Stub frame for a cascade thrust reverser structure

The invention relates to a stub frame (121) for a cascade thrust reverser structure of a nacelle (101) of an aircraft, said stub frame (121) being intended for being fastened to one or more cascade vanes (113, 181) and including an integral primary structure (141) with a substantially C-shaped longi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BOUILLON FLORENT, BARDIN STEPHANE, BELLANGER ALEXANDRE, DUBOIS LAURENT
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention relates to a stub frame (121) for a cascade thrust reverser structure of a nacelle (101) of an aircraft, said stub frame (121) being intended for being fastened to one or more cascade vanes (113, 181) and including an integral primary structure (141) with a substantially C-shaped longitudinal section, a secondary structure (143) acting as a cascade edge and attached to said primary structure (141) at one end, and transverse stiffeners (145) connecting the two ends (142, 144) of the primary structure (141). The invention also relates to a cascade thrust reverser structure and a nacelle comprising such a stub frame.