A350XWB S19.1 – Front Firewall Static Strength Analysis
S19.1 – Front Firewall – Linear and Non-Linear Static Calculation (composite and metallic) and Acoustic Fatigue
A320-800 S19.1 Air Intake System Acoustic Fatigue
Dynamic calculation and acoustic fatigue analysis of A320 Air Intake
S80+ Consoles. Vibration and shock
Vibration (MIL-STD-810), shock (MIL-S-901) and thermal (CFD) analysis of the S80+ submarine consoles.
RBX Radar. Vibrations and shock
A350XWB Section 19 – Aircraft Structures
S19 A350XWB – Calculation of aircraft structures: fatigue and damage tolerance analysis, finite element modelling (GFEM and DFEM), non-linear simulation of structures, optimisation, automation and scheduling of processes, and definition of calculation methodologies.
Frigate F110 – Vibration and shock of control consoles
Vibration (MIL-STD-810) and shock (MIL-DTL-901E, including DSSM) analysis of the F110 Frigate’s 2- and 3-monitor consoles.
A350XWB S19.1 – Static and Fatigue & DT Analysis
Linear and non-linear static calculation (metallic and composite material), fatigue and crack growth calculation, and acoustic fatigue calculation of S19.1
Dynamic Load Analysis of C295
Dynamic load analysis of C295 aircraft and derivaties: dynamic landing, discrete gust, continuous turbulence, taxi, torpedoes and payload release, and blade loss.
Static Analysis of S18, S19 and CWB
Structural Analysis and Justification associated with the Integration of the Advanced Refueling Boom System (ARBS) on the A-330 MRTT Aircraft
A320-800 S19.1 Exhaust System Acoustic Fatigue
A320 Exhaust dynamic calculation and acoustic fatigue analysis
A380 Wing Booms
ICEMM carried out a resizing analysis of the A380 wing booms. This resizing was carried out to correct the cracks that appeared in the ‘Booms’ as a consequence of the existence of additional stresses derived from the manufacturing and assembly process.
A380-e Belly Fairing
ICEMM has participated in the analysis of the metallic structure of the belly fairing of the Airbus A380-e. In this project, the analytical calculation of the different elements that make up the metallic structure of the belly fairing (stringers, frames, cross fittings, bars, etc.) has been carried out, starting from the parts of the Airbus A380_ALS08-S3i2 belly fairing model and resizing all the impacted parts.
