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CUT-OUT REINFORCEMENT [1 record]

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Record 1 2007-04-12

English

Subject field(s)
  • Aircraft Airframe
CONT

The aim of this thesis work is to develop an effective cut-out reinforcement for composite sandwich fuselage shells. Because flat plate theory shows that only tangential stresses act in the vicinity of the cut-out, the proposed reinforcement concept involves fibres oriented in parallel to the edge of the cut-out. As no production process was suitable for producing the desired reinforcement, a process based on the working of simple yo-yo is designed and implemented. A preliminary assessment of the effectiveness of the reinforcement concept is made by subjecting two test plates (one reference plate and one reinforced plate) to a uniaxial tension test.

Key term(s)
  • cutout reinforcement
  • cut out reinforcement

French

Domaine(s)
  • Cellule d'aéronefs

Spanish

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