发明名称 AIRCRAFT ASSEMBLY COMPRISING A MOUNTING STRUT BUILT INTO THE NACELLE AND ARRANGED AT THE REAR SECTION OF THE FUSELAGE
摘要 In order to reduce engine deformation, the subject matter disclosed herein provides an assembly for an aircraft, comprising an aircraft rear section, an engine, a nacelle, and a mounting strut for mounting the engine on the rear section, the assembly also comprising mounting for mounting the engine on a rigid structure of the strut, the mounting comprising two engine mounts designed to react the axial thrust forces generated by the engine. According to the subject matter disclosed herein, the rigid structure of the strut comprises a first portion partially enveloping the engine, this first portion comprising an external skin forming part of an external aerodynamic surface of the nacelle, and the two engine mounts are arranged diametrically opposite each other at the rear of the rigid structure, being attached to the first portion.
申请公布号 US2015259074(A1) 申请公布日期 2015.09.17
申请号 US201414575332 申请日期 2014.12.18
申请人 Airbus Operations (S.A.S.) 发明人 Guillemaut Julien;Alby Sébastien;Colmagro Jérôme;Pome Pascal;Blanc Jonathan;Robiglio Thomas;Sjostrom Tobias
分类号 B64D27/26;B64D29/06 主分类号 B64D27/26
代理机构 代理人
主权项 1. An assembly for an aircraft, comprising an aircraft rear section, an engine, a nacelle, and a mounting strut for mounting the engine on the rear section, the assembly also comprising mounting for mounting the engine on a rigid structure of the mounting strut, the mounting comprising two engine mounts designed to react the axial thrust forces generated by the engine, wherein the rigid structure of the strut comprises a first portion partially enveloping the engine, the first portion comprising an external skin forming part of an external aerodynamic surface of the nacelle, and wherein the two engine mounts that react the axial thrust forces are arranged diametrically opposite each other at the rear of the rigid structure, being attached to the first portion.
地址 Toulouse FR