Finite Element Analysis

cabin interiors - tray table

Client's original preferred internal design producing 78mm displacement and twist under load 

Client's original preferred internal design producing 78mm displacement and twist under load 

Our revised design delivering an acceptable 20mm displacement and no twist

Our revised design delivering an acceptable 20mm displacement and no twist

An interim 413 Mpa, down from 2651 Mpa with the original design, but still unacceptable

An interim 413 Mpa, down from 2651 Mpa with the original design, but still unacceptable

After internal redesign and interlocking hinge applied, 223 Mpa is well within material tolerance

After internal redesign and interlocking hinge applied, 223 Mpa is well within material tolerance

aerospace

Examination of component design failure modes at a range of temperatures

Examination of component design failure modes at a range of temperatures

Displacement investigation to understand the reasons for repeated 'creep' after repeated re-locking

Displacement investigation to understand the reasons for repeated 'creep' after repeated re-locking

water management

Displacement analysis to prove clip strength

Displacement analysis to prove clip strength