Abstract: The present disclosure includes a method and apparatus for changing livery on a vehicle. A method of inkjet printing an exterior surface of a vehicle, includes preparing at least a portion of the exterior surface of the vehicle in a first bay using crossflow or downflow air handling and using explosion protected equipment. That method includes inkjet printing at least the portion of the exterior surface of the vehicle in a second bay. This method includes clear-coating at least the portion of the exterior surface of the vehicle in a third bay using downflow or crossflow air handling, using air filtration and using explosion protected equipment.

Abstract: The present disclosure includes a method and apparatus for ink jet printing an exterior surface of a vehicle including a reversibly moveable crossbeam mounted above an open pit; a first track located above the reversibly moveable crossbeam, a first reversibly moveable monument including a first serial robotic manipulator including a first end effector defining a first end effector range of motion based on fully extended reversible movement of the first serial robotic manipulator; a second track located in the open pit beneath the reversibly moveable crossbeam; a second reversibly moveable monument coupled to the second pair of rails, the second reversibly moveable monument including a second end effector defining a second end effector range of motion based on fully extended reversible movement of the second serial robotic manipulator. The first end effector range of motion overlaps the second end effector range of motion.

Abstract: Methods and structural gap filler for one up assembly of structures. Drilling debris generated between the first component and the second component during drilling of an injection hole are encapsulated by injecting a structural gap filler through the injection hole and between the first component and the second component.

Abstract: A fuel tank protection system having an outer wall for a fuel tank, an inner wall for the fuel tank, a gap between the inner wall and outer wall, and an intumescent material located within the gap between the inner wall and the outer wall.

Abstract: Fuel tanks and methods of manufacture are presented. A fuel tank in a wing of an aircraft comprises a composite skin, a composite spar, and a structural gap filler between a flange of the spar and a first surface of the skin, the structural gap filler having a compressive strength equivalent to or greater than a compressive strength of a joint between the composite spar and the composite skin.

Abstract: A device actuation system for actuating a treatment device includes a first drive gear rotatably mountable to the treatment device, a coupler rail slidably mountable to the treatment device, a second drive gear rotatably mountable to the coupler rail, and a coupler gear rotatably mountable to the treatment device and engageable with the coupler rail. In addition, the device actuation system includes a drive rail locatable between the first drive gear and the second drive gear of the gear system. The coupler gear is rotatable to move the coupler rail in a manner maintaining the second drive gear in continuous engagement with the drive rail against the first drive gear. The first drive gear and the second drive gear are rotatable in a manner causing at least one of translation and rotation of the treatment device relative to the drive rail.

Abstract: A pitch-yaw actuation system includes a pitch frame, a yaw frame, a pitch actuator, a yaw actuator, and a universal joint assembly. The pitch frame is pivotably coupled to a device frame via a pitch hinge. The yaw frame is pivotably coupled to the pitch frame via a yaw hinge. The pitch actuator pivots the pitch frame about a pitch axis. The yaw actuator pivots the yaw frame about a yaw axis oriented orthogonal to the pitch axis. The universal joint assembly couples the yaw actuator to the yaw frame, and includes a universal joint slidably coupled to a linear guide mechanism. The guide mechanism axis is oriented at an angle that allows the universal joint to move in a manner accommodating misalignment of the yaw actuator with the yaw frame during pivoting of at least one of the pitch frame and the yaw frame.

Abstract: An autonomous shim fabrication system includes a gap data acquisition device that acquires gap data for a gap between mating surfaces of components that are to be assembled, a gap data conversion system that converts the gap data into three dimensional computer solid model data of the gap, a solid model data correction system that corrects the solid model data to generate corrected solid model data of the gap, and a solid model data conversion system that converts the corrected solid model data into a manufacturing sequence. When the manufacturing sequence is executed by a computer communicatively coupled to a manufacturing machine, the system controls the manufacturing machine to manufacture a shim corresponding to the gap.

Abstract: A method for manufacturing composite parts. A temporary removal layer may be placed on an inner mold line tool. A composite material may be laid up on the inner mold line tool for a composite part. The inner mold line tool may be positioned with the composite part inside an outer mold line tool. The composite part and the temporary removal layer may be transferred from the inner mold line tool to the outer mold line tool. The inner mold line tool and the temporary removal layer may be removed from inside of the outer mold line tool after transferring the composite part and the temporary removal layer to the outer mold line tool.

Abstract: A method for manufacturing composite parts. A temporary removal layer may be placed on an inner mold line tool. A composite material may be laid up on the inner mold line tool for a composite part. The inner mold line tool may be positioned with the composite part inside an outer mold line tool. The composite part and the temporary removal layer may be transferred from the inner mold line tool to the outer mold line tool. The inner mold line tool and the temporary removal layer may be removed from inside of the outer mold line tool after transferring the composite part and the temporary removal layer to the outer mold line tool.