According to one embodiment, a structure for an aircraft includes a first structural member (2), a second structural member (3) coupled to the first structural member (2), a fastener (4) and a conductive object (5). The fastener (4) couples the first structural member (2) to the second structural member (3). The fastener (4) is inserted into an insertion hole formed in a portion where the first structural member (2) is overlapped with the second structural member (3). The fastener (4) is in electrically non-contact with the first and second structural members (2, 3) in the insertion hole. The conductive object (5) is embedded inside at least either one of the first and second structural members (2, 3). The conductive object (5) prevents a spark between the fastener (4) and each of the first and second structural members (2, 3) by forming a current pathway that leads current, flowing inside the at least either one of the first and second structural members (2, 3), to the other structural member.
STRUCTURE FOR AIRCRAFT, METHOD OF MANUFACTURING STRUCTURE FOR AIRCRAFT AND METHOD OF MAKING DESIGN INFORMATION OF STRUCTURE FOR AIRCRAFT
FLUGZEUGSTRUKTUR, VERFAHREN ZUR HERSTELLUNG EINER STRUKTUR FÜR EIN FLUGZEUG UND VERFAHREN ZUR HERSTELLUNG VON ENTWURFSINFORMATIONEN EINER STRUKTUR FÜR EIN FLUGZEUG
STRUCTURE POUR AÉRONEF, PROCÉDÉ DE FABRICATION DE STRUCTURE D'AÉRONEF ET PROCÉDÉ DE FABRICATION D'UNE STRUCTURE D'INFORMATIONS DE CONCEPTION POUR AÉRONEF
2018-04-11
Patent
Elektronische Ressource
Englisch
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