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 perform 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: tension, compression, bending, peeling, creep, impact, fatigue, fracture mechanics and vibroacoustics.
We design and execute component tests for R&D, support, development, validation, and industrialization. Once we understand the client's needs, we begin with virtual testing to help define the process. We then design and manufacture the tooling, and finally, we perform the tests at our facilities. We are capable of conducting 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:
The COMANDO project, in which CIDAUT (Castilla y León) participates along with CTAG (Galicia), IBV and ITENE (Valencian Community),…
Implementation period: from January 1, 2025 to December 31, 2025. Project objective The objective…
The project entitled “Research on Thermoplastic Materials and Induction Bonding Processes for High-Value Functional Structural Applications…
EXPLORATION OF STRUCTURE-PROPERTY RELATIONSHIPS BY ALTERING GLYCOL BACKBONE UNSATURATION (DOUBLE/TRIPLE BONDS) IN FURAN-BASED POLYESTERS
REUSABLE FIBER COMPOSITE CRASH BOXES FOR SUSTAINABLE AND RESOURCE-EFFICIENT MOBILITY
A NEW EXPLANED BEAD FOAM BASED ON BIO-POLYPROPYLENE (BioEPP): FABRICATION AND REINFORCEMENT WITH NANOPARTICLES