Design and Engineering Analysis Capability

The Aerospace Engineering Services Design organisation specialises in the preparation and management of structural and systems offload work packages, using a comprehensive range of CAD, stress and knowledge based engineering  tools including, CATIA and ICAD.

The scope of these capabilities covers:

Structural & Mechanical Design

  • Aircraft wing primary metallic structure
  • Flaps and ailerons (composite & metallic)
  • Aircraft doors
  • Fuselage structure
  • Engine pylons & nacelles
  • Primary composite structure
  • Composite fairings
  • Mechanical systems
  • Rail body shell & interior
  • Automotive chassis, body & trim
  • Jet engine component design
  • Marine design

Airbus A380 Design Participation

Static Strength Analysis

  • Classical methods
  • Computer automated
  • FE & BE modelling
  • MSC Nastran / Patran
  • MSC FatigueBeasy, Ansys

Electrical Design & Installation

  • Avionics system integration
  • Aircraft systems update
  • Wiring & schematic diagrams

Loads

  • Aircraft and component loads
  • Weight critical design evaluation
  • Aircraft take-off mass / CG analysis

CAD Systems

  • CATIA, CADDS 5, CADAM
  • Anvil 1000, 4000 & 5000
  • Intergraph EMS, I-Deas
  • Electricad & BCAWD

Structural Integrity

  • Stress surveys
  • Fatigue life assessment
  • Stress concentrations & LEFM
  • Stress intensities
  • Crack growth scenarios

Design Support

  • Concurrent engineering
  • Modifications & repair schemes
     
Design

Site Modified 13 July 2010 by Phil Edon    Phil.edon@ukes.aerospace.gknplc.com

 

 

Aerospace Engineering Services