Abstract:
A method and apparatus for shaping fuselage sections. A first fuselage section is held in a holding structure in a cradle in a cradle system. Force are applied to the first fuselage section with an actuator system to a portion of the first fuselage section such that a first current shape of the first fuselage section changes towards a first desired shape for the first fuselage section to join the first the fuselage section to a second fuselage section.
Abstract:
A wire inspection system is provided. The wire inspection system includes a mirror assembly including an odd number of sides arranged to form a pyramid structure configured to surround a wire segment, wherein a plurality of the sides include a mirror, a light source configured to illuminate the wire segment, and at least one camera configured to acquire a plurality of images of the wire segment that are reflected by the plurality of mirrors, wherein each image of the plurality of images shows a different side of the wire segment.
Abstract:
A method and apparatus for shaping fuselage sections. A first fuselage section is held in a holding structure in a cradle in a cradle system. Force are applied to the first fuselage section with an actuator system to a portion of the first fuselage section such that a first current shape of the first fuselage section changes towards a first desired shape for the first fuselage section to join the first the fuselage section to a second fuselage section.
Abstract:
A wire inspection system is provided. The wire inspection system includes a mirror assembly including an odd number of sides arranged to form a pyramid structure configured to surround a wire segment, wherein a plurality of the sides include a mirror, a light source configured to illuminate the wire segment, and at least one camera configured to acquire a plurality of images of the wire segment that are reflected by the plurality of mirrors, wherein each image of the plurality of images shows a different side of the wire segment.