FEMPLY

 
 

AeroFEM is selling partner of PlySim Analysis Services for FEMPLY.

 

FEMPLY is a Composite Ply-Based Modelling tool fully integrated into Siemens' FEMAP Pre/ Post-processor offering gast, efficient and simple definition of complex component layups.

 

Developed by PlySim, a leading Composites Engineering Consultancy, FEMPLY is a versatile tool developed and used by Composite Engieneers on real-world projects in a wide range of markets.

 

Perpetual Node-locked and Network Floating licenses are available.

  

Features:

 

FEMPLY includes a large range of features to improve the Simplicity, Speed, Versatility and Reliability of Composite Pre and Post-processing:

 

 
  • Simple,intuitive user interface.
 
  • Edit multiple plies in one operation.
 
  • Completely integrated into FEMAP. No exporting to external programs required.
 
  • A single definition of Laminate Properties, Failure Theorem and Offsets can be applied all Composite Property sets.

 
  • Geometry Independent.

 
  • Automaticallyre-mapexistingpliesontoa newmeshoraftermesh refinement.
 
  • Import Plies, Materials and Properties from other FEMPLY layup files.

 
  • Ply definitions are unrestricted by interior holes etc.

 
  • FEMPLY Layup Files can be easily read,modified or written by in-house
    programs.

 
  • FEMPLY uses FEMAP’s Global Ply functionality for easy post-processing.

 
  • Import Global Plies from legacy models.

 

Fly Draping Analyses and Flat Ply Shape Export

 

 
  • Accurately account for fibre angle deviation during the manufacture process.
 
  • Verify planned production processes.
 
  • Reduce the need for modifications or redesign late in the manufacturing process. 
 
  • Directly extract 2d CAD ply shapes for use in ply booklets or cutting patterns.
 
  • Enhance the accuracy and reproducibility of the component

 

Advanced Failure Theorem Post-Processing

 

 
  • Robust Post-Processing to Hill, Hoffman, Tsai-Wu, Max Stress, Max

    Strain, Puck, Cuntze, LaRC02 and User-Defined failure theorems.
 
  • Inverse ReservFactors.
 
  • Output vectors by Layer,GlobalPly and Maximum.
 
  • Critical Ply and Fibre Angle output vectors to quickly and easily identify critical areas.
 
  • Sandwich Stability Calculations for Skin Wrinkling, Shear Crimping and          Honeycomb Dimpling.
 
  • Failure Envelope Charting and Export. 

 

 

Laminate, Bill of Materials and Failure Calculation Reporting

 

 
  • Automated Mirosoft Word reporting of Failure Theorems, Failure Envelopes, Failure Indices and Critical Results
 
  • Bill of Material, Layup, Ply and Material Summary Reports including layup and ply application region images.
 
  • Sandwich Stability Reports including Failure Theorem summary, Failure Envelopes, Failure Indices and Critical Results.

 

 

AeroFEM-FEMPLY Brochure_2015.pdf

 

 

 

 

 

 

 

 

 

 

 

  

 

 

 

   

 

 

 

  

 

 

 

 

 

 

 

 
 

 

Für mehr Informationen

kontaktieren Sie:

 

 

 

 

 

 

 

 

Andres Graf

AeroFEM GmbH

Aumühlestrasse 10

CH-6373 Ennetbürgen

Telefon

+41 (0)41 619 85 12

agraf(a)aerofem.com