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Constant swirls of innovative ideas are starting to push composites and hybrid metal-composite components for use in an ever expanding circle of products. Recent discoveries of Graphene/Au composites have invigorated innovations for its application to aerospace and space products. Attributes such as a low CTE, stiffness, and light weight attract other manufacturers of smaller products to use composites for enhanced performance and durability. The uses and economics of composites is an enormously broad subject. Examples of composite materials will be described in this paper to provide samples of applications selected for their far reaching potential to enhance product performance. Examples will also be presented to explain the application of carbon based composites where the product performance or application would not be possible without special materials.

Fusing aluminum in a multi-material lightweight vehicle is presented via studies on joining dissimilar materials, joining methods, and the performance of the joined materials. The use of aluminum offers a material that embodies properties to meet new standards as the automotive industry continues to pursue improvements in fuel efficiency and emissions. Aluminum’s strength, light weight, and corrosion resistance offers manufacturers a material alternative to steel and an additional material, which has long been known in the industry, to be employed in automotive construction. Topics of technical interest include: • Forming • Galvanic Corrosion • Welding, Fastening, Bonding • Maximizing Weight Benefits Production of strong, lightweight structures will contribute significantly to automobile manufacturers meeting mandated fuel economy standards, as well as customer preferences for utility, comfort, and safety.

In order to support the T-38 Wing Life Improvement program, the Materials and Process Product Support group was requested to perform a metallurgical examination of a test article containing several cold expanded holes drilled in an aluminum/aluminum and an aluminum/steel assembly. The assembly, complete with a wing skin which were composed of a trunnion or landing ear rib, and a tip rib, was designed to represent a miniature T-38 wing and was used to determine the feasibility of cold expanding or cold working of holes drilled in T-38 wings using automated machinery incorporating a split mandrel process per Process Specification FH-114.

Modern aircraft manufacturing involves drilling and countersinking hundreds of thousands to millions of holes. Doing this work by hand accounts for 65% of the cost of airframe assembly, 85% of the quality issues, and 80% of the lost time due to injuries. Automated drilling and countersinking replaces traditional hand methods and involves using numeric control machinery to drill and countersink a finished hole “one shot” (drilling a finished hole without using pilot holes or tool changes). This is a proven cost reducing technology that improves quality where it has been applied successfully. The focus of this book is on automating the process of drilling and countersinking holes during airframe manufacturing.

Probabilistic methods are used in calculating composite part design factors for, and are intended to conservatively compensate for worst case impact to composite parts used on space and aerospace vehicles. The current method to investigate impact damage of composite parts is visual based upon observation of an indentation. A more reliable and accurate determinant of impact damage is to measure impact energy. RF impact sensors can be used to gather data to establish an impact damage benchmark for deterministic design criteria that will reduce material applied to composite parts to compensate for uncertainties resulting from observed impact damage. Once the benchmark has been established, RF impact sensors will be applied to composite parts throughout their lifecycle to alert and identify the location of impact damage that exceeds the maximum established benchmark for impact.

The economic determination to introduce automated/mechanized operations into the airframe assembly process is complex. Any one or all of the primary elements associated with airframe assembly requires that the current process of placing, drilling, countersinking, sealing and fastening parts by hand be compared with the economic value of changing to automation. A systematic cost analysis will be used to identify the equilibrium point where value is added by inserting automation technology into the airframe assembly manufacturing process. Components will be defined and utilized to provide the resource boundary, production possibility frontier, demand curve, elasticity of demand and the cross elasticity of demand for substitutes between hand drilling and automation.

Rapid advances in cloud-based computing, robotics and smart sensors, multi-modal modeling and simulation, and advanced production are transforming modern manufacturing. The shift toward smaller runs on custom-designed products favors agile and adaptable workplaces that can compete in the global economy. This paper and presentation will describe the advances in Digital Manufacturing that provides the backbone to tighten integration and interoperability of design methods interlinked with advanced manufacturing technologies and agile business practices. The digital tapestry that seamlessly connects computer design tools, modeling and simulation, intelligent machines and sensors, additive manufacturing, manufacturing methods, and post-delivery services to shorten the time and cost between idea generation and first successful product-in-hand will be illustrated.

This essential information captures the state of the composites industry to assist engineering/technical professionals in charting a course for achieving economic success. The material characteristics of composites, their applications, and complex composites manufacturing processes depend on many factors. These are all fully considered and presented to meet the challenges that face this marketplace.

Aerospace assembly operations are still highly dependent on human labor and processes. This paper will describe and illustrate the transformational technologies that will enable replication of the human cognitive (in context) textural ability to assemble airplane and space structure. The paper will also provide use case examples where these innovative technologies have been applied successfully. Without context, data are just dots, floating around without meaning. With context data becomes an enlightened component of knowledge that brings value to information. In-context enlightened knowledge provides manufacturing visibility within factory operations. Visibility is a key component of the Smart, Brilliant, or Intelligent Factory.

Up until the last two decades, aluminum in airplanes and steel in automobiles were the primary materials used to produce these two complex machines. These metal-to-metal assemblies, and specifically the same-type metal-to-metal assemblies, have resulted in distinct manufacturing process advantages over decades of production. However, advances in material types have driven manufacturing to adapt and align the fabrication and assembly processes to continue to facilitate a quality product that is reliable, can be manufactured at a price point that is affordable and be manufactured in quantities that can be widely distributed. Dissimilar metal and composite material assemblies are now requiring highly complex manufacturing processes. Innovations in Automotive and Aerospace Assembly addresses how these new, disruptive materials usage are changing the manufacturing and production processes for the transportation industries.

“One shot” drilling and countersinking multiple stack ups of dissimilar materials with automated equipment requires a system of elements and controls. Each of the elements necessary to drill and countersink multiple stack ups of dissimilar materials in a single operation has been successfully combined and applied to an automated system. An explanation will be provided for the use of Microsoft Excel, standard drill libraries and math formulas to rapidly determine and insert the proper end effector position and drill/countersink commands into the machine control programming code. Surface location identification for coordination of the machine time and measurement based coding and the machine components necessary to interact with the time and measurement based machine code will also be explained.

The introduction of composite materials onto air vehicles has complicated the traditional hole/countersink assessment criteria due its finished-part thickness variability; softer and dissimilar properties than the metallic substructure where it is mounted and attached; and the increased attention to other acceptance criteria such as fiber tear, fiber pull, and moisture propagation in the hole that degrades fastener capability. The addition of composite materials further complicates the assembly process by adding a boundary layer of liquid shim or sealant between the composite piece (usually a skin) and the substructure. Current hole inspection systems are absent the ability to assess the interior condition of the composite hole such as fiber tear, damage to the liquid shim, and debris or burrs between the multiple stacks of dissimilar material.

A compact x-ray backscatter gauge has been developed to detect hidden edges of substructure and precisely determine edge distances prior to drilling. The portable system can be mounted at the drill for automated operation or used as a hand-held unit for manual operation. The gauge requires access to only one side of the assembly and can operate either in contact with the surface or held off the surface by as much as 10 mm. The system is capable of locating edges hidden under either a metallic or composite skin and maintaining edge distance tolerances within approximately a quarter of a mm.

The Future of Airplane Factory: Digitally Optimized Intelligent Airplane Factory defines the architecture, key building blocks, and roadmap for actualizing a future airplane factory (FAF) that is digitally optimized for intelligent airplane assembly. They fit and integrate with other FAF building blocks that aggregate to a Digitally Optimized Intelligent Airplane Factory (DOIAF). The word "intelligent" refers to the ability of a system to make right decisions and take right action in the highly dynamic and fluid environment of the modern airplane manufacturing space. The event-driven dynamics inherent in the complexity of this environment drive the need for expert knowledge which resides in intelligence systems incorporating the experience of experts. Expert knowledge need not be smart, brilliant, or possess genius as long as the outcomes are derived from right decisions resulting in right actions-applied rapidly to sustain an optimized factory enterprise.