors are in working opposition. The first and second end effectors perform a synchronous operation at the new location.

Abstract: Apparatus for installing fasteners in a workpiece is mounted for computer controlled movement over the workpiece surface. The apparatus includes all of the tools, fasteners, drives and controls on-board that are needed to operate autonomously, without external connections. The apparatus may also include an on-board power supply for powering the tools, drives and controls. A supply of fasteners is held in an on-board replaceable cassette. An on-board fastener transferring device transfers individual fasteners from the cassette to the tools.

Abstract: Apparatus for installing fasteners in a workpiece is mounted for computer controlled movement over the workpiece surface. The apparatus includes all of the tools, fasteners, drives and controls on-board that are needed to operate autonomously, without external connections. The apparatus may also include an on-board power supply for powering the tools, drives and controls. A supply of fasteners is held in an on-board replaceable cassette. An on-board fastener transferring device transfers individual fasteners from the cassette to the tools.

Abstract: A system for removing debris generated by a cutting tool draws the debris into a mixing chamber formed in a workpiece clamp where the debris is combined with a high velocity airflow. A vacuum source draws the debris-air mixture into a cyclonic airflow extraction chamber where the mixture is accelerated before being extracted from the clamp through an exhaust channel. A clamping ring seals the area surrounding the cutting site so that air velocity in the mixing chamber is increased and debris is accelerated into the extraction chamber.

Abstract: A system includes an end effector, a robotic wrist for orienting the end effector; and a robotic arm for positioning the end effector. The robotic arm is foldable into a stack. The robotic wrist is mounted to a last link of the robotic arm.

Abstract: An instrumented fastener (e.g., a “tack” fastener) includes one or more light sources (e.g., light-emitting diodes) configured to produce a light beacon that includes encoded information regarding the instrumented fastener (e.g., part number), wherein the direction of the light beacon can be used to align external and/or internal assembly systems to the instrumented fasteners. The light beacon may be activated automatically, or via an instruction received from an external system. Once aligned, the assembly system may, for example, proceed with installing permanent fasteners between neighboring tack fasteners.

Abstract: An apparatus comprises a housing, a core located in the housing, a coil unit associated with the core and located in the housing, and a backing plate made of a high-permeability material. The apparatus may be used for generating high clamping forces between materials that are interposed between the core and the backing plate such that manufacturing operations can be carried out. The core has a cross section with an elongate shape. The coil unit is configured to generate magnetic fields and has the elongate shape.

Abstract: The different advantageous embodiments may provide an apparatus that may comprise a number of robotic platforms, a wireless communications system, and a computer system. The number of robotic platforms may be configured to move to a number of locations in an assembly area and interact with a number of robotic devices. The wireless communications system may be configured to provide communication with the number of robotic platforms and the number of robotic devices within the assembly area. The computer system may be configured to exchange information with the number of robotic platforms and the number of robotic devices using the wireless communications system.

Abstract: A morphing aircraft includes a lifting body and a telescopic lifting or control surface, such as a wing, coupled to the lifting body. The lifting surface is deployable between extended and retracted positions relative to the lifting body and configured such that, when disposed in the extended position, the flight characteristics of the aircraft correspond to those of a low-speed, high-lift aircraft, and when disposed in the retracted position, the flight characteristics of the air-craft correspond to those of a high-speed, low-lift aircraft, the lifting surface is disposed entirely within the lifting body, and an outboard end surface of the lifting surface blends continuously into an outer mold line surface of the lifting body.

Abstract: An apparatus comprises a plurality of mobile robotic machines, a wireless communications system, and a motion control system. The plurality of mobile robotic machines may be capable of moving to a number of locations in an assembly area and performing operations to assemble a structure in the assembly area. The wireless communications system may be capable of providing communications with the plurality of mobile robotic machines within the assembly area. The motion control system may be capable of generating position information for the plurality of mobile robotic machines in the assembly area and communicating the position.

Abstract: One embodiment of a fastening apparatus may include at least one of a fastener and a collar having a code with information regarding the fastener and/or collar. The code may be communicated to one or more databases of a computer. The fastener and/or collar may be tightened, located, maintained, and/or inspected according to the code and/or database information.

Abstract: An apparatus may comprise a permanent magnet unit, an end effector, and an electromagnetic clamping device. The end effector may be capable of performing workpiece operations. The electromagnetic clamping device may have an activated state and a deactivated state.

Abstract: Methods are disclosed for producing a hole in a work-piece having first and second layers of material. The first layer of material contains a full-sized hole through the first layer of material. The first layer of material is positioned adjacent the second layer of material. An orbital drill is secured to the first layer of material to position a cutting tool of the drill within the through-hole. During operation, when the cutting tool is used to cut a hole in the second layer of material, the alignment keeps the orbital drill stationary.

Abstract: A system includes an end effector, a robotic wrist for orienting the end effector; and a robotic arm for positioning the end effector. The robotic arm is foldable into a stack. The robotic wrist is mounted to a last link of the robotic arm.