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.


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    Title :

    AN ATTACHMENT FOR SUSPENDING AN AIRCRAFT ENGINE


    Additional title:

    BEFESTIGUNG ZUM AUFHÄNGEN EINES FLUGZEUGTRIEBWERKS
    ATTACHE POUR LA SUSPENSION D'UN MOTEUR D'AÉRONEF


    Contributors:

    Publication date :

    2023-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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