An attachment 107 for attaching an aircraft engine 106 with a first receiving element 108 to an aircraft structure 105 with a second receiving element 109 may include at least three fasteners 114 and a stacked layer 110. Stacked layer 110 may include at least two sheets 111, at least three holes 113 through the stacked layer 110, a first connecting portion 115 that includes a first hole 113 of the at least three holes 113, a second connecting portion 116 that includes second and third holes 113 of the at least three holes 113, and a suspension portion 117 that is located between the first connecting portion 115 and the second connecting portion 116.
AN ATTACHMENT FOR SUSPENDING AN AIRCRAFT ENGINE
BEFESTIGUNG ZUM AUFHÄNGEN EINES FLUGZEUGTRIEBWERKS
ATTACHE POUR LA SUSPENSION D'UN MOTEUR D'AÉRONEF
2023-09-06
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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