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    Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods
    2.
    发明授权
    Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods 有权

    公开(公告)号：US11332255B2

    公开(公告)日：2022-05-17

    申请号：US16352332

    申请日：2019-03-13

    申请人： Airbus Operations (S.A.S.)

    发明人： Olivier Pautis ,  Jérôme Colmagro ,  Jonathan Blanc

    IPC分类号： B64D27/26

    摘要： A primary structure of a strut for bearing an aircraft power plant including a front part intended to be joined to an aircraft power plant and a rear part intended to be joined to a structure of the aircraft, the front part being formed from a box including an upper longitudinal member, a lower longitudinal member, and lateral panels. A main rib is located at an interface between the front part and the rear part. The rear part is formed from a set of four connecting rods. The first end of each connecting rod is joined to the front part of the primary structure and the second end of each connecting rod is joined to a separate interface for fastening to the structure of the aircraft. This allows a substantial simplification of the primary structure of a strut for bearing an aircraft power plant, which can have advantages in particular in terms of cost, mass, and simplicity of implementation and integration.

    AIRCRAFT ASSEMBLY COMPRISING A MOUNTING STRUT BUILT INTO THE NACELLE AND ARRANGED AT THE REAR SECTION OF THE FUSELAGE
    3.
    发明申请
    AIRCRAFT ASSEMBLY COMPRISING A MOUNTING STRUT BUILT INTO THE NACELLE AND ARRANGED AT THE REAR SECTION OF THE FUSELAGE 审中-公开
    包括安装在内的飞机组件安装在NACELLE上并安装在FUSELAGE的后面部分

    公开(公告)号：US20150259074A1

    公开(公告)日：2015-09-17

    申请号：US14575332

    申请日：2014-12-18

    申请人： Airbus Operations (S.A.S.)

    发明人： Julien Guillemaut ,  Sébastien Alby ,  Jérôme Colmagro ,  Pascal Pome ,  Jonathan Blanc ,  Thomas Robiglio ,  Tobias Sjostrom

    IPC分类号： B64D27/26 ,  B64D29/06

    CPC分类号： B64D27/26 ,  B64D27/20 ,  B64D2027/262

    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.

    摘要翻译： 为了减少发动机变形，本文公开的主题提供了一种用于飞行器的组件，其包括飞行器后部，发动机，机舱和用于将发动机安装在后部上的安装支柱，该组件还包括安装 将发动机安装在支柱的刚性结构上，该安装件包括两个发动机支架，其被设计成反应由发动机产生的轴向推力。 根据本文公开的主题，支柱的刚性结构包括部分包围发动机的第一部分，该第一部分包括形成机舱的外部空气动力学表面的一部分的外部皮肤，并且两个发动机支架沿径向相对 彼此在刚性结构的后部附接到第一部分。

    PRIMARY STRUCTURE OF A STRUT FOR BEARING AN AIRCRAFT POWER PLANT, THE REAR PART OF WHICH IS FORMED BY A SET OF CONNECTING RODS
    5.
    发明申请
    PRIMARY STRUCTURE OF A STRUT FOR BEARING AN AIRCRAFT POWER PLANT, THE REAR PART OF WHICH IS FORMED BY A SET OF CONNECTING RODS 审中-公开

    公开(公告)号：US20190283890A1

    公开(公告)日：2019-09-19

    申请号：US16352332

    申请日：2019-03-13

    申请人： Airbus Operations (S.A.S.)

    发明人： Olivier Pautis ,  Jérôme Colmagro ,  Jonathan Blanc

    IPC分类号： B64D27/26

    摘要： A primary structure of a strut for bearing an aircraft power plant including a front part intended to be joined to an aircraft power plant and a rear part intended to be joined to a structure of the aircraft, the front part being formed from a box including an upper longitudinal member, a lower longitudinal member, and lateral panels. A main rib is located at an interface between the front part and the rear part. The rear part is formed from a set of four connecting rods. The first end of each connecting rod is joined to the front part of the primary structure and the second end of each connecting rod is joined to a separate interface for fastening to the structure of the aircraft. This allows a substantial simplification of the primary structure of a strut for bearing an aircraft power plant, which can have advantages in particular in terms of cost, mass, and simplicity of implementation and integration.

    ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN ENGINE ATTACHMENT BODY EQUIPPED WITH AT LEAST ONE SHACKLE SUPPORT FITTING THAT PASSES INTO THE BOX SECTION OF THE ATTACHMENT PYLON
    8.
    发明申请
    ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN ENGINE ATTACHMENT BODY EQUIPPED WITH AT LEAST ONE SHACKLE SUPPORT FITTING THAT PASSES INTO THE BOX SECTION OF THE ATTACHMENT PYLON 有权
    组装飞机，包括发动机附件机身，配有至少一个SHACKLE支撑配件，将其插入附件PYLON的箱体部分

    公开(公告)号：US20150197341A1

    公开(公告)日：2015-07-16

    申请号：US14571786

    申请日：2014-12-16

    申请人： Airbus Operations (S.A.S.)

    发明人： David Ewens ,  Jonathan Blanc

    IPC分类号： B64D27/26 ,  B64F5/00

    CPC分类号： B64D27/26 ,  B64D27/18 ,  B64D2027/262 ,  B64D2027/264 ,  B64D2027/266 ,  B64F5/40 ,  Y10T29/49815

    摘要： In order to allow better introduction of forces into the box section of an aircraft engine attachment pylon, the subject matter herein discloses a pylon including a primary structure forming a box section on the outside of which a body of the engine attachment is arranged, the latter also being equipped with shackles that are articulated on the body and can be articulated on the engine. According to the disclosure herein, the body has, at at least one of its ends, a one-piece fitting including a first joining portion on which one of the shackles can be articulated, and also a second joining portion that is fixed to the box section and passes into the latter.

    摘要翻译： 为了更好地将力引入到飞机发动机附件塔的箱部分中，本发明的主题公开了一种吊架，其包括在其外侧上形成有发动机附件的主体的后部的主体结构， 还配备有在身体上铰接并可以在发动机上铰接的手铐。 根据本文的公开内容，本体在其至少一个端部具有一体式配件，其包括第一接合部分，其中钩环中的一个可以铰接在其上，第二接合部分固定到箱体 并进入后者。