An attachment for attaching an aircraft engine with a first receiving element to an aircraft structure with a second receiving element may include at least three fasteners and a stacked layer. Stacked layer may include at least two sheets, at least three holes through the stacked layer, a first connecting portion that includes a first hole of the at least three holes, a second connecting portion that includes second and third holes of the at least three holes, and a suspension portion that is located between the first connecting portion and the second connecting portion.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ATTACHMENT FOR SUSPENDING AN AIRCRAFT ENGINE


    Beteiligte:
    BLACHA MARTIN (Autor:in) / SCHELCHER MARC (Autor:in) / GARCIA RIOS ADRIANA (Autor:in)

    Erscheinungsdatum :

    11.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Attachment for suspending an aircraft engine

    BLACHA MARTIN / SCHELCHER MARC / GARCIA RIOS ADRIANA | Europäisches Patentamt | 2022

    Freier Zugriff

    AN ATTACHMENT FOR SUSPENDING AIRCRAFT ENGINE

    BLACHA MARTIN / SCHELCHER MARC / GARCIA RIOS ADRIANA | Europäisches Patentamt | 2021

    Freier Zugriff

    AN ATTACHMENT FOR SUSPENDING AN AIRCRAFT ENGINE

    BLACHA MARTIN / SCHELCHER MARC / GARCIA RIOS ADRIANA | Europäisches Patentamt | 2023

    Freier Zugriff

    Beam for suspending a turboshaft engine from an aircraft structure

    DUNLEAVY PATRICK / LEFORT GUILLAUME / MASSON RICHARD et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Support used for suspending engine

    JIANG JIANPING / JIANG QIAN | Europäisches Patentamt | 2015

    Freier Zugriff