A manufacturing system manufactures a rotating assembly by attaching a plurality of attached target members in a circumferential direction of a rotating main body portion. A storage member capable of storing the plurality of attached target members is placed on a stand. A measurement device measures a physical amount of the attached target member An attachment device attaches one attached target member to a predetermined position in the circumferential direction of the rotating main body portion based on the physical amount measured by the measurement device A transfer device transfers the attached target member.

A method of assembling or disassembling a housing shelf configured at least from shelf plates and frames, including a step in which a chuck holds a frame; a step of determining, based on an image captured by an imager that captures an image of the frame held by the chuck and positioned at an imaged position, a position of a target portion of the frame on the image; and a step of determining, based on the determined position on the image, at least one correction value for causing a change in a release position for the frame when the frame is released from the chuck onto the shelf plate. The target portion may be an inner wall surface of the frame. An illumination unit may be arranged between the imager and the imaged position of the frame.

An end effector provides one up assembly drilling through mated components, including a panel, by preloading the components. The end effector includes a drill and clamp dispenser for temporarily inserting and removing expansible single-sided clamps at various pre-drilled locations in the panel. In one method, pilot holes are first pre-drilled into mated components, for example an aircraft wing panel and a wing rib or spar; an initial pilot hole location is identified, and an expansible clamp is inserted into a pilot hole adjacent a desired initial fastener hole location. The clamp is torqued, causing its expansion for preloading the wing panel and rib and/or spar components under a predetermined load. The fastener hole is then drilled, the end effector untorques and removes the clamp and identifies a second (and/or next) pilot hole location, and the process is replicated.

A method for producing or assembling a product which includes at least two components, for example a motor vehicle or a motor vehicle module, by at least two fixing parts. The first fixing part is formed as a female part and the second fixing part is formed as a male part. The components disposed at a processing station and the first fixing part are measured by a measuring device, for example by a stationary camera or a camera fastened on a first or a second manipulator or photogrammetry bar having three cameras, and a deviation from a target geometry or target position is determined, and a corrected target position of the second fixing part is calculated on the basis of the determined deviation, such that the second fixing part is joined together with the first fixing part by the first manipulator and the product is thus produced.

A part manufacturing system and a method of manufacturing are provided. The system includes one or more part-moving robots, each having an end effector that grips a part. An operation robot performs an operation on the part while the part-moving robot holds the part. A fixed vision system is located apart from the robots and has at least one fixed vision sensor that senses an absolute location of the part and/or the end effector and generates a fixed vision signal representative of the absolute location. A controller collects the fixed vision signal and compares the absolute location with a predetermined desired location of the part and/or the end effector. The controller sends a repositioning signal to the part-moving robot if the absolute location varies from the predetermined desired location by at least a predetermined threshold, and the part-moving robot is configured to move the part upon receiving the repositioning signal.

A device is suitable for inserting sealing pads into one of the sectors of a turbine stator of a turbine, wherein the turbine stator includes a plurality of sectors with adjacent side faces abutting each other and slots arranged opposite each other in the adjacent side faces of two successive sectors. Each stator is configured to receive a predefined sealing pad. The device includes a support for supporting the sector; a robot arm with means for gripping the sealing pads, each predefined in accordance with the slot intended to receive it. The robot arm is configured to insert each predefined sealing pad into the slot intended to receive it of one of the side faces of the sector.

A method of producing a shim for use in an aircraft airframe (200) comprising: providing a plurality of component parts (202, 204) of the aircraft airframe (200); measuring a surface of each of the component parts (202, 204) and creating a digital models of the component part (202, 204) therefrom; digitally assembling together the digital models of the component parts (202, 204) thereby to produce a digital model (600) of at least part of the aircraft airframe (200); using that digital model (600), creating a digital model of a shim (604), the digital model of the shim (604) filling a gap between at least two digital models of component parts (202, 204) in the digital model (600) of at least part of the aircraft airframe (200); and producing a physical shim using the digital model of the shim (604).

Systems and methods for automated manufacture are provided. Nominal data measurements are obtained for an article. An identification scan is performed of parts within the work area by a machine vision system. An initial scan of the parts within or adjacent to the work area identified as being needed to form said article is performed by the machine vision system to identify target points. The target points are compared at a controller with the nominal data measurements. Automated material handling machines are commanded to grasp and move the parts within said work area to form the article.

Systems and methods for automated manufacture are provided. User input is received by way of user systems indicating nominal data measurements for an article. Automated material handling machines move parts within view of a machine vision system which performs an initial scan to identify features of said parts. Locations of areas for joining are determined by comparing the identified features to the nominal data measurements and the automated material handling machines move the parts into positions in accordance with the nominal data measurements to form the article. The automated material joining machines join the parts at said areas specified in said user input to form the article.

A device is suitable for inserting sealing pads into one of the sectors of a turbine stator of a turbine, wherein the turbine stator includes a plurality of sectors with adjacent side faces abutting each other and slots arranged opposite each other in the adjacent side faces of two successive sectors. Each stator is configured to receive a predefined sealing pad. The device includes a support for supporting the sector; a robot arm configured to grip the sealing pads, each predefined in accordance with the slot intended to receive it. The robot arm is configured to insert each predefined sealing pad into the slot intended to receive it of one of the side faces of the sector.