Invention Grant
US08561941B2 Pin system for the connection assembly of an engine pylon underneath a wing of an aircraft
有权
引擎系统,用于在飞机机翼下方的发动机塔架的连接组件
- Patent Title: Pin system for the connection assembly of an engine pylon underneath a wing of an aircraft
- Patent Title (中): 引擎系统,用于在飞机机翼下方的发动机塔架的连接组件
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Application No.: US13078593Application Date: 2011-04-01
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Publication No.: US08561941B2Publication Date: 2013-10-22
- Inventor: Stephane Combes , Pascal Gardes
- Applicant: Stephane Combes , Pascal Gardes
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations S.A.S.
- Current Assignee: Airbus Operations S.A.S.
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1052537 20100402
- Main IPC: B64D27/00
- IPC: B64D27/00

Abstract:
A connection assembly of an engine pylon underneath an aircraft wing, the wing being provided with a fitting, the engine pylon being provided with a fork joint nested in the fitting and fixed to the said fitting by means of a traversing pin system, including: an external primary pin, a secondary pin mounted inside the primary pin, a primary shoulder mounted directly around the primary pin, at a blind end of the pin system, to block the said pin in translation, a secondary shoulder mounted around one end of the secondary pin, at a blind end of the pin system, to block the system in rotation, and an interlocking assembly mounted around the primary pin and the secondary pin, at a free end of the pin system, to block the pin system in translation.
Public/Granted literature
- US20110266389A1 PIN SYSTEM FOR THE CONNECTION ASSEMBLY OF AN ENGINE PYLON UNDERNEATH A WING OF AN AIRCRAFT Public/Granted day:2011-11-03
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