5. Conclusion and outlook
From an aeronautical engineering point of view, understanding mechanical performance in the event of fire is an essential safety issue, as the loss of stiffness, strength and creep resistance can lead to the deformation and collapse of aeronautical composite structures, with catastrophic consequences. Thus, the structural properties of composites under thermal stress (high temperature or flame) are fundamental data for the dimensioning of parts and structures in parts of the aircraft where certification standards are very strict.
In order to establish design rules, this article provides information on the specific methodology and characteristic behaviors and properties needed to better understand thermomechanical couplings within composite materials subjected to critical conditions in service. In particular, this requires the use of specific test facilities that...
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Conclusion and outlook
Bibliography
Standards and norms
- Federal Aviation Regulations (FAR) standard – Powerplant Installation and Propulsion System Component Fire Protection Test Methods, Standards and Criteria with Change. - FAA AC20-135 - 1990
- Aircraft: environmental testing method for on-board equipment – Fire resistance in designated "fire zones". - ISO 2685 - 1998
- Federal Aviation Regulations (FAR) standard – Fire Test to aircraft material – test method...
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