STRUCTURE D'AÉRONEF COMPRENANT UN CAPTEUR AVEC UN SYSTÈME DE JONCTION AMÉLIORÉ ET AÉRONEF COMPRENANT LADITE STRUCTURE
STRUCTURE D'AÉRONEF COMPRENANT UN CAPTEUR AVEC UN SYSTÈME DE JONCTION AMÉLIORÉ ET AÉRONEF COMPRENANT LADITE STRUCTURE
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A sensor is fixed on an aircraft structure by a joining system which includes at least one enclosure in which is positioned at least one transducer, at least one passage configured to allow at least one conducting element to pass through the enclosure, at least one flexible connection connecting each transducer present in the enclosure to said enclosure and at least one binder joining together the enclosure and the structure. This joining system makes it possible to limit the spread of the deformations of the structure toward the transducer or transducers and ultimately the risks of malfunction.
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STRUCTURE D'AÉRONEF COMPRENANT UN CAPTEUR AVEC UN SYSTÈME DE JONCTION AMÉLIORÉ ET AÉRONEF COMPRENANT LADITE STRUCTURE
AIRCRAFT STRUCTURE COMPRISING A SENSOR WITH AN IMPROVED JOINING SYSTEM AND AIRCRAFT COMPRISING SAID STRUCTURE
LUFTFAHRZEUGSTRUKTUR, DIE EINEN SENSOR MIT EINEM VERBESSERTEN VERBINDUNGSSYSTEM UMFASST, UND LUFTFAHRZEUG, DAS DIESE STRUKTUR UMFASST
2020-08-19
Patent
Electronic Resource
French
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