The invention relates to an assembly for attaching a pylon (104) to an aircraft engine (102), the assembly comprising an engine front mount (150) comprising a front tang (112) and a front clevis (113), a lower tang (114) and a lower clevis (115), and a port/starboard link (118), the front tang and the front clevis connect the attachment pylon and the engine via a front pin (120) mounted in the front tang and the front clevis, and the lower tang and the lower clevis connect the attachment pylon and the engine via a lower pin (122) mounted in the lower tang and the lower clevis, and a port/starboard link mounted between the attachment pylon and the engine via a mounting pin, where the front pin and the lower pin are orthogonal to the mid-plane (XZ), and where the mounting pin of the link is parallel to the mid-plane (XZ). The vertical occupied space of the assembly is reduced.
本发明涉及一种附接吊挂架(104)与飞行器发动机(102)的组件,该组件包括发动机前安装件(150),该发动机前安装件包括前柄脚(112)和前连接叉(113)、下柄脚(114)和下连接叉(115)、以及左舷/右舷连杆(118),该前柄脚和该前连接叉经由安装在该前柄脚和该前连接叉中的前销(120)将附接吊挂架和发动机相连接,该下柄脚和该下连接叉经由安装在该下柄脚和该下连接叉中的下销(122)将附接吊挂架和发动机相连接,该左舷/右舷连杆经由安装销而安装在附接吊挂架与发动机之间,其中,前销和下销正交于中平面(XZ),并且其中,连杆的安装销平行于中平面(XZ)。这样的组件的竖直占用空间减小。
Assembly for attaching pylon to aircraft engine
附接吊挂架与飞行器发动机的组件
03.01.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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