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