Published: 2002
Total Pages: 177
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Contents include: Floor Drilling Gantry System; ONCE (One-Sided Cell End Effector), Robotic Drilling System; Implementation of a Universal Drive Blind Fastening System During Transition from Manual to Automated Assembly; Mechanical and Structural Aspects of the C17 Cargo Ramp and Cargo Door ADFS; C17 Cargo Ramp and Door Automated Drilling & Fastening System-Project Overview; Use of Electromagnetic and Vacuum Forces on Aircraft Assembly; Lightweight HH503 Handheld Riveter; Drilling Cost Model; Investigation of Manual One Way Assembly on Primary Wingbox Structure; An Algorithm for Assembly Centric Design; Robotic Orbital Drilling of Structures for Aerospace Applications; Radial and Tangential Forces, Tool Motion, and the Formation of Lobed Holes in Drilling; One Pass Drilling of Precision Holes in Aircraft Structures; Analysis & Modeling Reduce Development Risks For Improving Integration of Large Aircraft Components; AIRBUS A340 Final Assembly by S.O.J.A.: Semi-Automatic Orbital Fuselage Join Up Robot; A Versatile Riveting System for Metal/CFC Structures; Affordable Reconfigurable Tooling; Determinant Spar Assembly Cell; Vacuum Feeding and Chip Removal; Airplane Wing Structure Fatigue Life: Impact of Misaligned Lower Rivet Dies; State-of-the-Art Automated Fastening and Its Integration into an Existing Production Infrastructure Discussed with an Actual Example; A Study of the Influence of Drilling Method and Hole Quality on Static Strength and Fatigue Life of Carbon Fiber Reinforced Plastic Aircraft Material