SAE Technical Paper Series 2003
DOI: 10.4271/2003-01-2903
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The Design and Realisation of a Flexible Rapid Assembly Aero-Structure Manufacturing Cell – A Simulation Driven Approach

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Cited by 6 publications
(3 citation statements)
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“…It effectively integrates these technologies into an electromechanical integration application system, which combines several hardware and software systems. According to different assembly stages of the aircraft product, aircraft flexible assembly system can also be divided into three stages: component-level flexible assembly, [19][20][21][22][23][24][25][26][27] large component-level flexible assembly, 28,29 and large components alignment and joining. [30][31][32][33][34][35] Figure 1 shows the architecture of aircraft digital flexible assembly system and its application.…”
Section: Architecture and Principle Of The Flexible Assembly Systemmentioning
confidence: 99%
“…It effectively integrates these technologies into an electromechanical integration application system, which combines several hardware and software systems. According to different assembly stages of the aircraft product, aircraft flexible assembly system can also be divided into three stages: component-level flexible assembly, [19][20][21][22][23][24][25][26][27] large component-level flexible assembly, 28,29 and large components alignment and joining. [30][31][32][33][34][35] Figure 1 shows the architecture of aircraft digital flexible assembly system and its application.…”
Section: Architecture and Principle Of The Flexible Assembly Systemmentioning
confidence: 99%
“…The work described in this paper is part of much larger project at the University of Nottingham to develop a flexible rapid assembly cell for the automated manufacture of aero-structure assemblies. The individual technologies have been developed and tested for the robotic riveting, drilling and assembly [8,9].…”
Section: Introductionmentioning
confidence: 99%
“…It is the combination of non‐contact metrology and flexible robotic systems that is seen as the key enabler for the automated assembly of aerostructures. It is only by using such an approach that the inherent distortions and misalignments that occur in these types of structures can be compensated for (Webb et al , 2003). It is this methodology that is used in the work described in this paper.…”
Section: Introductionmentioning
confidence: 99%