公开(公告)号：US20110266389A1

公开(公告)日：2011-11-03

申请号：US13078593

申请日：2011-04-01

Applicant: Stephane COMBES ,  Pascal Gardes

Inventor： Stephane COMBES ,  Pascal Gardes

IPC: B64D27/02 ,  B23P11/00

CPC classification number: B64D27/26 ,  B64D29/06 ,  F16B21/16

Abstract: The invention relates to a connection assembly of an engine pylori underneath an aircraft wing, the wing being provided with a fitting (6), the engine pylori being provided with a fork joint (5) nested in the fitting and fixed to the said fitting by means of a traversing pin system (10), provided with: an external primary pin (11), a secondary pin (12) mounted inside the primary pin, a primary shoulder (13) mounted directly around the primary pin, at a blind end of the pin system, to block the said pin in translation, a secondary shoulder (14) mounted around one end of the secondary pin, at a blind end of the pin system, to block the system in rotation, an interlocking assembly (15, 16) mounted around the primary pin and the secondary pin, at a free end of the pin system, to block the pin system in translation.

Abstract translation: 本发明涉及飞机机翼下方的发动机幽门螺杆的连接组件，翼部设置有配件（6），发动机幽门设置有嵌套在配件中的叉接头（5），并通过 具有：外部主销（11），安装在所述主销内部的辅助销（12）的横向销系统（10）的装置，在所述主销周边直接安装的主肩部（13） 所述销系统中的所述销平移，在所述销系统的盲端处安装在所述副销的一端周围的次级肩部（14），以阻止所述系统旋转;联锁组件（15， 16）安装在主销和辅助销周围，在销系统的自由端，以平移来阻止销系统。