Abstract

Abstract The use of fiber-metal laminates (FML) allows for substantial advantages over a fuselage skin made of monolithic aluminum materials. Glass fiber prepreg reinforced aluminium is characterized by high damage tolerance capabilities, supporting the structural strength capability in case of any kind of damage. For this reason, FML, and GLARE in particular, have been identified as superior materials for aerospace applications. More than 400m2 FML is applied on each A380, as skin panels and as D-noses for both, vertical and horizontal stabilizer. FML possess the potential to become the baseline material for next-generation single-aisle aircrafts [1, 2, 6]. The development of a new production chain that will allow automated fuselage production for future short-haul aircrafts is the focus of the studies that make up the joint project AUTOGLARE. As part of the fifth call-up for the German Aeronautical Research Programme (LuFo), the German Aerospace Center (DLR) is working with its project partners Airbus Operations, Premium Aerotech (PAG) and the Fraunhofer Gesellschaft (FhG). The development of a production chain for stiffened fuselage panels made of Fiber metal Laminates should support a production rate of 60 aircraft per month [3]. This study contains the research work of the DLR and FhG regarding the automated and quality assured process for chain stiffened FML fuselages. In addition to a detailed explanation of the systems that were set up, this paper covers the planned tests, the completed demonstration models and the findings derived from them.

Highlights

  • Introduction and state of the artAbstractThe use of fiber-metal laminates (FML) allows Thanks to the multiple load path character of the FML confor substantial advantages over a fuselage skin made of cept, the structural capability of fuselage shells designed monolithic aluminum materials

  • Glass fiber prepreg rein- with the low cost alloy 2024 could be improved signififorced aluminium is characterized by high damage toler- cantly

  • The GLARE fuselage panels, which are applied on ance capabilities, supporting the structural strength capa- the A380, which are applied on the A380, fulfill and exbility in case of any kind of damage

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Summary

Quality Assurance in Glass Prepreg

FML are parts mostly manufactured manually by workers, which results in high production times and non-reproducible part quality. If this material is to be used for the generation short range aircraft with up to 60 units per month, an automation of the manufacturing process to increase the productivity is necessary [8]. For this reason, the layup of glass fiber prepreg material with automated placement technologies like Auto-. Inside the project AUTOGLARE, the approach includes concept design, development and implementation of feasible feature mated Tape Laying (ATL) or Automated Fiber Placement (AFP) were tested at the DLR research platform Grofi in

Steering is required to layup gap- and overlap-free into a double
Curing with inline QA
State of the art in Airbus A380 manufacturing
Findings
Conclusion
Full Text
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