Device for intermediate fastening between an aircraft fuselage and an aircraft undercarriage

The structure has support element (S) that is provided with the abutments. The panel elements are formed with the edge portions engaged by the abutments. A channel-shaped element is arranged for retaining the panel elements against the abutments. The channel-shaped element is engaged against the fac...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Bellet, Daniel, Gallant, Guillaume
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:The structure has support element (S) that is provided with the abutments. The panel elements are formed with the edge portions engaged by the abutments. A channel-shaped element is arranged for retaining the panel elements against the abutments. The channel-shaped element is engaged against the face of support for retaining the panel elements against the abutments. The support element is provided with longitudinal shoulders. A face plate (4) is formed for engaging support element and is provided with shoulders uniform with those on support element.