Wing panel assembly

Details Wing panel assembly Wing panel assembly

B - Operations, Transporting

64

F

B64F 5/00 (2006.01) B23P 19/04 (2006.01) B23P 19/10 (2006.01) B64C 3/26 (2006.01)

Patent

CA 2543769

An apparatus for fabricating stiffened wing panel components for a large commercial jet transport airplanes with planks, stringers and yoke assembly including a first support structure mounted on a saddle supported on a track extending along an elongated pit, a downwardly opening U-shaped yoke on a support structure, an actuator for pivoting the yoke, a second pivotal mount for the yoke on the support structure, a rotational actuator for rotating the yoke and a fixture supported on a vertically adjustable elevator mounted in the pit.

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