CASE STRUCTURE INTERPOSED BETWEEN THE ENGINE AND THE NACELLE WITH JOINTED FERRULE SEGMENTS

A case structure interposed between the engine and the nacelle of the aircraft including: a ferrule surrounding the engine and comprising a plurality of segments (12A, 12B), at least one radial arm (14) ensuring connection to the nacelle, a plurality of attachment means for securing this plurality o...

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Bibliographische Detailangaben
Hauptverfasser:	BELJAMBE CEDDRIC, DAUTREPPE FREDERIC, ROBIN NOEL
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A case structure interposed between the engine and the nacelle of the aircraft including: a ferrule surrounding the engine and comprising a plurality of segments (12A, 12B), at least one radial arm (14) ensuring connection to the nacelle, a plurality of attachment means for securing this plurality of ferrule segments together or with at least one radial arm, the plurality of attachment means including an articulation device (24) configured for ensuring coupling of the lifted-rotated-pushed type ensuring after disengagement of the ferrule segment, its pivoting about a pivot axis parallel to a longitudinal axis of said engine and then its blocking in a disengagement position.