SET COMPRISING AN AIRCRAFT TURBOMACHINE AND ITS MOUNTING PYLON

FR3156428A1Pending Publication Date: 2025-06-13SAFRAN AIRCRAFT ENGINES SAS
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Patent Information

Application Number
FR2023013864
Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2023-12-08
Publication Date
2025-06-13
Patent Text Reader

Abstract

The invention relates to an assembly (1) comprising an aircraft turbomachine (2), a pylon (40) for attaching the turbomachine to an element of the aircraft, and a system for suspending the turbomachine from the pylon, the turbomachine having a longitudinal axis (X) and comprising from upstream to downstream, in the direction of gas flow: > a fan casing (11) extending around the longitudinal axis, and > a gas generator (16) configured to receive an air flow generated by a fan, the pylon (40) being of generally elongated shape along said longitudinal axis and being capable of being fixed to the element of the aircraft, characterized in that connecting elements of the suspension system are all located upstream of the combustion chamber (19). Figure for abstract: Fig. 1
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Citation Information

Patent Citations

  • ASSEMBLY COMPRISING AN AIRCRAFT TURBOMACHINE AND ITS MOUNTING PYLONE

    FR3114129A1

  • Engine assembly for aircraft comprising an engine as well as a device for locking said engine

    WO2007033994A1

  • Structural assembly disposed between the attachment pylon and the fan casing of an aircraft engine

    WO2012085388A1

  • Structure for linking and supporting a turbine engine on an aircraft pylon

    WO2022248791A1