ASSEMBLY BETWEEN AN AIRCRAFT PYLON AND A TURBOMACHINE

The invention relates to an assembly between an aircraft pylon (30) and a turbomachine (20) of longitudinal axis (X), the pylon (30) and the turbomachine (20) each comprising front and rear longitudinal regions, the assembly comprising a rear support (40) configured to connect the rear region of the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	GLEMAREC, Guillaume, MAINGRE, Eric François Michel, VIGNES, Jean-Baptiste, SEIZE, Guilhem
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to an assembly between an aircraft pylon (30) and a turbomachine (20) of longitudinal axis (X), the pylon (30) and the turbomachine (20) each comprising front and rear longitudinal regions, the assembly comprising a rear support (40) configured to connect the rear region of the turbomachine (20) to the rear region of the pylon (30), the assembly being characterized in that the rear support (40) comprises a sliding pivot connection arranged between the rear region of the turbomachine (20) and the rear region of the pylon (30), so as to allow the turbomachine (20) only translational and rotational movements along and about the longitudinal axis (X) and along and about a vertical axis (Z) and a rotational movement about a transverse axis (Y). L'invention concerne un assemblage entre un pylône (30) d'aéronef et une turbomachine (20) d'axe longitudinal (X), le pylône (30) et la turbomachine (20) comportant chacun des zones longitudinales avant et arrière, l'assemblage comportant un support arrière (40) configuré pour relier la zone arrière de la turbomachine (20) à la zone arrière du pylône (30), l'assemblage étant caractérisé en ce que le support arrière (40) comporte une liaison pivot glissant agencée entre la zone arrière de la turbomachine (20) et la zone arrière du pylône (30) de manière à autoriser à la turbomachine (20) seulement des mouvements de translation et de rotation selon l'axe longitudinal (X) et selon un axe vertical (Z) et un mouvement de rotation selon un axe transversal (Y).