Aeronautical
Development of aircraft components and structures
Development of aircraft components and structures
We have a Development Engineering group capable of covering the different phases, from structural analysis and design to manufacturing engineering.
We have extensive experience in the use of calculation tools (Catia V5, Nastran, Abaqus, ISAMI, PDM-Link, etc.).
We carry out concurrent engineering from the initial phase of the project.
We master the use and processing of the most commonly used reinforced composite materials (thermoplastics and phenolic or epoxy resins reinforced with carbon or glass fiber).
Cidaut has carried out the detailed sizing and design of the metal structure of the Belly Fairing of the AIRBUS A350XWB.
Processing of polymeric and metallic materials
Prototyping of reinforced composite materials in open and closed mold
Analysis of materials and characterization of their properties
Manufacture of special tools
Execution of special tests on component
Industrialization and modernization of production operations
We make the characterization and validation of all types of materials (metallic, plastic, foamed, elastomeric, textile, composite) as well as their structural joints (riveted, welded, screwed, adhesive, etc.), using tests of: traction, compression, bending, peeling, creep , impact, fatigue, fracture mechanics and vibroacoustics.
We design and execute component tests whether they are R&D&i, support or development, validation or industrialization. Once the client's needs are known, we begin with the virtual test, to help us define the process, later we design and manufacture the tooling and finally we carry out the tests in our facilities. We are capable of carrying out static, dynamic, vibroacoustic and fatigue tests considering a wide range of loads, displacements and frequencies.
We have appropriate equipment and facilities to prototype and manufacture any development:
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