Techniques and devices are disclosed for fabrication layout device. The device includes a table with a work surface. The work surface being a continuous surface and configured to support a plurality of railing pieces for fabrication of a railing assembly. The device further includes a beam located above the work surface. The beam is operatively coupled to the table, such that the beam moves relative to the work surface in a first direction. Attached to the beam is an ink dispenser. The ink dispenser is configured to move along the beam in a second direction different from the first direction. The ink dispenser is further configured to dispense ink onto the work surface of the table in the form of a pattern of the railing assembly. Railing pieces are positioned on the pattern so that they can be assembled to one another.

A flexible, multi-product, multi-technology, expandable facility for manufacturing products, such as biologicals, pharmaceuticals, or chemicals, and manufacturing processes using elements of such a facility.

A flexible, multi-product, multi-technology, expandable facility for manufacturing products, such as biologicals, pharmaceuticals, or chemicals, and manufacturing processes using elements of such a facility.

A laser preheating control method is applied to a laser preheating control device. When a cutter processes a workpiece along a process path, a laser source of the device is provided to output a laser beam to the workpiece for selectively forming a laser spot on the workpiece surface. And according to a movement direction of the cutter, a laser controller of the device is provided to form the laser spot only on a preheating region of the workpiece, where in front of the cutter in the process path, for preheating the workpiece in the preheating region. As a result, the laser spot will not repeatedly heat the workpiece behind the cutter in the process path, and the qualitative change of the workpiece caused by repeating heating is preventable.

A method for manufacturing an aircraft floor rail includes a step of manufacturing, separately, a first part of the floor rail, comprising at least a first flange, from a corrosion-resistant first material, and a second part of the floor rail, comprising at least a second flange, from a second material having a density that is different from, in particular lower than, that of the first material, and a step of assembling the first and second parts of the floor rail by crimping.

A method for manufacturing an aircraft floor rail includes a step of manufacturing, separately, a first part of the floor rail, comprising at least a first flange, from a corrosion-resistant first material, and a second part of the floor rail, comprising at least a second flange, from a second material having a density that is different from, in particular lower than, that of the first material, and a step of assembling the first and second parts of the floor rail by crimping.

A method for laser assisted machining is provided, by utilizing a computer to develop interrelated heating and machining plans, from a variety of input data describing the material to be machined, the properties of lasers and pyrometers used for heating the material, and computer models of the machining arrangement, workpiece and final part to be produced. An iterative process continues until the machining and heating plans result in the cutting zone of the workpiece being maintained at a desired temperature with no obstruction in the line-of-sight of at least one laser and pyrometer throughout the machining process, while also maintaining the cutting tool at or below a desired maximum temperature.

A device for machining a work piece creates an electrical potential between an electrode and the work piece or another conducting body proximate to the work piece. The electrical potential establishes an electrical field within the work piece that is expected to repel electrons and create a region of positively charged ions which repel one another. This region is expected to be weakened and material is expected to be removable from this region of the work piece using less force and energy than when machined by traditional machining techniques.

A method and apparatus for laser or plasma cutting of pieces from laminar material wound in coil is provided. The apparatus provides a cutting station, with an operative cutting area and a receiving cavity, means for positioning and holding the laminar material suspended in the operative area above the receiving cavity during cutting operations, an electronic control unit and movable device for selective collection of the machined pieces. The electronic control unit controls the movement of the movable device between an active and a passive position so that that the movable device is in passive position when the cutting head is performing cutting operations generating swarf, letting such swarf to fall inside the cavity, and is in active position when the cutting head is performing cutting operations to detach pieces from the laminar material skeleton, to collect the pieces separately from the swarf and the skeleton.

A blind tack fastener includes a pull stem having an elongated shaft with an extended tail portion. The blind tack fastener also includes a crush-initiating washer, a crush sleeve, and a swage collar, surrounding the elongated shaft of the pull stem. The elongated shaft has a breakaway groove configured to create a predictive fracture point below the head-end surface of the swage collar, such that a hole in the swage collar serves as a centering lead-in for a drill that can be used to remove the blind tack fastener.