An inboard beam includes a body having an upper flange and a lower flange coupled thereto. The upper flange includes a first upper inboard aperture and an upper outboard aperture formed therein. The lower flange includes a first lower inboard aperture and a lower outboard aperture formed therein. An upper beam fitting is coupled to the upper flange and lower beam fitting is coupled to the lower flange. The upper beam fitting includes a first upper inboard post. The upper beam fitting includes an upper outboard post extending parallel to the inboard post. The lower beam fitting includes a first lower inboard post. The lower beam fitting includes a lower outboard post extending parallel to the lower inboard post.
Inboard beam with pin system for anti-rotation and centrifugal force retention
2021-03-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
INBOARD BEAM WITH PIN SYSTEM FOR ANTI-ROTATION AND CENTRIFUGAL FORCE RETENTION
European Patent Office | 2020
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