During your Engineering Peaks, Spires is able to assist your team in developing Interface Load reports through our Finite Element Analysis software Nastran/Patran, Abacas and Ansys, as well the ability to perform hand calculations to proof the derived Software solution. We are your extended arm in assisting you to meet your objectives within a very competitive aerospace sector!
Our Finite Element Analysis team can assist you from creating a mesh analysis study, Fatigue and damage tolerance components using Nastran, Patran, Abacus and Ansys to produce a full interface load report.
Through our Finite Element Analysis knowledge-based team, which has extensive years of experience in FEA for Aircraft structural components be it for Primary or Secondary Structures we have a full ‘24hr around the clock capability’’ to support your daily needs.
We can produce detailed Finite element models for component assemblies, providing full static and fatigue analysis:
Linear and non-linear static modal and dynamic analysis, fatigue failure prediction, stress concentrations, Max strain, and Bearing Post-buckling.
Typical Interface Load reports that have been completed by Spires Engineering Consultancy team are:
- Aircraft Metallic Rib design
- Composite Spar
- Aircraft Sandwich Panel
- Composite Flap Track Fairing
- Cabin Interiors i.e, Monuments, Gallies, and Seating design
Compatible file types accepted include the following:
If you have any questions about our Finite Element Analysis at Spires Engineering Consultancy? Please call one of our engineers now +44(0)1865 910296 or send us an email by clicking here.