Patent classifications
B23P21/00
AIRCRAFT COMPONENT POSITIONING DEVICE, AIRCRAFT ASSEMBLY SYSTEM, AND AIRCRAFT ASSEMBLY METHOD
The object is to provide an aircraft component positioning device, an aircraft assembly system, and an aircraft assembly method with which it is possible to precisely dispose components on a planar member of an aircraft without using a positioning jig. A positioning device (2) includes a detection unit (5) that detects positions of a plurality of first components installed on a planar member of an aircraft, a virtual position creation unit (6) that creates a virtual position between the plurality of first components on the basis of the positions of the plurality of first components that are detected, and a position determination unit (7) that, on the basis of the virtual position that is created, determines an installation position of a second component, different from the plurality of first components, that is installed on the planar member.
AIRCRAFT COMPONENT POSITIONING DEVICE, AIRCRAFT ASSEMBLY SYSTEM, AND AIRCRAFT ASSEMBLY METHOD
The object is to provide an aircraft component positioning device, an aircraft assembly system, and an aircraft assembly method with which it is possible to precisely dispose components on a planar member of an aircraft without using a positioning jig. A positioning device (2) includes a detection unit (5) that detects positions of a plurality of first components installed on a planar member of an aircraft, a virtual position creation unit (6) that creates a virtual position between the plurality of first components on the basis of the positions of the plurality of first components that are detected, and a position determination unit (7) that, on the basis of the virtual position that is created, determines an installation position of a second component, different from the plurality of first components, that is installed on the planar member.
Composite Assembly For Unhardened Fuselage Components
Systems are provided for fabricating a preform for a fuselage section of an aircraft. The system includes advancing a series of arcuate mandrel sections in a process direction through an assembly line, laying up fiber reinforced material onto the arcuate mandrel sections via layup stations, uniting the series of arcuate mandrel sections into a combined mandrel; and splicing the fiber reinforced material laid-up onto the arcuate mandrel sections.
Stacking apparatus and stack manufacturing system
To provide a stacking apparatus and a stack manufacturing system having high accuracy and productivity. A stacking apparatus 10 includes: a stage unit 4 on which a material to be stacked 90 is placed; a sandwiching member 11 that is vertically movable with respect to the stage unit 4, and between which and the stage unit 4 the material to be stacked 90 is sandwiched; a press member 13 that is vertically movable with respect to the sandwiching member 11 and presses the material to be stacked 90; and a guide pin 14 that guides a stack 91a pressed and stamped out of the material to be stacked 90 by the press member 13.
Door attachment method, and door moving device and sagging measurement device used therefor
A door attachment method assembles a door with a high degree of accuracy. Embodiments include a primary fastening step of bolting hinges to attachment surfaces of a vehicle body; a door panel position measurement step of measuring a relative position of a door panel in an opening when a door is brought into a cantilevered state and the hinges are fastened; a loosening step of loosening the fastening; a door position correction step of moving the door within the attachment surfaces based on a measurement result in the door panel position measurement step; and a secondary fastening step of re-fastening the hinges to the attachment surfaces. Throughout the primary fastening step, the door panel position measurement step, the loosening step, the door position correction step, and the secondary fastening step, a state where clamps respectively grip the hinges to cause the hinges to abut the attachment surfaces is maintained.
BALL BEARING ASSEMBLY METHOD AND ASSEMBLY DEVICE, AND BALL BEARING PRODUCED USING SAID ASSEMBLY METHOD
A ball bearing assembly device includes: an inner and outer ring holding unit which holds an outer ring and inner ring in a state where an outer ring raceway surface and inner ring raceway surface are eccentric to each other on a same plane so as to form a gap space; a stocker; a robot arm; a ball holding mechanism which is disposed at a tip of the robot arm; and a control unit. The control unit controls the ball holding mechanism to hold any ball from the stocker, controls the robot art to transport the held ball to a ball insertion position in the gap space corresponding to a kind of ball bearing, and inserts the held ball into the gap space, which are repeated by the number of balls of the ball bearing.
PRODUCTION PROCESSING APPARATUS, PRODUCTION PROCESSING METHOD, PROGRAM, AND WORK MANUFACTURING METHOD
[Solving Means] A production processing apparatus according to the present technology includes a first robot arm and a plurality of first tilt tables. The first robot arm is capable of conveying a work. On each of the plurality of first tilt tables, the work conveyed by the first robot arm can be mounted. The plurality of first tilt tables are tilted a predetermined angle from a horizontal surface at positions on a circumference of a circle with the first robot arm being a center, and the work is subjected to production processing in a state where the work is mounted on one of the plurality of first tilt tables.
METHOD FOR CONVEYING AT LEAST ONE VEHICLE COMPONENT TO A VEHICLE BODY WITH AT LEAST ONE ROBOT DEVICE IN AN ASSEMBLY STATION AND ASSEMBLY STATION HAVING THE ROBOT DEVICE
A method is disclosed for conveying a vehicle component to a vehicle body with a robot device in an assembly station. The assembly station includes a provisioning position in which the vehicle component is provisioned for conveying to the vehicle body. The assembly station further includes a final assembly location at which the vehicle component is final-assembled on the vehicle body. The robot device grips the vehicle component in the provisioning position and conveys the vehicle component to the final assembly location.
SYSTEM AND METHOD FOR FORMING A FOUNDATION TRUSS
A system and method for forming a foundation truss for a box spring or mattress foundation frame includes a first truss rail assembly station having a series of block feeders, a top rail hopper and a filler strip hopper that received stacks of truss components such as blocks, top rails and filler strips and feed such truss components into stacked registration. The stacked truss components are moved into engagement with a series of staplers that secure the filler strips, top rails and blocks together to form first truss rail portions, which are then fed to a second truss rail assembly station where a bottom rail is automatically applied thereto.
AUTOMATIC PRODUCTION SYSTEM
This system has an articulated robot having an arm and a base portion which rotatably supports the arm; and a rotation positioner to which the base portion of the articulated robot is mounted. A turn axis of the base portion of the articulated robot is orthogonal to a rotation axis of the rotation positioner. Thus, interference of a workpiece with the arm can be avoided and flexibility of works performed by the robot can be expanded.